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![Aircraft Logbook Entry
XXX Partners Inc. Work Order: 291419 Date: October 22 , 2012
Serial Number: 2581XX Tail Number: NXXGS Model: Hawker 800 ACTT: 7176.6 LNDS: 5068
Engine Position: 1 Engine S/N: P-91363 Engine TSN: 6939.1 Engine Cycles: 4936
Engine Position: 2 Engine S/N: P-91371 Engine TSN: 7121.6 Engine Cycles: 5039
APU APU S/N: 877641 APU TSN: 3066.0 APU CSN: 7769
2. C/W the following Maintenance Schedule Inspection items:
800 Hour “B1-B12” Manufacturer’s routine inspection.
1600 Hour “C1-C12” Manufacturer’s routine inspection.
12 Month “E1-E12” Manufacturer’s routine inspection.
24 Month “F1-F12” Manufacturer’s routine inspection.
48 Month “G” Manufacturer’s routine inspection.
783003, 783004, 783011, 783012, 783015, 783016 -200/400/800/1600 hour Thrust Reverser inspection Nordam TR5000 MM 78-30-00.
3. C/W the following MS Structural inspection requirements:
320032 8 Year/4 Year main landing gear fairing strut NDT. ( NTM 32-10-103)
510002 1000 flights-Front pressure bulkhead. Detail inspect.
510003 12 Year/4 Year flight compartment skin & window structure above windshields NDT. (NTM 53-10-105A)
510005 15-18Year/8 Year center fuselage structure below the floor NLG bay to frame 13 & 16 to 19 NDT. (NTM 53-10-108, 107, 108B & 109)
510006 15-18Year/8 Year structure below escape hatch frames 13 to 14.
510007 15-18Year/8 Year center fuselage structure below the floor frames 8 to 17 NDT. (NTM 53-10-106A)
510008 15-18Year/8 Year center fuselage structure below the floor frames 13 to 16 NDT. (NTM 53-10-108A)
510009 8 Year / 4 Year entry door surround.
510010 15-18Year/8 Year center fuselage structure above the floor inspection and NDT. (NTM 53-10-101, 102, 103A, 104 & 106)
520009 8 Year Escape Hatch-Detailed Inspection -internally and externally.
530001 8 Year / 4 Year skin exterior under the dorsal intake, forward of frame 19.
530002 8 Year/4 Year fuselage skin under wing to fuselage fairings.
530009 15-18Year/8 Year fuselage skin under ventral tank.
530010 15-18Year/8 Year Ventral fuel tank and tank access panels removed IAW AMM 28-10-15
530011 8 Year Left front face of rear pressure bulkhead [frame 19]
530012 8 Year right front face of rear pressure bulkhead [frame 19]
530018 2400 Hours Fuselage skin adjacent to cabin window cutouts.
550002 8 Year horizontal stabilizer front, rear spar, attachment fittings and elevator hinge brackets inspection. Applied CPC IAW AMM 55-13-00.
550003 15-18Year/8 Year vertical stabilizer detailed inspection. (NTM 55-30-101, 102 & 103)
550004 16-8 Year horizontal to vertical stabilizer attachments.
550005 24 Year / 8 Year horizontal stabilizer bond test. (NTM 55-10-104A)
550006 8 Year/4 Year elevators NDT. (NTM 55-20-101 & 102)
550007 4 Year elevator detailed inspection.
550008 4 Year elevator trim tabs connecting rods.
550009 4 Year rudder detailed inspection.
550010 4 Year rudder trim tab, servo tab connecting rods.
550011 8/4 Year rudder NDT. (NTM 55-40-101)
550012 15-18Year/8 Year horizontal stabilizer NDT. (NTM 55-10-101, 102, 103 & 105)
550014 8 Year rudder hinge brackets and attachments.
550015 2 Year elevator mass balance weights & spigots.
570007 8 Year/4 Year wing bottom skins and stringers inspection and NDT. (NTM 57-30-101)
570008 8 Year/4 Year main landing gear and sidestay attachment fittings.
570011 3900 Hour/8 Year wing front spar, forward face. Ref. Aviation Partners, Inc. ICA
570012 2300 Hour/4 Year wing rear spar rear face. Ref. Aviation Partners, Inc. ICA
570013 2400 Hour/4 Year airbrakes hinges detailed inspection.
570014 2400 Hour/4 Year aileron inspection and NDT. (NTM 57-50-107)
570015 2400 Hour/4 Year aileron detailed inspection.
570016 2400 Hour/4 Year aileron connecting rods, trim and servo tabs.
570017 2400 Hour/4 Year flaps and flap vanes inspection and NDT. (NTM 57-50-105,106)
570028 4 Year Wing Leading Edges
570029 3600 Hour/8 Year wing internal structure / fuel system non return valves in inner and outer wings. Ref. Aviation Partners, Inc. ICA
570030 4800 Hour/8 Year then every 4 Years aileron outboard hinge casting inspect and NDT. (NTM -Ref. API # SRH-09-003)
4. C/W the following MS Out of Phase inspection requirements:
300007 1 Month purge of the airplane ice protection system.
340013 36 Month Compass swing IAW 800 AMM 34-23-14. [Installed new Compass Card as required]
5. Addressed the following Airworthiness Directives and MFG Service Bulletins:
AD 2012-11-09 Amendment 39-17072 “Chemical Oxygen Generators” is not applicable due to units not installed.
AD 2012-17-01 Amendment 39-17164 “Goodyear Tires” is not applicable due to p/n not installed.
Complied with AD 2012-02-08 Amendment 39-16931. Removed and reinstalled modified RT-910 TCAS II computer unit p/n 4066010-913 s/n 92081106,
modified by ACSS Repair and Overhaul CRS# L3ZR029X / EASA 145.5441. MOD STATUS: ACH SB34-66](https://image.slidesharecdn.com/c6e781ee-4a5c-4cb2-9db4-46d52d556bc0-161128225554/85/NXXGS-LOG-330-320.jpg)
![ Complied with SB 32-4068 dated July, 2011 “Nose Landing Gear Dragstay Assembly Design Improvement” [dragstay p/n 258UN3-143A s/n DHL/DH/732]
Reassembled with new roller p/n 140-818020-0001.
Entry Continued on Next Page 1 of 4
Hawker 800A, S/N: 2581XX NXXGS Aircraft Log Book Entry Continued ACTT: 7176.6 Date: 10/22/2012
6. C/W the following MS Life Limited/Component Overhaul requirements and Tasks:
080005-Weighed Aircraft and Updated Flight Manual W&B Info
212015-60M, HP Duct-Overheat switches-Test in accordance with Kiddie Graviner 26-12-70 and Hawker 800 AMM 26-10-12. [2ea] 156D/05 (1)
323009-5000 Landings, Installed an overhauled L/H Main undercarriage Jack p/n AIR48502/7 s/n LK9008460, overhauled by APPH Wichita CRS# OU2R070L /
EASA 145.5895 under W/O# 637984. Removed s/n LK8800820.
323010-5000 Landings, Installed an overhauled R/H Main undercarriage Jack p/n AIR48503/7 s/n LK0655, overhauled by APPH Wichita CRS# OU2R070L / EASA
145.5895 under W/O# 637984.Removed s/n LK8803594.
323011-5000 Landings, Installed an overhauled Nose undercarriage Jack assembly p/n AIR45404/1 s/n LK9302336, overhauled by APPH Wichita CRS# OU2R070L
/ EASA 145.5895 under W/O# 637984.Removed s/n unk.
323015-5000 Landings, Installed an overhauled L/H Main Gear Door Jack p/n AIR48485/3 s/n APB94940, overhauled by APPH Wichita CRS# OU2R070L / EASA
145.5895 under W/O# 636011. Removed s/n LK8800504.
323016-5000 Landings, Installed an overhauled R/H Main Gear Door Jack p/n AIR48484/3 s/n LK0562, overhauled by APPH Wichita CRS# OU2R070L / EASA
145.5895 under W/O# 636010. Removed s/n LK8802336.
334005.1-1500 Hr, Installed new L/H winglet tip strobe light assembly p/n 02-0250276-00.
334005.2-1500 Hr, Installed new R/H winglet tip strobe light assembly p/n 02-0250276-00.
340016-24M, Check static plates and Airframe surrounding structure IAW Hawker 800 AMM 34-11-29.[part of F3]
342561-24M, Inspect Under Upper and Lower TCAS Antenna {ICA Document #44504900}.
351008-6 Year, Overhaul-B/E Aerospace/Puritan Bennett Passenger. Installed 13ea. new passenger Observer/Cabin/Lav oxygen masks p/n C351-2000-205
[DOM: 01/2012]. IAW Hawker 800 AMM 35-20-31.
340001.1, 340002.1-24M Replace NZ-2000’s Battery-IAW Honeywell IM #A09-3642-002.Installed 2ea. new #1 and #2 FMS NZ-2000 batteries p/n 7020116-1. Next
Due: 10/2014.
7. Installations with 337’s
Installed new LoPresti Speed Merchants “Boom Beam” wing mounted Taxi / Landing light System with new LoPresti Speed Merchants “Boom Beam” Nose
mounted HID light System in accordance with LoPresti Speed Merchants “STC STO2893AT” dated June 28, 2004, LoPresti Speed Merchants Installation
Instructions LSM-500-042 Rev T dated 10-26-10, LSM-500-047 Rev K dated 12-9-10 and LoPresti Master Drawing List (MDL) No. 47 Rev. Q dated 05-21-12 or
later FAA approved revision. Ref. FAA form 337 and Additional Equipment list/Weight and balance form dated 10/22/2012 for details.
Landing/Taxi light kit P/N: LSM-500-042-2860
Nose Taxi light kit P/N: LSM-500-047-2860
Installed 2 ea. ECS USB charging outlets located in the cockpit on the respective pilot and copilot side facia panels and related electrical system in accordance
with ECS assembly drawing number ECS-210210 and StandardAero electrical systems drawing number 1023231 rev A. Ref. FAA form 337 and Additional
Equipment list/Weight and balance form dated 10/22/2012 for pertinent details.
8. Performed the following miscellaneous maintenance:
3300002-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45580. Removed s/n 39442.
3300550-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45097. Removed s/n 42063.
3300552-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45112. Removed s/n 42065.
3300560-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45659. Removed s/n 36930.
3300561-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45649. Removed s/n 36929
3300557-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45570. Removed s/n 42067.
3305011-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45107. Removed s/n 5323.
3305011.1-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45113. Removed s/n 35532.
3305013-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45111. Removed s/n 36928.
3350011-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45634. Removed s/n 14909.
Installed new L/H flap outboard hinge bearing retaining ring p/n A50Y.
Installed new NLG axle plate felts p/n 25UN107.
Installed new L/H flap outboard hinge bolt p/n A112-12J.
Installed new L/H and R/H flap inboard hinge bolts p/n A112-15G.
Installed new R/H flap outboard hinge bolt p/n A112-12J.
Installed 2ea. new L/H flap outboard driveshaft Gaitors p/n A9030.
Installed 2ea. new R/H flap outboard driveshaft Gaitors p/n A9030.
Installed new Dorsal fairing bolt p/n DHS1473-10 with nut p/n H51132-3K7.
Installed new manhole panels [W311] seal p/n 25WS619.
Installed 2ea. new L/H aileron cable pulleys p/n AS103.[L/H outboard flap well]
Installed 3ea. new Rudder servo tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y.
Installed 3ea. new Rudder Trim tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y.
Installed new Rudder lower hinge mount bolt p/n 25TE241.
Installed new Rudder servo tab center mount bolt p/n DHS1432-10E.
Installed new Escape Hatch rain seal p/n 25FC7767-3.
Installed new L/H Airbrake outboard upper hinge bolt p/n 25WS4253AB.
Installed new L/H Airbrake outboard Lower hinge bolt p/n 25WS4253AB.
Installed new L/H Airbrake inboard lower hinge bolt p/n A111-12G.
Installed new R/H Airbrake outboard lower hinge bolt p/n 25WS4253AB.](https://image.slidesharecdn.com/c6e781ee-4a5c-4cb2-9db4-46d52d556bc0-161128225554/85/NXXGS-LOG-331-320.jpg)
![ Installed new R/H Airbrake inboard lower hinge bolt p/n A111-12G.
Installed new R/H flap outboard hinge fairing bracket p/n 25-8WS2093-1A.
Installed new R/H Airbrake outboard upper hinge bolt p/n 25WS4253AB.
Installed 2ea. new L/H and R/H swing down panels camlocks p/n 1126000-4
Installed 2ea. new L/H and R/H swing down panel camlocs p/n 2600-5.
Installed 2ea. new L/H and R/H swing down panel camlocs p/n 2600-7.
Installed 4ea. new L/H and R/H swing down panel camlocs p/n 2600-6.
Entry Continued on Next Page 2 of 4
Hawker 800A, S/N: 2581XX NXXGS Aircraft Log Book Entry Continued ACTT: 7176.6 Date: 10/22/2012
Performed the following miscellaneous maintenance Continued:
Installed 10ea. new L/H and R/H swing down panel camlocs lock washers p/n 2600LW.
Installed new NLG, Nose strut barrel p/n 25UN649 s/n WAL42983. Removed s/n UNK.
Installed new NLG, axle retaining nut p/n 25UN119.
Installed 3ea. new R/H elevator Trim tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y.
Installed new R/H elevator center mount bearing hinge mount bolt p/n 25TE241.
Installed new L/H Taxi light circuit breaker p/n MS26574-10.
Installed new R/H aileron, trim tab inboard bearing p/n ZWDSP4SP1-G81.
Installed new R/H aileron, center bearing attach bolt p/n 25-8WG43-1.
Installed new R/H aileron, inboard mount bolt p/n 25-8WG25-1.
Installed new L/H aileron, inboard mount bolt p/n 25-8WG25-1.
Installed new L/H aileron, center bearing attach bolt p/n 25-8WG43-1.
Installed 3ea. new L/H elevator, trim tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y.
Installed new L/H elevator, middle bearing attach bolt p/n 25TE241.
Installed new L/H elevator center mount hinge bolt p/n DHS1473-11-1-2E.
Installed new R/H wheel well hydraulic lines retaining plate p/n 25WS4081.
Installed new Fwd closet, curtain hangar p/n T2.
Installed 9ea. new aircraft static wicks p/n 10-900-53A-2.
Installed new #1 engine LP bleed duct gasket p/n 3071235-1.
Installed new #1 transponder coax [@ rack] right angle connector p/n CTR922.
Installed new R/H [A] horizontal stab.-to-vertical stab. p/n 25-8GF55-1.IAW Hawker 800 SRM 55-10-41.
Installed new L/H [A] horizontal stab.-to-vertical stab. p/n 25-8GF55-1.IAW Hawker 800 SRM 55-10-41.
Installed new R/H [B] horizontal stab.-to-vertical stab. p/n 25-8GF63-1.IAW Hawker 800 SRM 55-10-41.
Installed new L/H [B] horizontal stab.-to-vertical stab. p/n 25-8GF63-1.IAW Hawker 800 SRM 55-10-41.
Installed new R/H [C] horizontal stab.-to-vertical stab. p/n 25-8GF57-1.IAW Hawker 800 SRM 55-10-41.
Installed new L/H [C] horizontal stab.-to-vertical stab. p/n 25-8GFR128-1.IAW Hawker 800 SRM 55-10-41.
Installed new R/H [D] horizontal stab.-to-vertical stab. p/n 25-8GF59-1.IAW Hawker 800 SRM 55-10-41.
Installed new L/H [D] horizontal stab.-to-vertical stab. p/n 25-8GFR129-1.IAW Hawker 800 SRM 55-10-41.
Installed new R/H [E] horizontal stab.-to-vertical stab. p/n 25-8GF61-1.IAW Hawker 800 SRM 55-10-41.
Installed new L/H [E] horizontal stab.-to-vertical stab. p/n 25-8GF61-1.IAW Hawker 800 SRM 55-10-41.
Installed new overfin-to-stinger seals p/n 25-8TF437-265. IAW Hawker 800 SRM 51-43-00.
Adjusted rudder control cable tensions in accordance with Hawker 800 AMM 27-20-00.
Adjusted rudder auto pilot servo cable tensions in accordance with Hawker 800 AMM 27-20-121.
Adjusted airbrake cable tensions in accordance with Hawker 800 AMM 27-61-02.
Adjusted aileron autopilot cable tensions in accordance with Hawker 800 AMM 27-10-93.
Adjusted aileron trim cable tensions in accordance with Hawker 800 AMM 27-10-00.
Adjusted aileron control cable tensions in accordance with Hawker 800 AMM 27-10-00.
Adjusted crossfeed cable tensions in accordance with Hawker 800 AMM 28-20-83.
Adjusted L/H and R/H HP cable tensions in accordance with Hawker 800 AMM 76-10-00.
Adjusted L/H and R/H LP cable tensions in accordance with Hawker 800 AMM 28-20-83.
Adjusted elevator servo cable tensions in accordance with Hawker 800 AMM 27-30-00.
Resealed R/H wing fuel sump using PRC1422B1/2 in accordance with Hawker 800 AMM 20-00-00.
Accomplished crack repair by weld process to the R/H Thrust Reverser stang panel, then prepped, epoxy primered and top coated as required. All work done
IAW AC43.13-1B and Hawker 800 structural repair manual 54-10-31 and Hawker 800 AMM.
Accomplished Repair to R/H MLG strut barrel per Hawker Siddeley Aviation Repair Drawing #: 25UM/R179 “Plunger Tube Main U/C, Lug Removal” dated
2/7/1976.
Adjusted L/H and R/H main landing gear roller clearances in accordance with 800 AMM 32-10-25,401.
Removed light surface corrosion from some areas of the L/H and R/H thrust Reverser afterbody, treated primed and painted IAW Hawker 800 AMM 20-10-3527
and 51-20-11.
Removed and reinstalled L/H boost pump noise suppressor to remove light corrosion as required, then prepped, epoxy primered, applied top top coat-silver. All
work done in accordance with 800 AMM 20-10-228.
Removed light surface corrosion from some areas of the L/H and R/H wing leading edge lands, treated primed and painted IAW Hawker 800 SRM 51-43-00 and
51-73-00.
Accomplished Securing of main entry door guide pin sleeves IAW Hawker 800 AMM 52-11-00.
Accomplished painting of the NLG lower bearing assembly, retaining collar, and torque links, cleaned, treated and epoxy primed then painted [Matterhorn
white] IAW Hawker 800 AMM 20-10-228.](https://image.slidesharecdn.com/c6e781ee-4a5c-4cb2-9db4-46d52d556bc0-161128225554/85/NXXGS-LOG-332-320.jpg)
![ Reglued Escape hatch seal in many area’s as required using 1300L in accordance with 52-20-00.
Resealed nose landing gear strut assembly using the following new parts: 1ea. seal P/N: AIR45598, 1ea. seal P/N: 423000A, 1ea. seal P/N: 25UN523, 2ea. seals
P/N: AIR45596, 2ea. seals P/N: AIR110410 and 1ea. seal P/N: DHS1650C. Serviced nose strut assembly as required. All work done in accordance with Hawker
800 CMM 32-20-30 and Hawker 800 AMM 12-32-00.
Resealed L/H and R/H main landing gear strut assemblies using the following new parts: 4ea. seals P/N: AIR117292, 2ea. seal P/N: AIR46174, 2ea. seal P/N: 25-
6UM31, 2ea. seals P/N: 21UM495-9, 4ea. Delta seals P/N: S30948, 2ea. seal P/N: 100-240-1109, 2ea. seal DHS1650A and 2ea. seal P/N: DHS1650C. Serviced
strut assemblies as required. All work done in accordance with Hawker 800 CMM 32-10-01 and Hawker 800 AMM 12-32-00.
Removed corrosion from outboard L/H horizontal leading edge landing and repaired strap as needed in accordance with Hawker 800 Structural Repair Manual
51-24-11-001,51-25-00-001,51-31-00-001, 51-41-00-001,51-42-00-001,51-43-00-001,51-44-00-001.55-10-11-001 Fig.1,55-10-11-001.
Entry Continued on Next Page 3 of 4
Hawker 800A, S/N: 2581XX NXXGS Aircraft Log Book Entry Continued ACTT: 7176.6 Date: 10/22/2012
Performed the following miscellaneous maintenance Continued:
Accomplished crack Repair to the R/H Flap located inboard aft at trailing edge using flush patch/internal doublers, in accordance with Hawker 800 Structural
Repair Manual “Flap skin Repairs Aft of Spar [pre-Mod. 253297]” 57-55-12-201 Sec.3.with Fig.203.
Accomplished Repair to Cabin center aisle floor stringer @ FR.224 in accordance with Hawker 800 Structural Repair Manual “Fuselage Center Section Center
Structure Repair Schemes” 53-20-11-201 Fig. 203.
X-rays performed by Certified Inspection Service Inc. CRS #X18R997N on project # 18767.
Removed and replaced various hardware, bonding jumpers, lamps, abrasion tape, sealant and paint as needed with new parts in accordance with Hawker 800
AMM. Details on file under StandardAero WO#: 291419.
I certify this Aircraft has been inspected in accordance with a “B, C, E, F & G” inspection
under FAR 91.409 F (3) and approved for return to service. Details under W/O# 291419
Date 10/22/2012 ACTT: 7176.6
Signed Thomas Styczynski for
CRS# GW4R221M, Augusta, GA. 30906 4 of 4
SERVICE RECORD ENTRY
XXX Partners Inc.
Hawker 800 S/N: 2581XX
Work Order Number: 291419 Date: 10/22/2012
ACTT: 7176.6 Ldgs: 5068
Engine Serial Number: P-91363
Position #1
Engine TSN: 6939.1 Engine CSN: 4936
1. 720005-Complied with 150 to 200 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00.
o Analyze oil and filter.
o Inspect chip detector for contamination.
2. 720011-Complied with 300 to 400 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00.
o DEEC Bit Check
o Electrical Wiring Connectors
o Fan Rotor Assembly Blades
o Fuel Heater Oil Tube
o Fuel Nozzle Shrouds
o Plumbing lines and connections
3. 730005-Complied with 600 to 800 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00.
o Fuel Filter Element](https://image.slidesharecdn.com/c6e781ee-4a5c-4cb2-9db4-46d52d556bc0-161128225554/85/NXXGS-LOG-333-320.jpg)
![Augusta, Georgia
Aircraft Logbook Entry
XXX Partners Inc. Work Order: 323954 Date: February 12, 2016
Serial Number: 2581XX [NA04XX] Tail Number: NXXGS Model: Hawker 800A ACTT: 7,767.9 LNDS: 5,513
Engine Position: 1 Engine S/N: P-91363 Engine TSN: 7,530.4 Engine Cycles: 5,381
Engine Position: 2 Engine S/N: P-91371 Engine TSN: 7,712.9 Engine Cycles: 5,484
1. C/W the following Maintenance Schedule Out of Phase Inspection items IAW Hawker 800 AFMS:
210001 400 Hour Cooling Turbine-drain and replenish the oil {Mobil Jet II}, Inspect magnetic detector plug.
210006 400 Hour water separator inspection for satisfactory condition.
340013 - 36 Month, Main and standby compass check swing. IAW Hawker 800A AMM 34-23-14.
2. C/W the following MS Life Limited/Component Overhaul Requirements, and tasks IAW Hawker 800 AFMS:
400 Hour-Strobe light intensity check-Tail strobe.
3. Performed the following miscellaneous maintenance:
Installed new “S8” drain valve insert p/n 25SF2551-1 with new drain screw p/n MS3212-31L. IAW Hawker 800A AMM 34-00-00, 34-11-19-501. [Reference
SB 34-3282].
Installed new “S8” drain body reservoir p/n 25-7SF231. IAW Hawker 800A AMM 34-00-00, 34-11-19-501.
o I certify that the Standby static system was tested and inspected and found to comply with Appendix E of FAR 43.
Installed new upper Fwd ADF antenna p/n 7510300-901 s/n 1412N357. Removed p/n 7510300-901 s/n 04118911 in accordance with Hawker 800A AMM
34-51-05.
Installed new upper Aft ADF antenna p/n 7510300-901 s/n 1507N865. Removed p/n 7510300-901 s/n 88100194 in accordance with Hawker 800A AMM
34-51-05.
Installed Repaired #2 Flux detector p/n 7010133 s/n 97123920 in accordance with Hawker 800A AMM 34-20-15-501. Removed p/n 7010133 s/n
98054125. Unit repaired by Honeywell International under work order 274278 dated Aug 24 2012.
Swapped Compass controller/compensators sides. Controller P/N: 7004545-902 s/n: 88110550 moved to #2 side and S/N: 88110552 moved to #1 side.
All maintenance performed on this aircraft was performed in accordance with the current regulations of the
Federal Aviation Administration and is approved for return to service with respect to the work performed.
Details on file on W/O #: 323954.
Date 02/12/2016 Signed: Chris Mann for
, CRS# GW4R221M, Augusta, Ga. 30906](https://image.slidesharecdn.com/c6e781ee-4a5c-4cb2-9db4-46d52d556bc0-161128225554/85/NXXGS-LOG-411-320.jpg)
NXXGS LOG
- 1. Hawker BAe125-800SP NXXGS In servicedate: 2/21/1989 (née NXXXBA, NXXXX) SN 258XXX (NA04XX) Maintenance Record in Microsoft Word program format This document is a digital supplement to the maintenance logbook and records relevant actions performed on the airframe, engines and avionics installed on this aircraft. Its primary purpose is to provide the operator with the means to quickly access maintenance data pertinent to this aircraft using standard document search techniques; it is also an electronic backup to the paper log records. New logbook pages can be easily generated by filling in the companion document “Mx Log Template.docx” template or by simply copying a recent entry and overwriting with current information as necessary. Log entries dating from 4/23/09 (“Version 2.1”) incorporate a helpful feature (embedded Microsoft Excel object) that automatically calculates the engine times and cycles based on the input of current airframe times/cycles. This document is a work in progress; the history prior to April 2007 is incomplete; as opportunity allows it is updated with older relevant records. Notes added for clarification/research but not in official documents are highlighted in red. Greg Stultz, Maintenance Manager, XX XXX LLC 4/26/2016 NOTE: INFORMATION DETERMINED TO BE SUPERSEDED OR OBSOLETE MAY NOT BE INCLUDED IN THIS DOCUMENT!
- 2. NOMENCLATURE/LOCATION P/N ONS/N ON DATE ON/CYC ON/HRS ON #1 ABEX HYDRAULIC PUMP APO5V-086-03 4202203 42022-03 AH-17680 6/13/2009 #1 AC ALTERNATOR BA02801-1 1304 11/28/2007 #1 AC-801 AHRS AHARS CONTROLLER/REMOTE COMPENSATOR 7004545-902 88110552 1/13/88 # 1 AHARS AH600 7003360-943 99064271 4/4/2012 # 1 AZ-810 ADC 7000700-668 88092843 4/14/2004 #1 DC-550 DISPLAY CONTROLLER 7016986-108 06036287 7/21/2006 #1 Engine 3074600-1 P-91363 12/14/1989 #1 FGC 7003974-732 91123099 6/12/2013 #1 FLUX VALVE FX-600 7010133 1103J876 7/1/2015 #1 FMS CDU CD-800 7004403-902 86090164 6/20/2011 #1 FZ-800 FLIGHT GUIDANCE COMPUTER 7003974-732 91123099 6/12/2013 #1 IC-1080 INTEGRATED AVIONICS COMPUTER 7017000-20704 06097714 4/16/2010 #1 IM-600 CONFIGURATION MODULE 7025973-02401 5113864 2/27/2006 #1 INVERTER, MODEL # SI-1250A 501-1235-01 1702 5/7/1992 #1 Main Battery, RG-390E 40562003 3/2/13 NEW # 1 MFD DU-1080 7023460-02006 06093736 4/19/2007 #1 FMS NZ-2000 NAVIGATION COMPUTER 7018879-03020 98082029 4/16/2010 # 1 PFD DU-1080 7023460-02006 04030977 2/25/2014 #1 RCZ-851 7510700-802 95061573 4/10/08 OH #1 RI-553 REMOTE INSTRUMENT CONTROLLER 7016954-938 06042390 7/21/2006 #1 RMU-850 7012100-806 92030861 4/21/08 OH #1 RNZ-850 NAV 7510100-731 88020121 2/27/2006 # 1 Starter Generator 23080-064 2428 8/17/2010 #2 ABEX HYDRAULIC PUMP APO5V-086-03 4202203 42022-03 AH-17642 4/14/2014 #2 AC Alternator BA02801-1 1860 OH on 12/12/2008 #2 AC-801 AHRS AHARS CONTROLLER/REMOTE COMPENSATOR 7004545-902 88110550 1/13/88 # 2 AHARS AH600 7003360-943 89071429 12/23/2014 #2 AZ-810 ADC 7000700-668 88123056 2/27/2006 #2 B WINDOW NH24016-92 L369711 7/28/08 #2 DC-550 DISPLAY CONTROLLER 7016986-108 03065072 10/31/2014 #2 Engine 3074600-1 P-91371 6/16/1989 #2 FLUX VALVE FX-600 7010133 97123920 2/12/2016 #2 FMS CDU CD-800 7004403-902 88090372 8/21/2015 #2 FZ-800 FLIGHT GUIDANCE COMPUTER 7003974-732 99025228 10/4/2010 #2 IC-1080 INTEGRATED AVIONICS COMPUTER 7017000-20704 06117846 4/16/2010 #2 IM-600 CONFIGURATION MODULE 7025973-02401 5113865 2/27/2006 #2 INVERTER, MODEL # SI-1250A 501-1235-01 1215 4/1/2008 #2 Main Battery RG-390E 40562002 3/2/13 NEW #2 FMS NZ-2000 NAVIGATION COMPUTER 7018879-03030 96091165 4/16/2010 # 2 PFD DU-1080 7023460-02006 06093729 4/19/2007 #2 RCZ-851 7510700-802 880100192 ON 12/09 #2 RMU-850 7012100-806 89010294 2/27/06 #2 RNZ-850 NAV 7510100-731 04037330 7/1/2015 #2 STARTER GENERATOR 23080-064 6949 2/3/12
- 3. #2 VHF commantenna chelton ALT PN: S65-8280-44 VF10-347-2 16-21-IT 2341 #2 WC-870 RADAR CONTROLLER 7008471-804 89100794 5/1/2007 #3 AUX BATT UJ RG-126 40636573 2/25/2014 NEW #4 AUX BATT UK RG-126 40636584 2/25/2014 NEW #5 AUX BATT UL RG-126 40184860 2/25/2014 NEW /VY/ OVER FO B WINDOW 25-8NF2065-1- 1552 DHB307 1/19/88 AFIS DATA LOADER 15655-0201 1403 AIRSHOW 400 VIDEO OU 920050 1387 1/17/2013 APU ASSY 62T-40C8D1 877641 Artex ELT 110-406 1201 12/13/2000 Artex ELT Nav. Interface 453-6500 00570 12/13/2000 BRAKE ASSY # 1 AHA1897 5001DW 7/13/2011 BRAKE ASSY # 2 AHA1897 5006DW 7/13/2011 BRAKE ASSY # 3 AHA1897 ZV109 8/11/08 OH BRAKE ASSY # 4 AHA1897 PA031 1/21/09 Bridging Amp 071-0019-00 1942 CD-850 7513000-902 136 FMS DATA LOADER DL-950 G7226-01 2662 9/2/2015 HF CONTROL HEAD KFS 594 071-1274-01, MOD1 2050 HF POWER AMP ANT/COUPLER 064-1017-02 11724 5/1/07 REPAIRED HF Power Amp Coupler 064-1017-02 11724 5/1/07 REPAIRED HF Receiver Exciter 064-1015-01 26960 HF RECEIVER EXITER 064-1015-01 26960 IRS EMERGENCY BATTERY RG-131 40633504 2/25/2014 NEW IRU LASERREF III HG1075AE03 659 7/29/11 LT MLG UPPER TORQUE LINK PIN 258UM131-11A NSN 3/27/08 Microphone mike sw, fo side C9500-11-15A 1241 5/1/7 ON REPAIRED PILOT EROS O2 MASK MC10-14-124 63721 RH AIRFLOW ANGLE SENSOR 1703-12 1419 12/09 RT-910 TCAS II COMPUTER UNIT 4066010-913 92081106 10/22/2012 VQ / HC921H0467/000 621 VR/UNDER FO WRITING PAD 25-8NF2067-1- 1551 DHB216 1/13/88 VS / ELECTROSTATIC FILTER ND0075-1875 WU-870 RADAR RTA 7012640-922 89020226 8/7/2012
- 4. MOD STATUS BAe 125-800ASerial No: 2581XX 25F017AB 25F540A 25F598 25F697CE 25F731A 25F889B SB 34-3282 STATIC DRAIN INSTALL 25F966A 252707 By Greg Stultz observation: NOT IN RECORDS but capacitor on this AC. Installation of HYDRAULIC capacitor in the pressure line of the left engine driven pump to provide additional fluid capacity for nulling system vibration. 252856 252867AEF SECURITY LOCKS ON HINGED DOORS 252869AB 252872 252854AB 252902 252903 252904 252905 252900 252907 252908 252909 252910 252906 252912 252914ABDEFGHJK 252915A 252916 252911 252918 252919 252920 252922AB 252917 252924 252925 252926 252929 252923 252931 252932 252933 252934A 252930 252936ABCDEFGHJ 252937 252938 252939A 252935 252942 252943A 252944A 252945A 252940 252947A 252950A 252951A 252952A 252946A 252955A 252956A 252957A 252958A 252953A 252960A 252961ABCDEG 252962D 252964A 252959A 252967A 252970ABC 252971A 252972A 252965A 252975A Abex hyd pumps on, ripple suppressor at pump off. 252976A 252977A 252978A 252974ACD 252980A 252981B 252986A 252987A Introduces an Emergency brake pressure reducing valve operating cable of larger diameter. 252979A 252989A 252990ABD 252991A 252992A 252988A 252995B 252996BC 252997A 252998A 252993A 253000A 253001A 253002A 253003A NLG bridge casting pn change. 252999A 253007A Introduction of a “B” Screen mounted flight deck grab handle. 253008A 253010AB 253011A 253005A 253013A Windscreen Panels `B' NH24016- 91 and NH24016-92 with Bus-bars relocated to Lucas Mod.D7599. 253015AB 253017ABC 253018A 253012A 253020AB 253022A 253023A 253024A 253019B 253026A 253026KD 253028A 253029B 253025A 253031AC 253032A 253033A 253034A 253030A 253036A 253037A 253038ABD 253039A 253035ABC 253041A 253042A 253043A 253044A 253040A 253046A Stall detection system, deleted the Autopilot disconnect detector, 1 3rd channel. 253047A 253051AB 253052A 253045AB 253056A 253057A 253059A 253060A 253055A 253062A Hyd sys- Remove stall ident accumulator
- 5. 253063A 253064A 253065A253061AB 253067A 253067AB 253068A 253069A 253066A 253071A 253072A 253073A 253074A 253070ACD flight deck ventilation by the addition of an air shut-off valve to both cabin side wall air ducts 253076A 253077A 253078A 253080A 253075A 253083A 253084A 253085A 253086A 253081A 253088A 253089A 253090ABC 253091A Introduction of Negretti Aviation stall detectors 253087A 253093A 253094A 253095A 253096BCD 253092A 253099A 253100A 253101A 253102A 253097A 253104A 253105A 253106A 253107A 253103A 253112A 253113A 253114A 253115A 253109AB 253119A 253120A 253121A 253125A 253116A 253127A 253128A 253129A 253130AB Hyd sys- replace dolls eye with reservoir pressure gauge 253126A 253132A 253133A 253134A 253136ABDE 253131A 253138A GREASE FITTINGS ON ELEV TRIM JACK 253139A 253140A 253141A 253137A 253142ABD 253143A 253145A 253146A Stall detection system, deleted the Autopilot disconnect detector, 1 3rd channel. 253147A 253148A 253149A 253149D 253149B 253149C Mod.253529C: (Applicable to Pre-Mod.253149C airplanes). A screen window heat, A resistor is installed between terminals 9 and 10 of each screen A thermal controller. The resistors are installed on panel DA-E and improve the compatibility between the panel A thermal controllers and the solid state relay. 253150A 253152A 253155ABC 253157A 253158A 253160ABC 253161A Both A screen window heat temperature datums are lowered by using the temperature uplift relay to connect a resistor in parallel with the temperature sensor, giving a low temperature datum when the airplane is on the ground or in flight with both ENG ANTICE switches OFF. During flight with either ENG ANTICE switch ON the resistor will be disconnected by the temperature uplift relay, leaving the temperature sensor alone to control the temperature datum. The overheat temperature datum is set by the resistors connected in series with the overheat temperature sensors. 253162A 253163A 253165A 253166A 253167A 253168A 253170A Fuel sys-removes 4 nonreturn valves in each wing, stack pipes are atached to the diffuser of both gravity jet pumps. 253171B 253173A 253174A 253169A 253177A 253180ABC Ventral tank refuel valve coupling with nut plates. 253181AB 253182A 253175B the ram air exhaust is ducted to atmosphere through an outlet above the left pylon 253185A 253187A Temp guage, omit batt temp 253189A 253192A 253184A 253194A 253195A 253196A 253197A 253193CD 253198A 253199A 253200ABCEFGHJK 253201B time delay units progressively open the left-hand main air valve and to prevent the right-hand main air valve opening until the left-hand valve is almost fully open. On airplanes fitted with Mod.253201 the control circuit is revised to ensure that the venturi fan will only operate when: · A main air valve is not in the closed position, or · For airplanes with a Garrett APU: the APU air valve is not in the closed position, or · For airplanes with a Turbomach APU: the APU master switch is selected ON. A timing unit makes sure the venturi fan will operate for approximately 20 seconds after the airplane lands. Two check valves isolate the venturi when it is not in use. 253203A introduces HYD suction filter AIR87366/0 with a finer filter element 253208A 253209A 253210A 253215B 253221A 253223AB 253227B 253244A 253256A Fuel Booster pump installation mod 253257A 253223AB 253269A 253284A 253286A 253501 253267B 253524F 253527A 253529ABC "A" screen Solid state "Normal" temp limit relays 253535A 253511A 253538A Wing LE anti-corrosion arrangements SB 57-77 . 253543A 253566G 253596A 253597A 253803ABCD 253815B 253831AB 256956AB 257625 253803ABCD 257634A 257636 257638 257641 257630 257656A 257657A 257658A SB 32-209 Removes brake control valve hyd filter from the return connection. 257659A 257655A 257665B 257666A 257668A Brake heat pack wear indicator 257671AB 257673A 258500GE Pt.A 258605 258922ABCDEFJKLMN 258879AB 258880A 258953 258961 259166A 259167A 259206A 259283ACDE Thrust Reversers on 259404A TURBOMACH T-62 APU INSTALL 259602B 259659A 259758AB 259318A 259839A 259948, SB 24-284-9948A, RELOCATION OF APU/GCU EARTH, DONE 8/25/92 259949A 78-4048 TR accumulator seals 9/15/11 259798A
- 6. Installed STC’s SA2271SW BasicInterior 02/28/89 SA2710SW Removable Jumpseat 02/28/89 SA2722SW Hydraulic Quick Disconnect Panel 02/28/89 SA2824SW Long Range Oxygen System 02/28/89 SA2927SW DeVore Tel-Tail Lights 02/28/89 SA3539SW EFIS Master Switch-Sperry 02/28/89 SA3590SW Software Update to NZ9102 03/12/90 SA3590SW FMZ-800 FMS 03/12/90 SA3590SW Update Nav Computers 03/12/90 SA3644SW Fairchild A100 Cockpit Voice Recorder 02/28/89 SA3810SW Precise Pulse-lite Control Unit 2/28/89 SA3881SW Dual Honeywell Primus II SRZ-850 Integrated Radio System 02/28/89 SA3883SW Landing Gear Override Button 02/28/89 SA4147NM Installed Rosen Sunshade Monorail 03/12/96 SA4320SW Dual Radio master Switch 02/28/89 SA4324SW Outside Toilet Servicing 02/28/89 SA4710SW Solar T62T-40C8D1 APU 02/28/89 SA5799SW Teledyne Angle of Attack 02/28/89 SA5800SW SFENA Standby Horizon 02/28/89 SA5805SW Supplemental Radome Taxi / Landing Lights 02/28/89 SA5807SW Aft Baggage Avionics Rack 02/28/89 SA5808SW Forward Baggage Avionics Rack 02/28/89 SA5814SW HF Coupler Mount 02/28/89 SA5846SW Right Handed Ice Light 02/28/89 SA5936SW Sperry AA-300 02/28/89 SA5937SW Sperry DFZ-800 Digital Flight Control System Phase III 02/28/89 SA5938SW Sperry ADZ-810 Air Data System 02/28/89 SA7377SW Dual Sperry EDZ-817 Electronic Flight Instrument System (EFIS) 03/12/90 SA7377SW Updated Sperry EFIS System 02/28/89 SA7474SW Fuel Crossfeed/Transfer Annunciator Flasher 02/28/89 SA7475SW Instrument Power (26VAC) Monitoring System 02/28/89 SA7516SW Nose Compartment Radio Rack and Access Doors 02/28/89 SA7539SW TAS Heat Monitor Annunicator 02/28/89 SA7851SW Water System 08/25/90 SA298450 Concorde RG-390E Batteries ST00302WI TCAS II 11/01/96 ST00545WI Upgrade FMS 10/15/99 ST00837CH-D Allied Signal MK-VII EGPWS w/o Display 12/13/00 SA298430 Hawker Energy Batteries 09/12/03 9/13 & 14 /88 AFTT CYCLES Transcribed Aircraft Maintenance Log Entry 5.5 3 APPROVED FOR ISSUANCE OF CERTIFICATE OF AIRWORTHINESS FOR EXPORT. MANDATORY AND INSPECTION SB's SATISFIED 24-264 24-267 26-27 26-28 27-143 28-50 29-82 29-83
- 7. 32-201 32-207 32-21632-217 32-219 53-66 57-71-3207A-72-5 75-5 9/19/88 AFTT CYCLES Transcribed Aircraft Maintenance Log Entry 5.5 3 U.S. Standard Airworthiness Certificate, issued 9/19, 1988 2/21/89 AFTT CYCLES Transcribed Aircraft Maintenance Log Entry 16.4 6 U.S. Standard Airworthiness Certificate, issued 9/19, 1988 3/14/89 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 44.3 22 REPLACED AOA FLAP POS TX DESCRIPTION PN ON SN ON SN OFF Potentiometer 5401-976-0 nsn nsn FLAP POS SW 1021422 NSN NSN 3/27/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 66.9 29 CO-PILOT HEADING SELECT SYNCHRO VERY NOISY, REPLACED CP RI-818 CONTROLLER DESCRIPTION PN ON SN ON SN OFF CONTROLLER 7011245-912 88020174 88030236 5/14/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 176.2 67 RADAR SPOKES ON ALL DISPLAYS. REPLACED RADAR UNIT LAV INDIRECT LIGHTS INOP DESCRIPTION PN ON SN ON SN OFF RADAR ? NO PN IN LOG 88100161 88120214 INVERTER P1-156-4B 1300 1662 7/12/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 295.3 118 LIGHTNING SENSOR INOP. REPLACED SENSOR PROCESSOR . REPLACED #2 COM UNIT FOR EVIDENCE OF WATER DAMAGE. #1 FMS ALWAYS DIM, OCCASIONALLY GOES BLACK IN FLT. REPLACED SPEX WARRANTY EXCHANGED FMS CONTROL/DISPLAY UNIT DESCRIPTION PN ON SN ON SN OFF PROCESSOR 7011822-903 8804188 87120121 #2 COM UNIT 7510700-901 88100193 88090177 FMS 7004403-902 86060142 88040355
- 8. 7/26/89 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularity Report 315 124 LH FUEL SOV INOP DESCRIPTION PN ON SN ON SN OFF FUEL SHUT OFF VALVE 3515000/107 FRTR007-AA FRTR022AA 8/14/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 315 124 LH FUEL SOV INOP, REPLACED SAME. CW SB 24-269 INSPECT ELCON CONNECTORS FOR CONDITION CW SB27-151, INSPECTION OF ELEVATOR CABLE AT FRAME #7. DESCRIPTION PN ON SN ON SN OFF FUEL SHUT OFF VALVE 3515000/107 FRTR007-AA FRTR022AA 8/29/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 356.1 143 REPLACED O2 OXYGEN CONTENTS COCKPIT INDICATOR GAUGE. CW SB 27-145, CONTROL COLUMN INTERFERENCE CK BETWEEN GAITOR ATTACHMENT BOLT AND ELECTRICAL CONDUIT, CKS OK. DESCRIPTION PN ON SN ON SN OFF INDICATOR ST10015 617A 627 8/31/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 356.1 143 REPLACED FORWARD OXYGEN CONTENTS INDICATOR WITH REPAIRED UNIT. DESCRIPTION PN ON SN ON SN OFF OXYGEN IND ST 10015 617A 627 9/20/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 388 158 CW AD 89-18-13. APU FLT LIMITATIONS. INSTALLED COPY OF AD NOTE IN FLIGHT MANUAL SUPPLEMENTS, AND INSTALLED PLACARDS ON APU PANEL TO READ OPERATION OF APU DURING FLIGHT PROHIBITED EXCEPT DURING EMERGENCY
- 9. DESCRIPTION PN ONSN ON SN OFF 11/1/89 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 388 158 RESEARCH EMER AD 89-22-16, NA TO SN DEECS INSTALLED CABIN INDIRECT LIGHTS INOP, FOUND CONTROL WIRE LOOSE ON 10 AUX CB, CKS OK DESCRIPTION PN ON SN ON SN OFF 1/3/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 542 223 CW SB 32-223, INSPECT NLG JACK PIVOT RING FOR GREASE NIPPLE INSTL. DESCRIPTION PN ON SN ON SN OFF 1/16/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 560.8 229 REPLACED #1 AUDIO CONTROL PANEL DESCRIPTION PN ON SN ON SN OFF PANEL AV-850 7511000-910 88090171 8809021 1/31/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 571.6 234 REPLACED #1 COM UNIT. DESCRIPTION PN ON SN ON SN OFF RCZ-850 COMM UNIT 7510700-901 89010256 88090177 3/8/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 612 257 REPLACED #1, #2 NAV COMPUTERS, PN OFF 704402-906. REPLACED #1 AND #2 RADIO MANAGEMENT UNITS RMU DESCRIPTION PN ON SN ON SN OFF #1 NZ-920 7004402-905 88120807 88120807 #2 NZ-920 7004402-905 88120804 88120804 #1 RMU-850 7012100-944 88120248 #2 RMU-850 7012100-944 88110285
- 10. 4/9/90 AFTT CYCLES TranscribedExxon Mobil Corp CAMP Report 642.5 269 REPLACED WORN FLAP POSITION INDICATOR. TIME SINCE NEW 18 HRS, 7 CYC, 1 MO DESCRIPTION PN ON SN ON SN OFF FLAP IND 2132-1-11 53029 BG53029 BG46377 4/14/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 653.6 274 REPLACED WX WEATHER RADAR TRANSCEIVER XCVR DESCRIPTION PN ON SN ON SN OFF WU-870 RTA 7012640-902 88080140 88120185 4/23/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 668.5 283 RESEARCHED AD 90-06-13, MODIFY VG 14A, NA. RESEARCHED AD 90-05-09, NA. DESCRIPTION PN ON SN ON SN OFF 6/11/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 746 321 REPLACED #1 ENG LOWER FAN FLAP ACTUATOR ASSY DESCRIPTION PN ON SN ON SN OFF FAN FLAP 5453511-1 091 196 6/15/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 752 323 REPLACED LH & RH MLG TORQ LINK PIVOTS. MOD 3244A NEW BUSHINGS INSTALLED DESCRIPTION PN ON SN ON SN OFF BUSH 25-8UM123-1 7/21/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 793 341 APU ELECTRIC FUEL PUMP BOOST REPLACED DESCRIPTION PN ON SN ON SN OFF PUMP 1500-00-65 0076 0012 7/25/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 800 343
- 11. REPLACED LOWER CABININVERTER DESCRIPTION PN ON SN ON SN OFF INVERTER 18-996 5514 5183 8/1/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 806.9 345 REPLACED #1 RMU DESCRIPTION PN ON SN ON SN OFF RM 850 RMU 7012100-944 88080204 88110248 8/6/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 819 349 REPLACED #1 LH LEFT FUEL PROBE. TSN 807 CSN 345 MO 23 DESCRIPTION PN ON SN ON SN OFF FUEL QTY PROBE 0207KTU1 MOD 2 TU9053 TY110647 9/10/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 853 365 REPLACED #2 AUDIO CONTROL PANEL. CW SB 26-29 FIX INADEQUATE CLEARANCE BETWEEN ELEVATOR CABLE AND EXTINGUISHER PIPE ASSY. INSTALLED CHECKLIST MODULE DESCRIPTION PN ON SN ON SN OFF AV-850 7511000-910 88110215 88060131 MODULE 7990310-130 85100142 8090472 9/26/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 871 380 REPLACED TEMP CONTROL SENSOR DESCRIPTION PN ON SN ON SN OFF SENSOR 548408-1 SERIES 1 089C-1457 117C1396 11/9/90 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 932.7 422 REPLACED LH #1 AC GENERATOR CONTROL UNIT DESCRIPTION PN ON SN ON SN OFF AC GCU CB02701 H1228 H1417 2/6/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1020.1 479
- 12. CKD LEFT ANDRIGHT HAND WING PANELS FOR BOLTS IN FLOATING RIB, FOUND NORMAL OK DESCRIPTION PN ON SN ON SN OFF 2/18/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1033.2 489 REPLACED PULSE LIGHT CONTROL BOX DESCRIPTION PN ON SN ON SN OFF CONTROL UNIT 2400-25-4-4 K00482 S0186 2/19/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1034.6 491 REPLACED RADAR R/T ANTENNA ASSY. RADAR BLUE WX SYMBOL INTERMITTENTLY TURNS AMBER. FAULT CODE IN TEST MODE IS 24 FOR ONE SECOND, AND THEN TURNS TO 13. RADAR APPEARS TO OP NORMALLY. BASIC FAILURE CODE IS 13. DESCRIPTION PN ON SN ON SN OFF RADAR RECEIVER TRANSMITTER 7012640-902 88120185 8808140 3/5/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1038.9 494 CW GARRETT SB 731-79-3043 IMPROVED CLAMPING ARRANGEMENT ON FUEL HEATER FLUID TRANSFER TUBE (OIL LINE). DESCRIPTION PN ON SN ON SN OFF 3/19/91 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1053 503 REPLACED LH MLG OUTBOARD GEAR DOOR DESCRIPTION PN ON SN ON SN OFF DOOR 25-8UD43-115 DHB229 DHB75 4/15/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1066.2 513 HYDRAULIC LEAK UNDER REAR BAY, RESERVOIR EMPTY, REPLACED PRESSURE RELIEF VALVE. DESCRIPTION PN ON SN ON SN OFF PRESS RELIEF VALVE MS28893-6D 11090 11082 4/19/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1077 525 LH MLG RED LIGHT CAME ON WITH AC IN TURN, STAYED ON APPROX 1 MINUTE AND WENT OUT. REPLACED LH MLG DOOR UPLOCK MICROSWITCH DESCRIPTION PN ON SN ON SN OFF SWITCH 1EN-14N119
- 13. 6/21/91 AFTT CYCLES TranscribedExxon Mobil Corporation CAMP Report 1172.3 574 CW SB 21-140 INSPECT PRESSURIZATION CONTROL PIPE FOR CLEARANCE. DESCRIPTION PN ON SN ON SN OFF 6/26/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1172.3 574 REPLACED #1 INTERSTAGE TURBINE TEMP ITT GAUGE . HAD RED BAR THROUGH DIGITAL READOUT. DESCRIPTION PN ON SN ON SN OFF #1 ITT INDICATOR WL718RSA3 AD891 AH867 8/1/91 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1204 586 CW SB 25-66, INSPECTED FOR THIRD CREW SEAT BELT ARRANGEMENT DESCRIPTION PN ON SN ON SN OFF 11/12/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1319.8 656 REPLACED FWD O2 OXYGEN QTY INDICATOR DESCRIPTION PN ON SN ON SN OFF GAUGE 10015 870 758 11/15/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1332.3 662 LH FUEL BOOST PUMP FAILED. INSTALLED DIRECT READING GAGE AT LOW PRESS SW ADAPTER. PUMP PRESS 6-7 PSI, NEW PUMP AT 17 PSI DESCRIPTION PN ON SN ON SN OFF #1 BOOST PUMP 207-C01 1371 2030 11/20/91 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1335.6 664 REPLACED FUEL HEATER CHECK CK VALVE (NO POS NOTED) REPLACED OXYGEN O2 PRESSURE REGULATOR. OH UNIT FROM TEC-AIR SERVICES (FAA published an Advisory Circular 43-16, dated February 1995. In that publication Mr. Fred Stein, Technical Branch Manager (AEA 230), with the Eastern Regional Office pointed out that TEC AIR, in many instances, may have failed to properly overhaul and repair oxygen cylinder assemblies before returning them to service.) DESCRIPTION PN ON SN ON SN OFF CK VALVE (3073942-4 PN INCORRECT PER PART TEARDOWN REPORT ) 3073932-4 7-20404-185 7-20404-122 O2 PRESS REGULATOR WKA29720/1 588 899
- 14. 11/26/91 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularity Report 1337.6 667 REPLACED WX RADAR CONTROLLER DESCRIPTION PN ON SN ON SN OFF FO WX RADAR CNTL 7008471-802 88010332 88070465 LH FLAP JACKSCREW 25-8CW159A/B MEC/DHB/199 MEC/DHB/138 12/11/91 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1351. 674 #1 HYDRAULIC LO LIGHT INOP, REPLACED #1 HYDRAULIC LOW PRESSURE SWITCH DESCRIPTION PN ON SN ON SN OFF #1 HYD LOW PRESS SW HE15185-4SN1 2095 2312TW 1/24/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report SB 49-37 DETERMINED NA , APPLIES TO CHESTER INSTALLED APUs. 2/16/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1410.2 718 WING BOLT OR SOME OTHER COMPONENT IN FORWARD LOWER AREA MAKE LOUD BANGING NOISE IN TURBULENCE AROUND 290 – 310 KTS. SPEED BRAKES WERE NOT USED . NOISE OCCURRED IN DESCENT BETWEEN 17K AND 14K FEET. AC FERRIED TO KC AVIATION DAL FOR MX CKS PER BAe MOD 253165A – FUSELAGE WING ATTACHMENT , FWD JOINT FITTINGS REVISED TO REDUCE POSSIBILITY OF IN FLT CABIN NOISE IN TURBULENCE. CW INTENT OF MOD SB3165A, INSTALLED PARTS PER BAe KIT 25GFR155ELFTKT. KC AVIATION W/O # 0132 DATED 2-19-92 DESCRIPTION PN ON SN ON SN OFF R.I.L 25GF11 2/16/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1413 722 CW BAe MANDATORY SB 24-289, MOD 253267B IAW STEP 8,9,10,11,12,13,47,48,49,50 DESCRIPTION PN ON SN ON SN OFF R.I.L 25GF11 2/27/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1413 722 REPLACED THIRD CHANNEL #3 SYSTEM STALL DETECTOR FOR 1000 FPM STATIC LEAK. CW SB 24-288-3284A, PER INSTRUCTIONS 1,2,4AB,5,6, & 7, INTRODUCTION OF WHITE INDICATOR LABELS TO WINDSHIELD HEAT POWER SUPPLY CB DESCRIPTION PN ON SN ON SN OFF 3RD CHANNEL STAL DETECTOR 10201-01 200 122
- 15. 4/1/92 AFTT CYCLES TranscribedExxon Mobil Corporation CAMP Report 1444.7 743 UPGRADED MOBILE RADIO TELEPHONE TRANSCEIVER WITH VOICE PRIVACY NODE, PART HAS 1448 HRS, 737 CYC AND 37 MO SINCE NEW REPLACED LEAKING RT ENG LOWER FAN FLAP ACTUATOR ASSY FOR LEAKING. DESCRIPTION PN ON SN ON SN OFF MOBILE PHONE XCVR RT-18D 400-0125-1000 2156 2156 #2 ENG LOWER FAN FLAP ACTUATOR 5453511-1 303 194 5/7/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity and CAMP Report 1480.5 771 REPLACED #1 INVERTER FOR FAILURE DURING START AND CLIMB OUT. CW SB 53-74, MOD 253193 INSTALLATION OF DRAIN MAST AT REAR BAY EQUIPMENT VENTS. DESCRIPTION PN ON SN ON SN OFF #1 INVERTER, MODEL # SI-1250A 501-1235 1702 1227 6/23/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report NOT APPLICABLE NA SB 22-12, INTRODUCE (COLLINS) FLIGHT CONTROL COMPUTER FCC-86, PN 622- 6195-315, HONEYWELL SYSTEM INSTALLED. 7/14/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1529 809 CW AAI MANDATORY SB 56-10-01 INSP/REPLACEMENT OF CHROME PLATE SCREWS ON A SCREEN WINDOWS, NO CORROSION FOUND. CW BRITISH AEROSPACE MANDATORY SB 29-89-3269A , INTRO OF CHARGING INSTRUCTION LABEL FOR HYD SYS ACCUMULATORS PER INSTRUCTIONS 1-7 DESCRIPTION PN ON SN ON SN OFF 7/23/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1539.4 809 REMOVED 3RD , LONG RANGE, OXYGEN O2 BOTTLES, CAPPED AND STOWED LINES DESCRIPTION PN ON SN ON SN OFF 7/27/92 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1546 832 REPLACED STBY ALTIMETER, INSTALLED LOANER. CW SB 24-292, INSP OF BATTERY ELCON CONNECTOR FOR PRESENCE OF SHIPPING PLUGS, NONE FOUND. DESCRIPTION PN ON SN ON SN OFF
- 16. STBY ALTIMETER WL1605AML 40400-101 153AE576 8/25/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1573 846 CW SB 24-284-9948A, RELOCATION OF APU/GCU EARTH 8/28/92 APU TT APU CYCLES Transcribed Exxon Mobil Corporation CAMP Report 843 1195 REPLACED APU IGNITION EXCITER WITH NEW DESCRIPTION PN ON SN ON SN OFF EXCITER 110418-3 88151518 423 9/17/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1587 858 RIGHT #2 FUEL TEMP SWITCH REPLACED. INSTALLED TSN 1694, CYC 893, 48 MO. ON BAe800 SN NA0420 RH FUEL LOW PRESS SW REPLACED. INSTALLED TSN 1694, CYC 893, 48 MO. ON BAe800 SN NA0420 DESCRIPTION PN ON SN ON SN OFF RH FUEL TEMP SW 60010 0279TW 0281TW RH FUEL LO PRESS SW HTE690014-1 0207 0061 9/28/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report(NOTE TIMES AND CYCLES DISCREPANCY WITH PRIOR RECORDS) 1584 854 REPAIRED #2 HF COM POWER AMP, MOD STATUS 4,6,7. INSTALLED TSN 1035, CYC 629, MOS 32 DESCRIPTION PN ON SN ON SN OFF #2 HF POWER AMP MODEL KAC0952 064-01017-0002 12032 12032 9/30/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report INSTALLED OVERHAULED APU ELECTRONIC SEQUENCE UNIT. UNIT OH’D BY TECHNETICS, INC, 481 CYPRESS LANE, EL CAJON, CA 92020, 805-376-2595. DESCRIPTION PN ON SN ON SN OFF APU ESU CONTROL 161043-700 7584-0018 7584-0092 10/8/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1596 868
- 17. REPLACED #1 AHARS,INSTALLED PART TSN 1279, CYC647, MOS 32 DESCRIPTION PN ON SN ON SN OFF #1 AH-600 AHARS 7003360-943 88121186 88121189 11/3/92 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1626.1 894 REPLACED CABIN TEMP INDICATOR. UNIT OHD BY AIR DALLAS INSTRUMENTS, LB36 LOVE FIELD TERMINAL BLDG 8032 AVIATION PLACE, DALLAS TX 75235 CRS VE1R555K. DESCRIPTION PN ON SN ON SN OFF AEROSONIC B1010- 1113 51010-1113 503921 503451 1/19/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1697.1 947 REPLACED LH LANDING LIGHT LENS CW SB 32-229, INSPECTION OF CERTAIN SIDESTAY ASSY WITH POSSIBLE COARSE GRAIN, PN 258UM3- 125A SN DHL/DH/1467 NOT LISTED IN SB 32-229 TABLE, NO FURTHER ACTION RQD. DESCRIPTION PN ON SN ON SN OFF LH LANDING LIGHT LENSE 25W5333A NSN NSN 5/13/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1814 1038 LEAK CK OF APU NON RETURN VALVE AFTER CHANGE OK. CW FIRE FIGHTING LTD SB 26-108, BAe SB 26-34-3535A, INTRODUCTION OF PORTABLE FIRE EXTINGUISHER PN BA51015-3 WITH STRONGER OPERATING TRIGGER, SB 26-108 STEPS 3A, B STEP 1 AND 2 A,B,C,D,E,F AND G, (BAe SB 26-34) DESCRIPTION PN ON SN ON SN OFF no information 5/19/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1821 1044 CW SB 32-230-3511A, INSTALLATION OF NEW TORQUE LINK PINS WITH THICKER WALL AND IMPROVED GREASE RETENTION. REPLACED #1 PILOTS AUDIO PANEL FOR WEAK INTERCOM DESCRIPTION PN ON SN ON SN OFF #1 LH AUDIO PANEL 7511000-910 88020114 88110217 5/24/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 1822.6 1046 REPLACED #2 HF CONTROL HEAD. DESCRIPTION PN ON SN ON SN OFF HF 071-1274-01 2050 NO INFO
- 18. 6/15/93 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularity Report 1770.5 1072 ADJUSTED MIC LEVEL OF #2 FO CO-PILOTS AUDIO PANEL DESCRIPTION PN ON SN ON SN OFF #2 RH AUDIO PANEL 7511000-910 88100192 6/17/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report REPLACED STEERING SYSTEM RELIEF VALVE TO FIX HIGH PITCH SQUEAL HEARD IN STEERING SYSTEM WHEN TURNED LT OR RT. DESCRIPTION PN ON SN ON SN OFF RELIEF VALVE AIR48284/1 LK0101 LK8800420 7/26/93 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report DETERMINED SB 25-64 NA, OVEN PN 206B-LH-28/115 NIS DESCRIPTION PN ON SN ON SN OFF RELIEF VALVE AIR48284/1 LK0101 LK8800420 9/14/93 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1933.5 1122 TIME DELAY RELAY REPLACED. INSTALLED PN HAS HRS CYC, 1133 CYC, 60 MOS (NO LOCATION INFO) DESCRIPTION PN ON SN ON SN OFF TIME DELAY RELAY 5400619-1 017 018 9/30/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 1955 1134 CW MANDATORY SB 24-293-3501. REVISED MOUNTING ARRANGEMENTS FOR BATTERIES AND EMERGENCY CONTACTORS, TIME CHANGE DUE ON ALL PAX DROP DOWN O2 MASKS, REPLACED 1 – 11. DESCRIPTION PN ON SN ON SN OFF OXYGEN MASKS 17455-0 NSN NSN 10/21/93 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 1971.7 1143 REPAIRED FAILED #3 STANDBY STBY INVERTER REPAIRED BY FALCON ACCESSORIES, INC, 7798 BRANIFF, HOUSTON TX 77061 CRS#GP2R854K INCORPORATING SB 111692-014. IRREGULARITIES REPORT THIS DATE SHOWS CW SB 24-308 AND MPT SB 111692-014. DESCRIPTION PN ON SN ON SN OFF STBY INVERTER PC-250 MOD C 4309 11/24/93 AFTT CYCLES
- 19. Transcribed Exxon MobilCorporation Irregularities Report 2011.1 1176 REPLACED RH FUEL FLOW GAUGE WITH SERVICEABLE UNIT, CW AAI SB 49-72-01 ON 11/29/1993. DESCRIPTION PN ON SN ON SN OFF #2 FUEL FLOW INDICATOR 9-328-26 1399 2186 12/12/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2026.9 1194 REPLACED #1 LH FUEL FLOW INDICATOR FOR STICKING INDICATION. DESCRIPTION PN ON SN ON SN OFF FUEL FLOW GAUGE 9-328-26 2186 2191 12/13/93 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2029.5 1143 CW SB 57-77 REV 2 PARAGRAPH (C) (2)(B) INSPECTION OF LANDING LIGHT WINDOW ASSY RECESS TO LEADING EDGE MATING SURFACE, NO CORROSION FOUND. CW SB 30-65 INSPECTION OF WINDSCREEN PANEL A POWER CABLES FOR CHAFING ON FILTER MOUNTING BRACKETS. DESCRIPTION PN ON SN ON SN OFF 1/13/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2042.3 1160 REPLACED CABIN TEMP CONTROLLER FOR TEMP CONTROL INOP IN AUTO MODE. DESCRIPTION PN ON SN ON SN OFF CABIN TEMP CONTROLLER 617452-3 020C-576 038C-480 3/1/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2091.7 1258 FOUND FUEL DISCHARGE FROM APU FUEL DRAINS, FOUND FIRE EXTINGUISHER LINE TO FUEL CONTAINMENT BOX FULL OF FUEL. REMOVED TOP OF FUEL CONTAINMENT BOX AND FOUND BANJO FITTING BOLT LOOSE ON TOP OF FUEL PUMP, TIGHTENED SAME, OPS OK. DESCRIPTION PN ON SN ON SN OFF 3/3/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2093.2 1260 CW SB 21-A150, INSPECTION OF FAN VENTURI MOTOR FOR CLEARANCE. NO DEFECTS FOUND. DESCRIPTION PN ON SN ON SN OFF
- 20. 5/26/94 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularities Report 2191.5 1318 REPLACED AOA ANGLE OF ATTACK INDICATOR WITH SERVICEABLE UNIT FROM N803X. DESCRIPTION PN ON SN ON SN OFF AOA INDICATOR SLZ7681 CL1067B CL1068B 8/23/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2279.9 1368 CW SB 30-55-3529B, INTRODUCTION OF A RESISTOR AT THE MK 22 THERMAL CONTROLLER REPLACED CAPTS O2 MASK WITH OH’D MASK. DESCRIPTION PN ON SN ON SN OFF QUICK DON CREW OXYGEN MASK MC10-14-01 19244 2894 8/29/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2285.6 1371 REPLACED SAT/TAS CURRENT MONITOR TO FIX INOP SAT/TAS HEATER INDICATION SYSTEM INOP DESCRIPTION PN ON SN ON SN OFF CURRENT MONITOR 5201-800 109 558 9/6/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2292 1373 REMOVED AND REINSTALLED ENGINE SYNC AND APR CONTROLLER FOR TS N805X REPLACED WATER SEPARATOR BYPASS VALVE FOR STICKING IN OPEN POSITION. REPAIRED SURFACE RUST ON RH ELEVATOR LEADING EDGE, SOME PITTING NOTED. REMOVED RUST AND BLENDED PITTING TO .005, CHEMICALLY TREATED, PRIMED WITH EPOXY PRIMER AND TOP COATED WITH POLYURETHANE ENAMEL. DESCRIPTION PN ON SN ON SN OFF APR CONTROLLER 2101822-1 17-568 SYNC BOX 2118114-1-2 403-107 18-261 VALVE 171019-5 11-17-62 3-17-88 9/23/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2298.6 1380 CK’D AC FOR HEAVY LANDING PER PART 5 SPECIAL INSP. FLAPS WOULD NOT RETRACT FROM 45 DEGREE POS, FOUND ASYMMETRY NEEDED ADJUSTMENT, OP CKS OK. DESCRIPTION PN ON SN ON SN OFF 11/9/94 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2337.5 1415 CW SB 30-59 INSPECTION OF WINDSCREEN PANEL A FILTER UNITS FOR COMPONENT INTEGRITY IAW STEPS 2 A, B, C, D, ALL UNITS WITHIN ALLOWABLE TOLERANCE ( LESS THAN 280 Mv)
- 21. DESCRIPTION PN ONSN ON SN OFF 2/20/95 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2447 1505 CW SB 55-34, INSP LH AND RH TAIL PLANES FOR PRESENCE OF DRAIN HOLES, CW SB 55-34 IAW 2-B DRAIN HOLES ADD IAW RIC 25TP55. CRACK ORIGINATING FROM BOLT HOLE IN COVER PLATE. REPLACED WITH NEW PART DESCRIPTION PN ON SN ON SN OFF UNK 25W 4057A PN? NSN NSN 5/17/95 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2547 1568 IRS FAILS WHEN SELECTED ON. EYEBALL ON IRU HAS GONE TO YELLOW FROM BLACK. REMOVED AND REPAIRED IRU. UNIT REPAIRED UNDER WO 20007, DATED 5-25-95, BY HONEYWELL INC, 7825 RIDGEPOINT DRIVE, IRVING, TX 75063 CRS# TT1R518K. DESCRIPTION PN ON SN ON SN OFF IRU HG1075AE03 737 6/1/95 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2558 1577 CW SB 26-37-3543A, INTRODUCTION OF ENGINE FIRE BOTTLES WITH VISUAL PRESSURE INDICATION DESCRIPTION PN ON SN ON SN OFF NO INFO 6/5/1995 AFTT CYCLES Transcribed Exxon Mobil Corp SB & Modification Report 2558 1577 SB 78-16 INCORPORATED THIS DATE. 6/12/95 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2576 1589 REPLACED #1 AND #2 VLF/OMEGA RPU’S FOR TS OTHER AC DESCRIPTION PN ON SN ON SN OFF #1 RPU 7004608-901 88040232 90040322 #2 RPU 7004608-901 88040227 88010204 Exxon Corporation
- 22. BAE125-800 s/n: NA04XXNXXXX Aug. 15, 1995 TAT: 2648.7 Landings: 1627 Complied with the following S/B’s: S/B 53-82-3566G, Improved fluid drainage in fuselage. Removed and reinstalled #1 Engine, s/n P-91363, TSN: 2516.9, CSN: 1572; after MPI. Engine sync box PN 2118114-1-2, SN 103-1207 repaired by AlliedSignal and reinstalled. Swapped positions main batteries, installed #1 position SN 240992, #2 position SN 240987. Complied with following Camps Card Items: 291177-Inspect LH engine hydraulic pump splines All maintenance performed on this aircraft/engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to services with respect to the work performed. Garrett Aviation Services 17250 Chanute Road Houston, Texas 77205 Certified Repair Station XB1R606K By_______________________ Ref. to W.O. D52-5537 S4t1e4v9e ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ S/N P-91363 TSN: 2516.9 CSN: 1572 AUG. 5, 1995
- 23. Removed from #1position on BAE125-800, s/n: NA04XX, NXXXX, with a TAT of 2648.7 and 1627 Landings. Complied with all required pre-removal runs and checks I/A/W 731 light maintenance manual and aircraft flight manual. Took S.O.A.P. sample. All maintenance performed on this aircraft/engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to services with respect to the work performed. Garrett Aviation Services 17250 Chanute Road Houston, Texas 77205 Certified Repair Station XB1R606K By_______________________ Ref. to W.O. D52-5537 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ S/N P-91363 TSN: 2516.9 CSN: 1572 AUG. 15, 1995 Reinstalled in #1 position on BAE125-800, s/n: NA04XX, NXXXX, with a TAT of 2648.7 and 1627 Landings. Complied with all required runs and checks I/A/W 731 light maintenance manual and aircraft flight manual. Serviced with Exxon 2380 oil. All maintenance performed on this aircraft/engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to services with respect to the work performed. Garrett Aviation Services 17250 Chanute Road Houston, Texas 77205 Certified Repair Station XB1R606K By_______________________ Ref. to W.O. D52-5537 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
- 24. 9/27/95 AFTT CYCLES TranscribedExxon Mobil Corporation CAMP Report 2681 1655 REMOVED AND CALIBRATED STANDBY AIRSPEED INDICATOR, UNDER WO 77412 DATED 9/27/95 BY UNDERWOOD INSTRUMENT SERVICES INC, 4453 GLENN CURTISS, DALLAS, TX 75248 TEL 800-767-0767 (GOOD TEL # AS OF 6/25/2009) CRS#SN1R486K. DESCRIPTION PN ON SN ON SN OFF STBY AIRSPEED IND WL271AS1 AG 952 1/30/96 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 2802 1759 REMOVED RH FUEL BOOST PUMP PN 2070C01 AND INSTALLED NEW PUMP PURCHASED FROM AVSCO (AAR 877-227-9200) HAWKER SB AND MODIFICATION REPORT FAX RECORD REFLECTS EMBODIMENT OF SB 28-88-3256A. DESCRIPTION PN ON SN ON SN OFF #2 FUEL PUMP 2C40- 2ECH 2C40-2 6AL71 T909 Exxon Corporation BAE125-800 s/n: NA04XX NXXXX Feb. 12, 1996 TAT: 2819.0 Landings: 1768 I certify that the ALTIMETER/ADC/SDC tests and inspections required by FAR 91.411 has been performed in accordance with FAR 43 Appendix E and tested to 50,000 ft. #1 Alt. Make: Honeywell Serial #:87044536 Date Certified: 2-12-96 #2 Alt. Make: Honeywell Serial #:88105217 Date Certified: 2-12-96 #1 ADC: Honeywell Serial #:88112967 Date Certified: 2-12-96 #2 ADC: Honeywell Serial #:89013060 Date Certified: 2-12-96 This certifies that the ATC transponder tests and inspections required by FAR 91.413 were performed and found to comply with FAR 43, Appendix "F". #1 Make: Honeywell Serial #: 89010256 DATE: 2-12-96 #2 Make: Honeywell Serial #: 88070149 DATE: 2-12-96
- 25. All maintenance performedon this aircraft/engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to services with respect to the work performed. Garrett Aviation Services 17250 Chanute Road Houston, Texas 77205 Certified Repair Station XB1R606K By_______________________ Ref. to W.O. 6311 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 2/16/96 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2822.6 1774 AUTO TEMP CONTROL FOR CABIN AIR INOP – OK IN MANUAL MODE. FOUND LOW VOLTAGE COMING OUT OF CABIN TEMP SELECTOR SW. REPLACED SW, CKS OK DESCRIPTION PN ON SN ON SN OFF CABIN TEMP SELECTOR SWITCH 25-6MC415 077C-569 077C567 2/17/96 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2825.5 1776 REPLACED FAILED LH FUEL BOOST PUMP DESCRIPTION PN ON SN ON SN OFF LH #1 FUEL BOOST PUMP 2C40-2 2AL29 259 3/5/96 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 2846.9 1791 REPLACED LH HYD NON RETURN VALVE DESCRIPTION PN ON SN ON SN OFF #1 HYDRAULIC NON- RETURN VALVE AIR87246 LK0095 LK8800138
- 26. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Corporation BAE125-800 s/n:NA04XX NXXXX JULY 15, 1996 TAT: 2998.0 Landings: 1887 CAMP CARD RECORD ONLY: 27.490 AFMS TASKS 276039 LT AIRBRAKE OH & 276063 LH AIRBRAKE JACK EYE – END LIFE LIMIT R&R LT AIRBRAKE JACK AND EYE END. LT AIRBRAKE JACK PN OFF AIR46520-1, SN LK8711925, PN ON AIR46520-1, SNLK0454. PART INSTALLED HAS 0 HOURS AND LANDINGS. LH AIRBRAKE JACK EYE-END PN OFF AIR 22016, NSN, PN ON NOT NOTED, NSN UNREADABLE SIGNATURE, A&P 2207528 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 11/1/96 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 3078 1938 RESEARCHED AD 94-01-04 EFF 2/4/1994 FOUND NA, NO -904 PROCESSOR INSTALLED REPLACED STBY AIRSPEED INDICATOR REPLACED #2 UPPER XPDR ANTENNA DESCRIPTION PN ON SN ON SN OFF SMITH STANDBY AIRSPEED IND WL271A51 AG951 AG952 #1 UPPER TRANSPONDER ANTENNA S65-5366-7L 35878 #2 UPPER TRANSPONDER ANTENNA S65-5366-7L 35879 UPPER TCAS ANTENNA 7514060-902 96025434 LOWER TCAS ANTENNA 7514060-902 96025432 #1 LOWER TRANSPONDER ANTENNA S65-5366-7L 35880 2014, PN 10A1
- 27. #2 LOWER TRANSPONDER ANTENNA S65-5366-7L 358812025, PN 10A1 #1 GPS ANTENNA 26002806-201 1992 #1 GPS ANTENNA 26002806-201 1983 12/9/96 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3104.3 1954 REPLACED N1/N2 SYNC BOX FROM N802X DESCRIPTION PN ON SN ON SN OFF SYNC BOX 2118114-1 84-140 103-107 1/14/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3135 1975 #1 FMS UNIT PERIODICALLY LOSES ALL INPUT SENSORS AND GOES INTO AHRS NAV(ALL VOR, DME,VLF/OMEGA, IRS FAIL. #2 FMS OPERATES NORMALLY. REMOVED AND REPLACED #1 NAV COMPUTER. DESCRIPTION PN ON SN ON SN OFF #1 NAV COMPUTER 7004402-977 88120804 88120807 1/27/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3145.3 1989 TCAS FAILED. REPLACED TCAS II PROCESSOR UNIT WITH ON FROM N802X FOR TROUBLESHOOTING DESCRIPTION PN ON SN ON SN OFF TCAS PROCESSOR 4066010-904 95022286 95122697 2/25/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3171.1 2014 REF PREVIOUS ENTRY (2-24-97) REPLACED CABIN TEMP CONTROLLER DESCRIPTION PN ON SN ON SN OFF CABIN TEMP CONTROLLER 617452-3 068C-486 038C-480 2/27/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3177.7 2016
- 28. REMOVED AND REPLACEDLOWER ANTI-COLLISION LIGHT. REPLACED WITH WHELEN FLASHING UNIT. REPLACED OXYGEN BARMATIC SELECTOR VALVE REPLACED OXYGEN MASTER SUPPLY VALVE REPLACED OXYGEN PRESSURE REGULATOR TO COMPLY WITH SB 35-45 CW SB 35-46 BY INSPECTION OF SYS FOR UNQUALIFIED FLEX HOSES, CKS OK. DESCRIPTION PN ON SN ON SN OFF WHELEN ANTI- COLLISION LIGHT 010790044-03 01024 13910 OXYGEN BAROMETRIC SELECTOR VALVE K38002/1 274 302 OXYGEN MASTER SUPPLY VALVE WKA35831/2 384 794 O2 PRESSURE REG WK29720/1 674 405 3/10/97 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 3179 2017 INSTALLED #1 GPS CONFIGURATION MODULE DESCRIPTION PN ON SN ON SN OFF #1 GPS CONFIG MOD 7014940-903 97011767 3/10/97 Info from 337 form in W&B manual: Dual Honeywell GPS Sensor Units (GPSSU) PN HG2021GD02 were installed as sensors, and the single Honeywell IRS, PN HG1075AE03 was integrated as a LRN Sensor. The systems provide nav and steering data to both pilots and FO flight instruments and the autopilot. Lateral and vertical steering provided for enroute, terminal and approach operation. The systems have operational approval for Oceanic IAW AC 20-130A, and TSO C129 C1/C3 North Atlantic MNPS airspace IAW AC 91-49, Enroute and terminal IAW AC 20-130A, and TSO C129 C1/C3 and Non Precision Approach IAW AC 20-130A, and TSO C129 C1/C3 Duncan Aviation ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 3/18/97 From 337 form this date: Removed existing Grimes upper and lower rotating beacon assys and installed Whelen Flashing Beacon Assy’s PN 01- 0790044-01, SN 01022 and Lower PN 01-0790044-03 SN 01024 IAW Whelen form # 1-11-93/1 steps 1 – 12. Existing wiring used. Possible lamp part numbers are: 34-0226010-91 T28V150W (FB24) LAMP 28V AEROFLASH; FB24V15W ; C17312-1 ; 40- 0003 ; AFB26 ; 040-0003 ; T28 ; 1924 ; RAC17312-1 Upper Beacon Lens (Red) PN 68-4270569-52 Alternate PN, Clear Lens 68-4270569-32 Lower Beacon Lens (Red with drain hole) PN: 68-4270569-53 Alternate PN, Clear Lens (with drain hole) 68-4270569-33 Lens gasket, fuel resistant, PN 38-0270584-01. Mount plate gasket PN 38-0270586-00 Exxon Employee’s : Philip Kingwood AP 40562438, Inspected by James A. McCrosky IA2055636 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
- 29. 3/23/97 AFTT CYCLES TranscribedExxon Mobil Corporation CAMP Report 3193 2028 AD 97-05-03 EFF 3/18/1997 NA, HONEYWELL GPS INSTALLED , PN HG2021GB02 DESCRIPTION PN ON SN ON SN OFF 6/16/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3311.5 2108 RT ENG INSTRUMENTS CONSTANTLY FLUCTUATE. N1: 99.6+/- .2, ITT 880 +/- 2, FF 890+/- 15. LT ENG STEADY. CK ENG PTT2 SENSOR RESISTANCE(OK), SWAPPED PTT2 INLET SENSOR FOR TS, DRAINED P2 SENSOR LINES, CKD FUEL CONTROL ELECTRICAL RESISTANCE(OK), GRD CKS OK DESCRIPTION PN ON SN ON SN OFF 6/18/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3318 2104 RT SIDE SCREEN OVERHEAT WARNING. CYCLED LT SCREEN HEAT SW, LIGHT OUT BUT BACK ON AFTER SEVERAL MINUTES. SIDESCREEN SEEMS TO HAVE A HOT AREA WHERE BUBBLES HAVE FORMED. SWAPPED B SCREEN THERMAL CONTROLLERS, DESCRIPTION PN ON SN ON SN OFF LH CONTROLLER ND0075-2001 L205607 L205611 RH CONTROLLER ND0075-2001 L205611 L205607 6/18/97 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 3318 2104 REPLACED #2 GPS SENSOR. UNIT REPAIRED AT HONEYWELL , NORTHWEST SUPPORT CENTER, 4150 LIND AVE SW, RENTON, WA 98055 CRS# RN3R821L UNDER WO 228935 DATED 6-13-97 TSN 116 H, 73C, 3 MO DESCRIPTION PN ON SN ON SN OFF #2 GNSSU HG2021GD02 97022263 96081747 6/24/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3324.9 2107 REPLACED RH SIDE B SCREEN FOR OH DESCRIPTION PN ON SN ON SN OFF RH B SCREEN NH24016-92 L292142M L160004 7/2/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3324.9 2107
- 30. INSTALLED PULSE LIGHTNOISE FILTER PER APPROVED 337. DESCRIPTION PN ON SN ON SN OFF NOISE FILTER 05000 CL0030 - 7/11/97 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report AT 2006 HRS AND 2816 CYC (APU) FUEL PUMP REPLACED. INSTALLED PART HAS 854 H, 1080 CYC, 36 MO. DESCRIPTION PN ON SN ON SN OFF APU FUEL PUMP 4950037 2873-0835 PER TRANSCRIPTION 2873-0835 7/24/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3350.5 2119 REMOVED LOANER #1 GPS SENSOR AND INSTALLED REPAIRED ORIGINAL EQUIP GPS SENSOR DESCRIPTION PN ON SN ON SN OFF #1 GNSSU HG2021GD02 97022264 94100526 T.F.E.731-5R-1H P-91363 T.S.N. 3224.0 C.S.N. 2068 # 1 POSITION 8-6-97 EXXON CORP. BAE-800 NXXXX S/N NAO421 ACTT. 3362.8 LDGS. 2124 Complied with data logger diagnostic engine run , margins are 132 deg. F. & 331 N2 R.P.M. All maintenance performed on this A/C/engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details see w/o 37978 on file at this agency. Garrett Aviation Services 17250 Chanute Road Houston, Texas 77205 FAA approved Repair Station: XB1R6006K By KEN MILLER / _____________________________________ 8/14/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3366.9 2130 CABIN ALT INCREASE 300 TO 400 FPM WITH THROTTLE RETARDED IN DESCENT. LH HP/LP MIXER VALVE INOP. REPLACED MIX VALVE, CKS OK DESCRIPTION PN ON SN ON SN OFF
- 31. #1 HP/LP MIXING VALVE 3213788-1P-116 1036 Exxon Corporation BAE125-800 S/N: NA04XX NXXXX August 25, 1997 TAT: _______ Landings: __________ I certify that the ALTIMETER/ADC/SDC tests and inspections required by FAR 91.411 has been performed in accordance with FAR 43 Appendix E and AC 43.203 B tested to 50,000 ft. #1 Alt. Mfg: Honeywell P/N 4016341-906 S/N:87044536 Date: Certified: 8-25-97 #2 Alt. Mfg: Honeywell P/N 4016341-906 S/N: 91126839 Date: Certified :8-25-97 #1 ADC: Mfg Sperry P/N 700070-968 S/N:88112967 Date: Certified: 8-25-97 #2 ADC: Mfg Sperry P/N 700070-968 S/N:89013060 Date: Certified: 8-25-97 STBY ALT Mfg KOLLSMAN P/N WL1605 AM2 S/N: AE576 Date: Certified 8-25-97 All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to services with respect to the work performed. For details see work order 38781 on file at this agency. Garrett Aviation Services Certified Repair Station XB1R606K 17250 Chanute Road Houston, Texas 77205 By__________________________ 9/8/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3389.1 2144 INSTALLED IN LINE FUSES FOR GALLEY AND LAV INDIRECT LIGHTING. DESCRIPTION PN ON SN ON SN OFF AL5328 8/14/97 AFTT CYCLES
- 32. Transcribed Exxon MobilCorporation CAMP Report AD 97-18-03 EFF 9/22/1997 NA. OXYGEN MASK CONE AND SEAL NOT INSTALLED THIS AC. DESCRIPTION PN ON SN ON SN OFF #1 HP/LP MIXING VALVE 3213788-1 P-116 1036 9/30/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3121 2158 INSTALLED MODEL 900 DATA LOADER REPLACED FWD AND AFT APU FIRE BOTTLE EXTINGUISHER CARTRIDGES FOR TIME. DESCRIPTION PN ON SN ON SN OFF FMS DATA LOADER DL-900 7016600-901 97091047 87090253 APU FIRE EXTINGUISHER CARTRIDGES 13083-5 08-97 08-93 11/17/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3465 2190 REPLACED LEAKING LH HYD ON/OFF VALVE. REPLACED THRUST REVERSER DOOR LINK ARMS DID NOT PASS THICKNESS TEST (BELOW .080) DESCRIPTION PN ON SN ON PN OFF (8 EA.) TR DOOR ARM 543003-19 NSN 54530033-7 HYDRAULIC AUX HAND PUMP ASSY AIR45424/0 LK0520 LK8709838 EXXON CORP. BAe125-800 S/N 0421 NXXXX 12-04-97 TAT 3465.0 / Total Landings 2190 Removed and re-installed engine S/N P-91371 TSN 3464.6 CSN 2187, No.1 position following a Major Periodic Inspection. Completed all required post installation/inspection tests, checks, adjustments, and engine runs IAW TFE 731-3 Maint. Manual. Performed a minor sheet metal repair to the No.2 engine bypass duct top and bottom island fairings IAW Dee Howard Co. Fax dated 11/25/97 ref. # CS-001-J97. Performed weld repair of cracks in right flap outboard hinge fairing, blended weld flush, sanded and repainted fairing. Replaced a defective nutplate in No.2 engine bypass side panel. Removed No.2 engine Starter/Generator P/N 23080-005 S/N 4547 and installed an overhauled unit P/N 23080-005 S/N 6130. A 1200 hour ultrasonic inspection of left and right thrust reverser rod links, 8 ea. was performed by Paragon Aerospace Services, Inc. CRS # TH2R187L. Seven failed inspection. Customer installed new rods. Old rods were returned to customer.
- 33. Accomplished the followingCAMPs Items: 243002 = Right Starter/Generator. 291178 = Inspected right engine hydraulic pump splines. 761006 = Lubricate right engine teleflex cable. All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. GARRETT AVIATION SERVICES 17250 CHANUTE ROAD, HOUSTON, TEXAS 77032 CERTIFIED REPAIR STATION XB1R606K By _______________________________________ REF: W. O. No. 43932 & 42631 12-04-97 DOYLE G. LOWRANCE +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 12-04-97 EXXON CORP. BAe125-800 S/N 0421 NXXXX No.2 Engine S/N P-91371 12-04-97 TSN 3464.6 CSN 2187 Complied with AlliedSignal S/B TFE 731-72-3613 = Accomplished an incoming pressure test. Complied with Incoming Data Logger runs IAW TFE 731-5 Light Maint. Manual 72-00-00 Para 15C & D. Complied with incoming Vibration Survey IAW TFE 731-5 Light Maint. Manual 72-00-00 Para 12A & B. Removed and re-installed engine, No.1 position, HS BAe125-800 S/N NA04XX NXXXX TAT 3465.0 and 2190 total landings, following a Major Periodic Inspection. Completed all required post installation/inspection tests, checks, adjustments, and engine runs IAW TFE 731-3 Maint. Manual. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. GARRETT AVIATION SERVICES
- 34. 17250 CHANUTE ROAD,HOUSTON, TEXAS 77032 CERTIFIED REPAIR STATION XB1R606K By _______________________________________ REF: W. O. No. 43932 & 42631 DOYLE G. LOWRANCE 12/5/97 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3465 2190 REPLACED LEAKING LH HYD ON/OFF VALVE. DESCRIPTION PN ON SN ON SN OFF #1 ON OFF VALVE 7907015E FRTR157/F+ 025/AA 4/15/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3594.8 2289 CW MANDATORY SB 26-3002R1, REMOVE APU FUEL CONTROL FIRE EXTINGUISHER PIPE, PER ACCOMPLISHMENT INSTRUCTIONS. DESCRIPTION PN ON SN ON SN OFF 4/23/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3604.7 2293 FLITE PHONES INOP. WHEN SELECTED ON OR DATA THE MSG READS YOUR CALL IS FIRST ONLINE BUT NEVER CONNECTS. RT FOUND BAD, REPLACED BAD RT UNIT. DESCRIPTION PN ON SN ON SN OFF PHONE RT UNIT 153-017712-01 216 637 4/27/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3604.7 2293 REPLACED LH LANDING LIGHT LENS (CRACKED) REPLACED TORN LH FLAP DRIVE BOOT. DESCRIPTION PN ON SN ON SN OFF LH LANDING LIGHT LENS 25-9WS639-1 8001 FLAP DRIVE BOOT COVER A9030 NSN NSN 6/4/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3659.4 2332 CW MANDATORY SB 54-1-3815B R1, FILL PYLON FIREWALL UNUSED TOOLING HOLES ON LH AND RH ENGINE PYLON FIREWALLS. FILLED 7 ADDITIONAL HOLES IN PYLONS 3 ON THE RH AND 4 ON THE LH UNDER PANELS M9L, 10R, M11L, 12R, M13L. DESCRIPTION PN ON SN ON SN OFF
- 35. 6/9/98 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularities Report 3663.2 2334 REPLACED PILOT SIDE LH #1 COOLING FAN BLOWER, FROM ARNONI AVIATION. NEW. DESCRIPTION PN ON SN ON SN OFF BLOWER FAN TBL-2.5 NSN NSN 6/19/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3669 2336 CW SB 32-3015, REVISED NOSE WHEEL AXLE SHIMMING DESCRIPTION PN ON SN ON SN OFF 7/16/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3706.9 2353 REPLACED LAV LIGHTING POWER SUPPLY TO FIX INOP LIGHTS DESCRIPTION PN ON SN ON SN OFF POWER SUPPLY AL-5117 2095 608 EXXON BAE125-800A S/N NA04XX NXXXX 08-13-98 TAT: 3724.4 Total Landings 2363 Removed Customer’s engines, S/N P-91363, from the #1 pos. with TSN: 3594.4, CSN: 2307 and engine, S/N P-91371 , TSN: 3724.4 CSN: 2360 from the #2 pos. following Core Inspections. Installed Bank engines, S/N P-97402C from the #1 position at TSN: 1777.1 CSN: 1107 and S/N P-91403C, from the #2 position at TSN: 2801.8, CSN: 1947. Completed all required post installation tests, checks, adjustments, and engine runs IAW TFE 731-5R-1H Light Maintenance Manual and Aircraft’s Flight Manual. All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 59171 on file at this agency. Garrett Aviation Services, FAA Approved Repair Station: XB1R606K 17250 Chanute Road, Houston, Texas 77032 By: _____________________________________
- 36. Steven C. Griesmyer ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ EXXONCORP. BAe125-800 S/N 0421 NXXXX No. 1 Engine S/N P-91363 08-13-98 TSN: 3594.4 CSN: 2307 This engine was removed from Aircraft for a Core Inspection at a TAT: 3724.4 and LDGS.: 2363. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 59395 on file at this agency. Garrett Aviation Services, FAA Approved Repair Station: XB1R606K 17250 Chanute Road, Houston, Texas 77032 By: ________________________________ Steven C. Griesmyer ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ EXXON CORP. BAe125-800 S/N 0421 NXXXX No.2 Engine S/N P-91371 08-13-98 TSN: 3724.4 CSN 2360 This engine was removed from Aircraft for a Core Inspection at a TAT: 3724.4 and LDGS.: 2363. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 59395 on file at this agency.
- 37. Garrett Aviation Services,FAA Approved Repair Station: XB1R606K 17250 Chanute Road, Houston, Texas 77032 By: ________________________________ Steven C. Griesmyer ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Rental Engine TFE731-5R-1H S/N P-97402C 08-13-98 TSN 1777.1 CSN 1107 Installed this engine in the # 1 position BAe125-800A, S/N NA04XX, NXXXX with a TAT: 3724.3 and 2363 total landings. Complied with all required pre-removal runs and checks I/A/W TFE731-5R-1H Mfgs. Light Maintenance Manual. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 59395 on file at this agency. Garrett Aviation Services, FAA Approved Repair Station: XB1R606K 17250 Chanute Road, Houston, Texas 77032 By: _____________________________ Steven C. Griesmyer +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Rental Engine TFE731-5R-1H S/N P-91403 08-13-98 TSN: 2801.8 CSN 1947
- 38. Installed thisengine in the # 2 position BAe125-800A, S/N NA04XX, NXXXX with a TAT: 3724.3 and 2363 total landings. Complied with all required pre-removal runs and checks I/A/W TFE731-5R-1H Mfgs. Light Maintenance Manual . Complied with Vibration survey and Post S.B. 72-3613 Gearbox pressure checks. All checks were within Mfgs. limits. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 59395 on file at this agency. Garrett Aviation Services, FAA Approved Repair Station: XB1R606K 17250 Chanute Road, Houston, Texas 77032 By: _______________________________ Steven C. Griesmyer 9/24/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3744.2 2386 CABIN PRESSURE FLUCTUATES WITH POWER CHANGES. CABIN CLIMBS WHEN POWER IS REDUCED. CABIN RATE FLUCTUATES SLIGHTLY (50 TO 100 FPM) IN STEADY CRUISE FLIGHT. SWAPPED FLOW CONTROL VALVES WITH N803X FOR TS. DESCRIPTION PN ON SN ON SN OFF FLOW CONTROL VALVE 106884-3-1 1078 410
- 39. 9/29/98 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularities Report 3750.9 2388 REPLACED ALL 6 REAR BAY OVERHEAT DETECTORS REPLACED LH AND RH HP AIR DUCT OVERHEAT DETECTORS DESCRIPTION PN ON SN ON SN OFF BAY OVRHT DETECT 150D01-100 NSN NSN LH HP DUCT OH DETECT 156D/05/1 WAS3178 A097 RH HP DUCT OH DETECT 156D/05/1 WASC127 A021 10/6/1998 Eng TT CYCLES Transcribed Engine #1 P-91363 Logbook Entry 3724.4 2360 Transcription from #2 Engine ENTRY BY GARRETT AVIATION SERVICES, HOUSTON, CRS# XB1R606K 150-200 HOUR ROUTINE PERIODIC. 300-400 HOUR ROUTINE PERIODIC. 1200 HOUR ROUTINE PERIODIC. 2100 HOUR MAJOR INSPECTION (MPI) 2100 HOUR PLENUM INSPECTION 4200 HOUR COMPRESSOR ZONE INSPECTION (CZI) 4200 HOUR FAN SUPPORT INSPECTION 4200 HOUR ACCESSORY GEARBOX INSPECTION 10/8/1998 Eng TT CYCLES Transcribed Engine #2 P-91371 Logbook Entry 3594.4 2307 Transcription from #1 Engine ENTRY BY GARRETT AVIATION SERVICES, HOUSTON, CRS# XB1R606K 150-200 HOUR ROUTINE PERIODIC. 300-400 HOUR ROUTINE PERIODIC. 1200 HOUR ROUTINE PERIODIC. 2100 HOUR MAJOR INSPECTION (MPI) 2100 HOUR PLENUM INSPECTION 4200 HOUR COMPRESSOR ZONE INSPECTION (CZI) 4200 HOUR FAN SUPPORT INSPECTION 4200 HOUR ACCESSORY GEARBOX INSPECTION
- 40. EXXON BAE125-800A S/NNA04XX NXXXX 10-20-98 Total time: 3774.0 Total Landings: 2406 Removed No.1 rental engine, TFE731-5, S/N P-97402C, TSN 1826.0, CSN 1151 and No.2 rental engine, TFE731-5, S/N P-91403, TSN 2851.0, CSN 1991. Installed engines No. 1, TFE731-5, S/N P-91363, TSN 3594.4, CSN 2307 and No.2, TFE 731-5, S/N P-91371, TSN 3724.4, CSN 2360. Completed all required post installation tests, checks, adjustments, and engine runs IAW TFE 731-5R-1H Allied-Signal Light Maintenance Manual and Aircraft’s Flight Manual. All maintenance performed on this Aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. For details, see work order 63262 on file at this agency. Garrett Aviation Services CRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: _______________________ Les Berkheiser +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ No. 1 Engine S/N P-91363 10-20-98 TSN: 3594.4 CSN: 2307 Perform magnetic particle inspection of 2 ea. forward engine mounts in accordance with MIL-STD-1949. No Defects noted. Installed in the # 1 position BAe125-800A, S/N NA04XX, NXXXX with a 3774.0 Total Time 2406 total landings. Complied with all required post installation runs and checks I/A/W TFE731-5R-1H Allied-Signal Light maintenance manual and Aircraft’s Flight Manual. Serviced with Exxon 2380 oil. All maintenance performed on this engine was performed in accordance with current
- 41. regulations of theFederal Aviation Administration and is approved for return to service. For details, see work order 63262 on file at this agency. Garrett Aviation Services CRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: _______________________ Les Berkheiser ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ No.2 Engine S/N P-91371 10-20-98 TSN: 3724.4 CSN 2360 Perform magnetic particle inspection of 2 ea. forward engine mounts in accordance with MIL-STD-1949. No Defects noted. Installed in the # 2 position BAe125-800A, S/N NA04XX, NXXXX with a 3774.0 Total Time 2406 total landings. Complied with all required post installation runs and checks I/A/W TFE731-5R-1H Allied-Signal Light maintenance manual and Aircraft’s Flight Manual. Serviced with Exxon 2380 oil. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. For details, see work order 63262 on file at this agency. Garrett Aviation Services CRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: _______________________ Les Berkheiser ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
- 42. EXXON BAE 125-800S/N NAO421 NXXXX No.1 Engine TFE731- 5R-1H, S/N P-97402C 10-20-98 TSN 1826.0 CSN 1151 Removed rental from the No.1 position BAE125-800, S/N NAO421, NXXXX TAT 3774.0 with total landings of 2406. Complied with all required pre-removal runs and checks I/A/W TFE731-5R-1H Manufactures Light Maintenance Manual . Took S.O.A.P. sample. All maintenance performed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. For details, see work order 63262 on file at this agency. Garrett Aviation Services CRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: _______________________ Les Berkheiser ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ EXXON BAE 125-800 S/N NAO421 NXXXX No.2 Engine TFE731-5R-1H S/N P-91403 10-20-98 TSN 2851.0 CSN 1991 Removed rental from the No.2 position BAE125-800, S/N NAO421, NXXXX TAT 3774.0 with total landings of 2406. Complied with all required pre-removal runs and checks I/A/W TFE731-5R-1H Manufactures Light Maintenance Manual .
- 43. Took S.O.A.P.sample. All maintenanceperformed on this engine was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. For details, see work order 63262 on file at this agency. Garrett Aviation Services CRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: _______________________ Les Berkheiser ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ CORRECTED ENTRY EXXON BAE125-800A S/N NA04XX NXXXX 10-20-98 Total time: 3774.0 Total Landings: 2406 Removed No.1 rental engine, TFE731-5, S/N P-97402C, TSN 1826.0, CSN 1151 and No.2 rental engine, TFE731-5, S/N P-91403, TSN 2851.0, CSN 1991. Installed engines No. 1, TFE731-5, S/N P-91363, TSN 3594.4, CSN 2307 and No.2, TFE 731-5, S/N P-91371, TSN 3724.4, CSN 2360. Completed all required post installation tests, checks, adjustments, and engine runs IAW TFE 731-5R-1H Allied-Signal Light Maintenance Manual and Aircraft’s Flight Manual. Complied with the following "Out Of Phase" items: 720008 = Inspect rear cowling, core and nozzle, No.1 & No.2. 720009 = Inspect exhaust nozzle/clamp, No.1 & No.2. Complied with the following "Structural " items: 530017 = NDT mount brackets, No.1 & No.2. Accomplished teleflex lubrication, No.1 & No.2 All maintenance performed on this Aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. For details, see work order 63262 on file at this agency.
- 44. Garrett Aviation ServicesCRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: ___________________________________________ DOYLE G. LOWRANCE 10/30/98 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 3784.5 2416 REPLACED DAMAGED RH LANDING LIGHT LENS DESCRIPTION PN ON SN ON SN OFF RH LANDING LIGHT LENS 25-9WS639-2 NSN NSN 11/12/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3794.1 2424 CW MANDATORY SB 35-3034 INTRODUCE REPLACEMENT OXYGEN O2 FITTINGS IN LIEU OF FITTINGS INCOMPATIBLE WITH THE OXYGEN SYSTEM. CW STEPS 1-19. NOTE STC SA28245W 3RD BOTTLE INSTALLATION BY ARK MOD STEP 5A-F NA. DESCRIPTION PN ON SN ON SN OFF OXYGEN FITTING CONE CAP AS63400B NSN NSN 12/29/98 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report AD 98-25-02, EFF 12//1998 NA, PART NIS RAYTHEON AIRCRAFT RECOMMENDED SB 32-3023, MOD NO. 253800A&B, INTRODUCTION OF “LB” GREASE INSTEAD OF “LE” IN THE SIDESTAY AND UPLOCK SPRING STRUT ON THE MLG AND THE DRAG STAY AND STEERING SPRING STRUT ON THE NLG DEFERRED UNTIL 4000 CYCLES DUE TIME. 12/31/98 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3814.6 2441 RH #2 ENG HYD PUMP SHOWS SIGNS OF LEAKING AT CASE SEAL. REMOVED AND REPLACED RH #2 ENG HYDRAULIC PUMP DESCRIPTION PN ON SN ON SN OFF #2 ENG HYDRAULIC PUMP 42022-02 AH17852 AH-17852 AH18077
- 45. 1/19/99 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularities Report 3829 2454 AIR-CONDITIONING DUCT OVERTEMP SW FAILED BENCH CHECK. REPLACED SW DESCRIPTION PN ON SN ON SN OFF DUCT OVERTEMP SW 21346-5 4743 3622 1/21/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3830.4 2456 SWAPPED CABIN TEMP SENSOR BULB WITH BULB FROM N802X TO TS PROBLEM WITH THAT AC NOT GETTING WARM ENOUGH UNLESS MANUAL TEMP SELECTION USED. DESCRIPTION PN ON SN ON SN OFF CABIN TEMP SENSOR 607148-1-1 048C-6362 117C-6182 2/21/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3879.7 2494 REPLACED INOP MICROWAVE OVEN INVERTER DESCRIPTION PN ON SN ON SN OFF INVERTER SPS-1607 127 173 3/12/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3910 2514 CW SB 32-3135 INTRODUCTION OF IMPROVED TORQUE LINK BUSHINGS IAW STEPS 3A 1-23 DESCRIPTION PN ON SN ON SN OFF BUSH 25-8UM525-1 BUSH 25-8UM527-1 3/26/99 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report RAYTHEON OPTIONAL SB 34-3166 R1, ADC INCREASED ACCURACY (COLLINS) NA, PART NIS. DESCRIPTION PN ON SN ON SN OFF 3/30/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3925.2 2526 #1 FMS DISPLAY IS VERY DIM, REPLACED FMS CDU. DESCRIPTION PN ON SN ON SN OFF #1 FMS CDU 7004403-902 92100390 89030419 4/28/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 3958.7 2556
- 46. CW SB 32-3016R1 REMOVE NOSE WHEEL AND TIRE SPIN BRAKE. REMOVED LH AND RH SPIN BRAKE ASSEMBLIES, UPDATED W&B PATCHED HOLES IN FIBERGLASS AIR DUCT UNDER CO-PILOT FO SEAT. 8/6/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4025.1 2617 #2 FUEL QTY ERRATIC, DRIFTS 200 LBS. FOR TS SWAPPED #7 FUEL PROBES FROM WING TO WING. DESCRIPTION PN ON SN ON SN OFF LH #7 FUEL PROBE 0204KTU/7 TU9888 TU9887 RH #7 FUEL PROBE 0204KTU/7 TU9887 TU9888 8/13/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4030.5 2621 BUS TIE PROTECTION UNIT TRIPS INTERMITTENTLY. REPLACED BUSBAR PROTECTION UNIT . DESCRIPTION PN ON SN ON SN OFF BUS BAR PROTECT UNIT U3626/2 1444 1820 9/10/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4051 2633 REPLACED ELEVATOR TRIM MOTOR WITH PART FROM N803X. DESCRIPTION PN ON SN ON SN OFF ELEV TRIM MOTOR 622-3260-001 40 82 9/15/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4052.2 2635 REPLACED PORTABLE OXYGEN O2 BOTTLE FOR HYDROSTATIC CHECK DESCRIPTION PN ON SN ON SN OFF PORTABLE OXYGEN BOTTLE 176965-SMB 743731 743601 10/15/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4068 2648 REPLACED MAIN DOOR SEAL FOR NOISE. REPLACED WEATHER RADAR UNIT FOR SPOKING AT 10 O’CLOCK POS ONLY, IN BOTH AUTO AND MANUAL TILT AND ON ALL RANGES. REPLACED FLITE PHONE RT FOR ANNUNCIATION “ YOUR CALL IS 1ST IN LINE”. DESCRIPTION PN ON SN ON SN OFF MAIN ENTRY DOOR SEAL 25-9FC3763-1 JO577 NSN WX RADAR UNIT 7012640-922 90030520 88120185 FLITE PHONE RT UNIT 153-017712-01 204 837
- 47. 11/5/99 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularities Report 4084.2 2656 GALLEY LIGHTING DIM. REPLACED WITH TWO NEW LIGHT STICKS DESCRIPTION PN ON SN ON SN OFF GALLEY INCANDESCENT LIGHTING S27C25B28LSLS NSN NSN 11/8/99 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4087.3 2660 REMOVED AND REINSTALLED CABIN PRESSURE CONTROLLER FOR TS N802X. DESCRIPTION PN ON SN ON SN OFF CABIN PRESS CONTR 130530-4 77284 77284 11/5/99 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report CW MANDATORY SB 35-3170, INTRODUCE REPLACEMENT OXYGEN FITTING IN LIEU OF FITTING INCOMPATIBLE WITH THE OXYGEN SYSTEM, SB NA. DESCRIPTION PN ON SN ON SN OFF 12/27/99 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report CW AD 99-23-22 EFF 11/29/1999, AD IS NA. HONEYWELL COMM/XPNDR PN 7500700-802 INSTALLED DESCRIPTION PN ON SN ON SN OFF 01/07/00 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report SB 34-3236 REV 1, YEAR 2000 SOFTWARE ANOMALY INCORPORATED. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 01/6/00 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 4167.7 2726 REPLACED CABIN TRIPLE INDICATOR. PN ON 51010-113 SN 503921 WITH 2617.9 HOURS AND 1844 LDGS, AND 83 HOURS ON UNIT. PN OFF 51010-1114, SN 503466
- 48. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 2/10/00 AFTT CYCLES TranscribedExxon Mobil Corporation Irregularities Report 4130.3 2703 CREW REPORTED UPON DESCENT, THROTTLES BACK, CABIN ALTITUDE CLIMBS 2000 FPM. PERFORMED CABIN LEAK RATE TEST, GOOD AT 47 SEC. PERFORMED HP/LP AIR CK, ALL GOOD. FOUND RH OUTFLOW VALVE HANG UPON CLOSING. R&R RH OUTFLOW VALVE. OP CKS OK. PN ON 103278-13, SN ON 11-692, SN OFF 37-329. ON 2/11/00 HAD GALLEY ICE DRAWER REWELDED AT PINHOLE LEAKS BY GARRETT AVIATION HOUSTON. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 3/06/00 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4155 2722 MAIN BRAKE ACCUMULATOR GAUGE INACCURATE READS 2000 PSI WHEN AT 3000 PSI ACTUAL. PN ON AW-2-17H, SN ON B5176 SN OFF 4385 *++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 06/09/00 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4245.4 2796 NLG DOOR RED WARNING LT NOT ILLUMINATED WITH GEAR DOORS OPEN. FOUND AND REPAIRED BROKEN WIRE JUST AFT OF CANNON PLUG COMING FROM DOOR SW. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ December 07, 2000 FAA form 337 ENTRY by Garret Aviation Services “ Installed access door in ventral tank per Garrett Aviation Drawing# 2647-2 rev(-) sheet 1-2”RH Ventral Tank Access Door Mod” dated 08/14/00 and Report# 2647-2SA rev (-) “Structural Analysis-Inspection hole and cover installation
- 49. Hawker 125.800A airplaneRH side” dated 04/14/00 approved on 8110-3 dated August 15, 2000 by D. D. Shepherd, Jr, DERT-230307-CE Structures.” ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ EXXON BAE125-800A S/N: 2581XX NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 Complied with the following Airworthiness Directives and Service Bulletins: Complied with AD 97-03-07 by replacing the L. & R. Main Gear Pivot Fittings p/n 25-8UM173-1A, I/A/W, S.B.32-233-3597A. Complied with S.B. 32-3391, “Main Landing Gear Actuator Cylinder Head Inspection/NDT.” Complied with S.B. 53-95, Inspection for missing rivets at Frame 19. Installed missing rivets p/n CR3213-5 as per S.B. instructions. Raytheon Mandatory S.B. 24-32-78, “Electrical Power Change of Leland Static Inverter” is not applicable to this aircraft by serial number. Complied with the following Structural Inspections: 530001 4 Years Inspection – Skin Exterior Under The Dorsal Intake, Forward Of Frame 19. 530002 4 Years Inspection Of Fuselage Skin Under Wing- To-Fuselage Fairings. 520008 8 Years X-Ray On Main Entry Door Internal Structure (NTM 52-80-102. 530003 8 Years Inspection Of Wing To Fuselage Attachments Links, Brackets And Bolts. 530009 4 Years Inspection Of Fuselage Skin Cover By The Ventral Fuel Tank. 530010 4 Years Inspection Of The Ventral Fuel Tank, Internal Structure And Fuel System Components. 510003 4 years inspection of flight compartment skin and window structure above windshields. 510009 4 years inspection of entry door – structure at the lower edge of the surround. 530011 4 years inspection of front face of rear pressure bulkhead. 550001 1200 Hours/2 Year Inspection Of Horizontal To Vertical Stabilizer Rear Attachment Fitting. 550006 4 Years X-Ray The Internal Structure Of The Elevators.(NTM 55-20-101 & NTM 55-20-102) 550007 4 Years Inspection of Elevators, bearings, hinge brackets, mass balance weight side plates and mass balance weight spigots. 550008 4 years lubrication of elevator trim tabs and connecting rods. 550009 4 years inspection of rudder bearings for condition and lubrication. 550010 4 years lubrication of rudder trim tab and anti- servo tab. 550011 4 years x-ray rudder internal structure (NTM 55- 40-101). 320032 4 years inspection of main landing gear fairing strut. 570007 4 years x-ray of the wing bottom skins and stringers between the front and rear spars, rib 0 to 1 and between the center spar and rear spar from rib 1 to 4. (NTM 57-30-101) 570008 4 years inspection of landing gear and side stay attachment fittings. 570009 4 years inspection of the wing top skin, L/H and R/H, in the area of the wing fence. 570012 2400 hours/4 years inspection of the wing rear spar, forward face. 570013 2400 hours/4 years inspection of the airbrakes hinges for security. 570014 2400 hours/4 years Ailerons 10X inspection of hinge brackets and x-ray the internal structure. (NTM 57-50-107) 570015 2400 hours/4 years inspection ailerons bearings for condition and lubrication. 570016 2400 hours/4 years lubrication of connecting rods aileron trim and servo tabs.
- 50. 570017 2400 hours/4years x-ray internal structure of the flaps and flap vanes. 570024 4 years inspection of the horn balance weight. PAGE 1 OF 8 EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 24 ELECTRICAL Removed and reinstalled the L. Alternator p/n BA02801-1, s/n 1311 and R. Alternator s/n 1323, following overhaul by outside vendor “Falcon Crest Accessories” CRS# GP2R854K. Replaced defective Contactor p/n LDG150Y4, with overhauled unit s/n 1172 WECO Aerospace” CRS# UQ3R902L. 25 EQUIPMENT AND FURNISHINGS Installed Artex ELT p/n 110-406, s/n 1201, with Nav. Interface p/n 453-6500, s/n 00570, per Raytheon Aircraft Company drawing # 138-23009-1 rev (C), “ ARTEX ELT 110-406- Wiring Diagram, dated 02/05/99 and approved on 8110-3 dated June 08, 2000 by James A Chalsma DERY-710043-SW Systems & Equipment and recorded on 337 dated 12/07/00. Installed ELT Antenna p/n 455-0427, s/n 0206 per the following Raytheon Aircraft Company drawings: 138-440010- 17, rev (B) “ELT Antenna Instl.” Dated 10/12/95, C.O. G94918 rev (IR) “ELT Antenna Instl.” Dated 05/08/00, C.O. G95797 rev (IR) “ELT Antenna Instl.” Dated 05/08/00, 138-360049-1 rev (A) “ELT INSTL” dated 02/11/98, MOD003639-15 rev (A) “ARTEX ELT INSTL” dated 01/18/00, C.O. G95028 rev (IR) “ARTEX ELT INSTL” dated 02/01/00, 800-8378-2,-17 rev (L) “ELT Bracket Instl Tail cone” dated 06/06/85, C.O. G71924 rev (IR) “ELT Bracket Instl Tail cone” dated 04/16/96, C.O. G93700 rev (IR) “ELT Bracket Instl Tail cone” dated 06/18/99, C.O. G94481 rev (IR) “ELT Bracket Instl Tail cone”. Approved on 8110-3 dated June 12, 2000 by Jack W Ligon DERT-710164SW Structural/Systems, Equipment/Administrative and recorded on 337 dated 12/07/00. Performed field repair, in conjunction with ELT Antenna installation. Per Raytheon Aircraft co. Drawing, FR-HK-00762 rev (b) “Field Repair – Replacement supports for ELT Antenna mounts in fuselage Tail cone (ref Kit Drawing 138- 440010)” dated 11-07-00, and FR-HK-00804 rev (a) “Field Repair-Antenna Location Holes in fuselage, Tail cone skin, between Frames 24 & 25 and Intercostals 2 & 3” dated 09-13-00. Approved on 8110-3 dated November 07, 2000 by Mike Johnson DERY-635772-CE Structures and recorded on form 337 dated 12/07/00. PAGE 2 OF 8 EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 25 EQUIPMENT AND FURNISHINGS (Continued from previous page) Replaced the existing coverings on (6ea.) Passenger Seats, and (1ea.) Lavatory Seat, using Matching “Spinneybeck” Sabrina 781, and SAO777 Leather and Graphic Poly-foam 26120. All materials meet FAR 25.853 (a) burn requirements.
- 51. Replaced theInterior Headliner Covering, with new “Ensolite” foam insulation and “Spinneybeck” Arizona 1037 leather covering. All materials meet FAR 25.853 (a) burn requirements. Replaced Passenger Window and Emergency Hatch Panels Coverings, with new Ensolite Foam Insulation and “Spinneybeck”, Arizona 1037 Leather covering. All materials meet FAR 25.853 (a) burn requirements. All materials meet FAR 25.853 (a) burn requirements. Replaced the interior Side Panel Coverings with new “Ensolite” foam insulation and leather to match interior décor. All materials meet FAR 25.853 (a) burn requirements. Replaced all Accent Band Panel Coverings with new “Ensolite Foam”, and “Spinneybeck” Sabrina 777 Leather covering. All materials meet FAR 25.853 (a) burn requirements. Replaced the Rear Pressure Bulkhead panel covering and Valance coverings with new “Ensolite Foam” and leather to match existing patterns and colors. All materials meet FAR 25.853 (a) burn requirements. Replaced the Veneer on Galley “Coffee Canister Close-out “ and existing Cabinetry using White Oak Veneer p/n GAH00323 and applying Flex Polyester Flame resistant Top Coat. Installed “ new replacement “Coffee” “Water” and “Decaf” placards made by outside vendor. Reinstalled interior seat hardware, rails, seat buckles, latches, buttons and plates following re-plating by outside vendor, “High Tech Finishing”. Re-webbed all seat belts as required accomplished by outside vendor “Aircraft Belts Inc.”. Replaced worn Grospoint covering p/n GPFR0091 and Taupe GPFR0091 (#91), in the Forward and Aft Cabin Baggage Compartments and Lavatory Storage Areas. All materials meet FAR 25.853 (a) burn requirements. Recovered the Main Entry Door Handrail with Sabrina 781 Leather. All materials meet FAR 25.853 (a) burn requirements. PAGE 3 OF 8 EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 Recovered the Main Entry Door Steps using Burl Structure Flooring No.20 Brown, D/L45972/81199. All materials meet FAR 25.853 (a) burn requirements. Replaced Stereo System “Subwoofers” p/n C6508, with new units s/n 109060500-037 and s/n 109300600-044. Investigated report that the Cabin Speaker System would not come on. Found problem to be an improperly wired switch. Corrected wiring to switch and system worked normally. Replaced defective “Lavatory Call” Switch p/n 90E. 27 FLIGHT CONTROLS Replaced the L. & R. Aileron Bellcranks p/n 25-8CW23-1A & 25-8CW23-2A. Replaced the R. Aileron Bearings (2ea.) p/n SL4421-05 and Spacers p/n 258CW23-2A. Treated minor corrosion found in the R. Aileron Balance Weight area, replacing angle p/n S25-8WG-121-2, p/n S25- 8WG-123-4, p/n S25-8WG-127-4, priming and painting as required. Replaced the L. Aileron p/n. 25-8WG1/117, s/n DHB159 with new Aileron p/n 25-8WG111-61A, s/n DHB1045. Removed the Trim Tab from Aileron s/n DHB159 and installed it on the new Aileron s/n DHB1045. Reinstalled the L. & R. Aileron Tips following treatment for minor corrosion and repainting. Reinstalled the L.& R. Elevator Mass Balance weights following treatment for corrosion and replaced the Balance Weight Spigots p/n 257E157. Replaced the R. Aileron Idler Bushing p/n 25-8CWT1-1. Replaced the R. Aileron Outboard and Center Attach Bolts p/n SL4018-524-47, 25WG175-1 and 25WG45-3. Replaced the L Aileron Attach Bolts p/n’s 258WG175-1, (2ea.) 25-8WG-179-1, 25-8WG45-3 and 25-8WG-505-1. Treated minor corrosion on the L. Elevator Inbd. Spar Cap and repainted to aircraft color scheme. Replaced the L. Aileron Inbd. and Outbd. Trim Pulleys p/n AS103I557.
- 52. PAGE 4 OF8 EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 Replaced the L.& R. Elevator Outbd. Bearings p/n N8867 and retaining ring p/n A31Y. Replaced the R. Elevator Trim Jack Rod Bearing p/n CM4L-6E. Replaced the R. Airbrake Attach bolts (2ea.) p/n 25WS4253AB, (1ea.) p/n 25WB297A111-12G (2 ea.) p/n 25WS117 and (1ea.) p/n 25WS1117. Replaced the R. Inbd. Flap Hinge Bolts p/n DHS1432-15GG and p/n A112-12J. Replaced the L. Flap Attach Bolts p/n DHS1432-15GG and p/n A112-12J. Replaced the L. Airbrake Attach Bolts p/n A111-12G, (2ea.)2SWS42S3AB (2ea.)and 2SWB297. Replaced R. Airbrake hardware Thrust Washers p/n Du07 and Nut p/n AIR111076. Replaced the R. Airbrake Jack Supply Line Adapter p/n AS8592A. 28 FUEL Removed and reinstalled the Ventral Tank to correct fuel leak at bolt on the R/H Transfer Pipe Flange Housing. No leaks noted after re-torquing and sealing of bolt. Installed a R/H Access Panel on the Ventral Tank per Drwg. #2647-2 , approved by FAA 8110-3 form and recorded on 337 dated 12/07/00. VENTRAL TANK ACCESS DOOR MOD Replaced the L. & R. surge Tank Seals p/n’s 25-8WS1023-1 and 25-8WS1023-2. (nr/032) Replaced (3ea.)Man Hole Cover Seals p/n 25WS219. 32 LANDING GEAR Removed the L. & R. Main Gear Jacks p/n AIR48503-4, s/n’s 8800820 & 8303594. Complied with the Inspection I/A/W S.B. 32-3391 dated 8/2000. Reinstalled the R. Main Gear Jack with no defects noted. Reinstalled the L. Main Gear Jack, following repairs by outside vendor, “Arnoni” CRS# Y8AR872N. Reinstalled the L. & R. Landing Gear Side stays following replacement of Jack Pivot Assy. p/n 25-8UM87-1A with new p/n 25-8UM173-1A in accordance with S.B 32-233-3597A dated 8/95. PAGE 5 OF 8 (corrected entry 12-28-00 – by S.D.) EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 Installed new Jack Actuator Bushings p/n ARD2922, Right Main Landing Gear Door Strut failed NDI. Removed corroded pins and installed (6ea.) new replacement pins p/n DHS1293-6-90. Painted with primer and JetGlow #570-521. 34 NAVIGATION Removed and reinstalled Gyro p/n H341AGM-1, s/n 5689 following repairs by outside vendor “Executive Instruments, Inc. CRS#XN1R618K. Installed AFIS Antenna p/n 16040, N/S/N, per Garrett Aviation Services drawing # 43-2103-001 rev (-) “INSTL AFIS Antenna” sheet 1-5 dated August 02/2000 and Garrett Aviation Report # 43-2103-001-2581XXSA “ Structural Analysis Instl.-AFIS Antenna” dated November 15, 2000. Approved on 8110-3 dated November 15, 2000 by Parag Merchant, DERY-510250-SW Structures and recorded on 337 dated 12/07/00. Installed AFIS DMU p/n 400-045500-0210, s/n 2707, per Garrett Aviation Drawing # 43-2103-002 rev (b) “ INSTL-AFIS DMU” sheet 1-6, dated November 03, 2000 and Garrett Aviation report # 43-2103-002-2581XXSA rev (-) “Structural
- 53. Analysis INSTL-AFIS DMU”dated November 03, 2000. Approved on 8110-3 dated November 03, 2000 by Parag Merchant, DERY-510250-SW Structures and recorded on 337 dated 12/07/00. Installed AFIS DTU p/n 15655-0201, s/n 1403 in association with the above AFIS equipment. Pilot’s EFIS displays “Att 4” when it should be “Att 3”. Corrected programming pins on the Pilot’s Symbol Generator. Ops checked okay following pin corrections. Removed and reinstalled SG-818 (2ea.) SYM Generator’s p/n 7011674-118, s/n’s 89060399 and 88080266, and (1ea.) Multi-Function Generator p/n 7011674-118, s/n 91110450, following upgrading by Honeywell, to p/n 7011674-119 and 7011675-119. Removed and reinstalled Standby Altimeter p/n WL1605AM2, s/n AE576, following overhaul by outside vendor “Underwood” CRS# SN1R486K. PAGE 6 OF 8 (corrected entry 12-28-00 – by S.D.) EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 Installed Allied Signal Avionics MK-VII, Enhanced Ground Proximity Warning System EGPWS W/O Display, consisting of “EGPWS Computer” p/n 965-1076-001-206-206, s/n 2069, Annunciator Diode Box p/n 43-4129-003-1, s/n 100 and MFD Relay Box p/n 43-4139-001-2, s/n 101. The installation was accomplished I/A/W Garrett Aviation Services Drawing List DL837, dated April 22, 1998, no revision. Under Garrett Aviation Services STC ST00837CH-D dated May 06, 1999 and recorded on form 337 date 12/07/00. 38 WATER Replaced the Lavatory Water Heater Sockets p/n 2091104, Pin p/n 31F1021, Receptacle Connector p/n 48F1141, and Plug Connector p/n 31F1021. 52 DOORS Removed and reinstalled Tensator Motor following replacement of Door Cable Pulley p/n 25FC6811 and Bearings (2ea.) p/n T10E and retaining ring p/n A67Y. Complied with R. Ventral Tank Access Door Mod. In accordance with Drawing #2647-2. 53 FUSELAGE Replaced Chin Strap to Leading Edge seal p/n J4062X6FT. Replaced Dump Chute Hose p/n CD4x13x1.5. Removed and reinstalled the Dump Chute Base Plate following treatment for corrosion and painting. Repaired corrosion of Fuselage Skin, under the Ventral Tank, by installing doubler using 2014T6.040 I/A/W Structural Repair Manual 53-30-12. Replaced (4 ea.)cable guard under the Cockpit Step using 2024 T-3. Replaced the L. & R. Manhole Cover Seals (6ea.) p/n 25WS619. Replaced the Aft Ventral Seal p/n J3073X10FT. (nr/022) Replaced the Chinstrap to Fuselage Seal p/n J3073X10FT. Repaired minor crack in the Hydraulic Tunnel by fiber glass cloth and 6367 adhesive. PAGE 7 OF 8 EXXON BAE125-800A S/N: 28128 NXXXX
- 54. December 13, 2000TAT: 4402.6 Total Landings 2903 57 WINGS Replaced Wing Fillet Seals p/n J3081X9FT, per customer request. Replaced the R & L Wing Link Bolts (2ea.) p/n 25-8WS3005-1. This certifies that an “E1, E2, F1, F2, Inspections and “G” (48 Month Inspection), was complied with in accordance with Hawker 800 Flexible manufacturer’s approved program required by FAR91.409(f)(3) and found to be in airworthy condition. Complied with Post / Pre-Flight Inspections in accordance with the HS800 Flexible Maintenance Schedule. All maintenance performed on this Aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 93444, 93446, 93447 & 110451, on file at this agency. GARRETT AVIATION SERVICES, CRS # XB1R606K 1-800-877-5411 1725z0 Chanute Road Houston, Texas 77032 By: _______________________________________ Steven C. Griesmyer PAGE 8 OF 8 EXXON BAE125-800A S/N: 28128 NXXXX December 13, 2000 TAT: 4402.6 Total Landings 2903 57 WINGS Replaced Wing Fillet Seals p/n J3081X9FT, per customer request. Replaced the R & L Wing Link Bolts (2ea.) p/n 25-8WS3005-1. This certifies that an “E3, E4,F2, Inspections and “G” (48 Month Inspection), was complied with in accordance with Hawker 800 Flexible manufacturer’s approved program required by FAR91.409(f)(3) and found to be in airworthy condition. Complied with Post / Pre-Flight Inspections in accordance with the HS800 Flexible Maintenance Schedule. All maintenance performed on this Aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 93444, 93446, 93447 & 110451, on file at this agency. GARRETT AVIATION SERVICES, CRS # XB1R606K 1-800-877-5411 1725z0 Chanute Road Houston, Texas 77032
- 55. By: _______________________________________ Samuel Davenport(corrected entry 12-28-00) PAGE 8 OF 8 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++ APU Model T62T-40C8D1 P/N: 165101-200 S/N: 897611 December 13, 2000 Hr. Meter: 2925.0 Cycles: 4332 49 APU Accomplished an annual inspection in accordance with the Manufacturer’s Maintenance Manual inspection guide 49-20-00, SB-T-62T-49-77 rev. 8 dated 5/18/99. Inspected the Igniter and ops checked in accordance with the M.M. procedures. No discrepancies noted. Drained and re-serviced oil reservoir with Exxon 2380 Oil. Accomplished post-inspection ground runs and leak checks with no discrepancies noted. Replaced (2ea.) leaking air Seals p/n 460-200. This certifies that an Annual Inspection, was complied with in accordance with Manufacturer’s Inspection program required by FAR91.409(f)(3) and found to be in airworthy condition. All maintenance performed on this APU was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see work order 93444, 93446, 93447 & 110451 on file at this agency. GARRETT AVIATION SERVICES, CRS # XB1R606K 1-800-877-5411 17250 Chanute Road Houston, Texas 77032 By: _______________________________________ Steven C. Griesmyer December 13, 2000 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 12/13/00 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 4403 2903
- 56. REPAIRED CVR .ON HAS MODS 1,4,5,6,7,8,9,10,11 INCORPORATED. REPAIR BY UNDERWOOD INSTRUMENT SERVICES, 4453 GLENN CURTISS DR, DALLAS TX 75248, FAA CRS SN1R486K, UNDER WO 94051. DESCRIPTION PN ON SN ON SN OFF COCKPIT VOICE RECORDER 93-A100-83 54297 NSN 02/26/01 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 4455.3 2944 REPLACED APU HIGH OIL TEMP SW DESCRIPTION PN ON SN ON SN OFF APU HIGH OIL TEMP SW 160260-3 NSN NSN +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 05/3/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4509.7 2976 REPLACED PN 80037-121 DECAF COFFEE THERMOS WITH NEW PN THERMOS. DESCRIPTION PN ON SN ON SN OFF DECAF COFFEE THERMOS 80037-110V 3690 012 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 05/8 -11 /01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4527.2 2984 REINSTALLED #1 AND #2 NAV UNITS (AFTER TS?). DESCRIPTION PN ON SN ON SN OFF #1 NAV UNIT 7510100-911 91070702 NA #2 NAV UNIT 7510100-911 88080165 NA ON 5/11/01 REPLACED ALL MAXERETTS FOR TIME. DESCRIPTION PN ON SN ON SN OFF LH OB MAXERET AC65218 LA306 LA307
- 57. LH IB MAXERETAC65216 LA318 LAA322 RH IB MAXERETT AC65218 KW464 KS061 RH OB MAXERETT AC65216 KR172 KY358 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 05/18/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4530.4 2988 REMOVED THIRD CHANNEL STALL DETECTOR AND REPLACED WITH SERVICEABLE UNIT FROM N802X DESCRIPTION PN ON SN ON SN OFF STALL DETECTOR 10201-1 136 200 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 06/8/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4550.3 2998 SEALED ELT ELECTRICAL CONNECTION IAW AIRTEX DOCUMENT #570-0421 INSTALLATION PARAGRAPH 3.8. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 06/13/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4556 3000 REMOVED #2 INVERTER FOR TEMP INSTALL IN HAWKER 800 SN 258127. REINSTALLED SAME. DESCRIPTION PN ON SN ON SN OFF #2 STATIC INVERTER 501-1235-01 1709 1709
- 58. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ EXXON BAE125-800A S/N:28128 NXXXX June 20, 2001 Total Aircraft Time: 4558.1 Total Landings 3002 Complied with Raytheon Aircraft Hawker 800 Aircraft Flex Maintenance Schedule Overweight or Heavy Landing Inspection except for the following items: 5. Fuselage B. 1 through 3. 9. System and Equipment/Furnishings; A. Inspect: Items 6, 7, 8 B. Test: Item 1. 10. Final Items A. 1 through 3 B. 1 through 3 . Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT. All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service. For details, see work order 124585 on file at this agency. Garrett Aviation Services CRS XB1R606K 17250 Chanute Road - Houston, Texas 77032 By: _______________________ Les Berkheiser +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 07/03/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4606 3040 CW SB 00-12 REV 2 INSTALLATION OF SUPPLEMENTAL DATA PLATE. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 07/12/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularities Report 4564.2 3006
- 59. R&R INOP MICROWAVEOVEN DESCRIPTION PN ON SN ON SN OFF MICROWAVE OVEN R4080A 03848 03853 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 07/17/01 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 4564.2 3006 REMOVED FAILED 60 ZH GALLEY INVERTER. REPLACED WITH NEW FROM FALCON CREST, OH BY KGS ELECTRONICS, 418 LIVE OAK AVE, ARCADIA, CA 91006, TEL 626-574-1175 DESCRIPTION PN ON SN ON SN OFF STATIC INVERTER SPS1607 475 127 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 07/26/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 4606.2 3031 #2 COM NO #1 AUDIO PANEL HAS NO AUDIO BUT CAN TRANSMIT. UNABLE TO DUPLICATE. SWAPPED AV850 AUDIO CONTROL PANELS. DESCRIPTION PN ON SN ON SN OFF LH AV850 AUDIO CONTROL PANEL 7511000-910 88110217 88020114 RH AV850 AUDIO CONTROL PANEL 7511000-910 88020114 88020117 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Complied with Raytheon Aircraft Hawker 800 Aircraft Flex Maintenance Schedule Overweight or Heavy Landing Inspection except for the following items: 5. Fuselage B. 1 through 3. 9. System and Equipment/Furnishings; A. Inspect: Items 6, 7, 8 B. Test: Item 1. 10. Final Items A. 1 through 3 B. 1 through 3 .
- 60. Complied with RaytheonAircraft Hawker 800 Aircraft Flex Maintenance Schedule Overweight or Heavy Landing Inspection except for the following items: 5. Fuselage B. 1 through 3. 9. System and Equipment/Furnishings; A. Inspect: Items 6, 7, 8 B. Test: Item 1. 10. Final Items A. 1 through 3 B. 1 through 3 . Complied with Raytheon Aircraft Hawker 800 Aircraft Flex Maintenance Schedule Overweight or Heavy Landing Inspection except for the following items: 5. Fuselage B. 1 through 3. 9. System and Equipment/Furnishings; A. Inspect: Items 6, 7, 8 B. Test: Item 1. 10. Final Items A. 1 through 3 B. 1 through 3 . Complied with Raytheon Aircraft Hawker 800 Aircraft Flex Maintenance Schedule Overweight or Heavy Landing Inspection except for the following items: 5. Fuselage B. 1 through 3. 9. System and Equipment/Furnishings; A. Inspect: Items 6, 7, 8 B. Test: Item 1. 10. Final Items A. 1 through 3 B. 1 through 3 . Complied with Raytheon Aircraft Hawker 800 Aircraft Flex Maintenance Schedule Overweight or Heavy Landing Inspection except for the following items: 5. Fuselage B. 1 through 3. 9. System and Equipment/Furnishings; A. Inspect: Items 6, 7, 8 B. Test: Item 1. 10. Final Items A. 1 through 3 B. 1 through 3 . Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT. Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT.
- 61. Removed old sealon the right wing fillet and installed new seal P/N J3081X9FT. Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT. Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT. Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT. Removed old seal on the right wing fillet and installed new seal P/N J3081X9FT. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation BAE125-800 S/N 2581XX NXXXX August 13, 2001 Aircraft Total Time: 4575.4 Landings: 3014 Complied with the following CAMP’s cards: Card # Item 34.035 341085 Test Left Altimeter 34.045 341086 Test Right Altimeter 34.115 341240 Test No. 1 Air Data Computer 34.115 341241 Test No. 2 Air Data Computer 34.445 345229 System Test No. 1 Transponder 34.445 345230 System Test No. 2 Transponder 34.040 341103 Calibrate Standby Airspeed Indicator This certifies that the ATC Transponder test and inspections required by FAR 91.413 were performed and found to comply with FAR 43, Appendix “F”. # 1 Make: Make: Honeywell P/N 7510700-802 S/N 89010256 Date Certified: 08/13/01
- 62. # 2 Make:Make: Honeywell P/N 7510700-802 S/N 88070149 Date Certified: 08/13/01 This certifies that the altimeter and pitot/static test and inspections required by FAR 91.411 were performed and found to comply with FAR 43, Appendix “E”. The altimeters and pitot/static’s systems have been tested to 50,00 feet. #1 Altimeter Make: Honeywell P/N 4016341-906 S/N: 87044536 Date Certified: 08/13/01 #2 Altimeter Make: Honeywell P/N 4016341-906 S/N: 88125262 Date Certified: 08/13/01 #1 ADC Make: Honeywell P/N 7000700-968 S/N: 88112967Date Certified: 08/13/01 #2 ADC Make: Honeywell P/N 7000700-968 S/N: 89013060Date Certified: 08/13/01 Standby Alt Make: Smiths Ind. P/N WL1605AM2 S/N: AE576 Date Certified: 08/13/01 All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see W/O #127525 on file at this agency. Garrett Aviation Services, 17250 Chanute Road Houston, Texas 770327 CRS # XB1R606K By: _____________________ Les Berkheiser +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 09/01/01 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 4606.2 3031 AD 2001-15-17 FOUND NA BY AC MODEL. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 09/26/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 4606.2 3031 LH #6 FUEL PROBE REPLACED. DESCRIPTION PN ON SN ON SN OFF FUEL QTY PROBE 0204KTU6 5329 TU9877 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation
- 63. BAE125-800 S/N 2581XXNXXXX September 27, 2001 Aircraft Total Time: 4606.2 Landings: 3031 34 Navigation CW Integration check of the # 1 system, IAW FAR 43 Appendix “E” Paragraph “C” #1 ADC: Make: Honeywell P/N 7000700-968 S/N: 88112967 # 1 Make: Make: Honeywell P/N 7510700-802 S/N 89010256 All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see W/O #130182 on file at this agency. Garrett Aviation Services, 17250 Chanute Road Houston, Texas 770327 CRS # XB1R606K By: Ronald Wright / _____________________ +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ October 15, 2001 Exxon entry: TT 4619.3, CYC 3040 CW SB 57-3364 Issued Sept 2001, Modification 25F966A. By Installation of new P-Seal on the LH and RH Flap Shrouds. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 11/07 /01 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report 4646.0 3060 REPLACED #2 O2 OXYGEN SHUT OFF VALVE. DESCRIPTION PN ON SN ON SN OFF VALVE, OXYGEN SOV WKA31424 1143 126 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ November 19, 2001
- 64. Exxon entry: TT4649.1, CYC 3064 CW Mandatory SB 32-3499 Issued Oct 2001. Found none of the maxarets sn were on the lists. NFAR +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 11/15- 19 /01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 4649.1 3064 RH FUEL QTY FLUCTUATES. FOUND BAD RH #6 FUEL PROBE, REPLACED SAME. CW SB 32-3499. FOUND MAXERETS (SN) WERE NOT ON THE LIST. NO FURTHER ACTION RQD. DESCRIPTION PN ON SN ON SN OFF FUEL QTY PROBE 0204KTU6 635 TU9878 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 12/01/01 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 4676.1 3088 INSPECTED WING FAIRING (AVIONICS) SEAL PER AAI ( AAL ?) INFORMATION CIRCULAR 93-001. NO DEFECTS FOUND. REPLACED RH AIRBRAKE JACK WITH OH UNIT. DESCRIPTION PN ON SN ON SN OFF AIRBRAKE JACK AIR46521 LK0367 LK8204128 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 01/02/02 Exxon Mobil Corporation Irregularity report 4688.1 H 3098 L APU HOT SECTION SHROUD SW CHANGED AFTER FAILED TEST. DESCRIPTION PN ON SN ON SN OFF TEMP SW 160275-1 144606 47793 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ EXXON BAE125-800A S/N: 28128 NXXXX January 4, 2002 Total Aircraft Time: 4689.6 Total Landings 3102
- 65. Exxon MX Entry:Removed and replaced brake control valve due to leakage, PN installed, AC 67732, SN, XM035. Knife edges on new unit have 4500 cycle remaining. Paul Beckly AP 552132832 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 01/04/02 Exxon Mobil Corporation Irregularity report 4691 H 3104 L EMERGENCY ACCUMULATOR LIGHT COMES ON 10 MIN AFTER ENGINE SHUTDOWN. FOUND BRAKE CONTROL VALVE LEAKING FROM EXHAUST PORT. R&R BRAKE CONTROL VALVE. KNIFE EDGES ON INSTALLED VALVE HAD 4500 REMAINING CYCLES. DESCRIPTION PN ON SN ON SN OFF BRAKE CONTROL VALVE AC67732 XM035 KR087 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 01/14/02 Exxon Mobil Corporation Irregularity report 4691 H 3104 L REPLACED #2 AC GEN CONTROLLER. DESCRIPTION PN ON SN ON SN OFF #2 AC GENERATOR CONTROLLER CB02701 H1242 H1228 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 01/21/02 TT 4695.2 LDGS 3110 Precision Compass Calibrators performed compass swing this date, WO# 202005 02/05/02 TT 4709 LDGS 3117 AD 2001-17-26R1. This AD has been accomplished reference entry dated 9/5/01. No further action required Tim Reardon, DOM ExxonMobil A&P 40620562 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 04/18/02 Exxon Mobil Corporation Irregularity report 4775.1 H 3162 L
- 66. CW RECOMMENDED SB57-3500 WINGS INSP OF AILERON AT OB HINGE CASTING FOR CRACKING AND CORROSION. INSTALLED #5 DRAIN HOLE PER SB 57-3500 STEPS 1-7, AILERON EXEMPT FROM EDDY CURRENT INSP STEP 8 NA, PER RAYTHEON LTR FS-2002-04-03. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 07/05/02 TT 4823.2 LDGS 3200 Removed and Replaced Aft extinguisher fired fused indicator PN A1003, installed SN F761. Next due replacement 7/10/05 Tim Reardon, DOM ExxonMobil A&P 40620562 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 08/22/02 Exxon Mobil Corporation Irregularity report CORROSION REMOVAL FROM NOSE STEERING JACK BODY SB 32-3605, APPH SB 32-505 AND 32-3165, PREVIOUSLY CW 05-07-02 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 08/30/02 TT 4848.1 LDGS 3223 Work order F5QD Removed the 2 Flitefone 800 Telephone System cabin handsets P/N 400-018100-02 left sidewall S/N 2915 and right sidewall S/N 2943. Installed 1 Honeywell Airsat 1 handset PN 300-09623-0501. SN 1297 in the left cabin sidewall IAW Duncan Aviaiton Engineering change order # 42839800 Rev A as a minor alteration. The modified area of the RH panel was recovered using the materials listed below Removed existing Flitefone 800 Telephone system and installed Honeywell Airsat 1 Telephone system as follows: ITEM Part Number Serial Number Handset Cockpit 400-018100-02 2924 RT 800 153-017712-01 837 Loop Tap 2/ea 1014888-0001 NSN ANT 100 Antenna 071-00145-0002 537
- 67. ITU 100 064-01083-01011284 WH 100 (Cockpit Handset) 300-09623-0501 1284 Satellite Phone Switch DA80-000291 008 Junction Box 300-09606-0501 1615 Junction Box 300-09606-0501 1550 Electrical aspects of the install were completed IAW the following Duncan drawings: AirSat 1 Handset Switching Unit Block Diagram Drawing # 20573400, AirSat 1 Iridium Telephone System Wiring Diagram Drawing # 52066900, Airsat 1 Wire Routing # 49904500 Mechanical aspects of the antenna install were completed IAW Duncan drawing # 75016000 Mechanical aspects of the following component installs were IAW Duncan Document DUN-A-1, FAA Approved Practices and Techniques for Aircraft Alterations, Rev 8 as follows Cockpit Handset install IAW Duncan change order # 42839800, Rev A as a minor alteration. The ITU and Satellite phone switch installs completed per section 7….The Honeywell Junction Boxes (2 Ea) installs completed per section 1 and section 7. The bulkhead feed thru installs at FS 10.4 in the upper fuselage bay (non-pressurized area) was installed per section 2 and section 7 per Duncan change order # 4840100 Rev A as a minor deviation to this specific DUN-A-! section and paragraph reference. The system ground function tested satisfactorily There are no specific Instructions for Continued Airworthiness with respect to the Honeywell Airsat 1 System. Maintenance is accomplished in an on-condition basis. Reference FAA form dated August 29, 2002 08/30/02 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 08/30/02 TT 4049.9 LDGS 3224 Complied with SB 32-3522Issue Sept 2002 Landing Gear – Dunlop wheel tie bolt nuts inspection/replacement M.J Griffith? AP 463040582 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 09/30/02 Exxon Mobil Corporation BAE125-800 S/N 2581XX NXXXX September 23, 2002 Aircraft Total Time: 4876.1 Landings: 3236
- 68. Repaired Trimtab Per Hawker 800/900XP Structural repair Manual. 55-20-11-201 Fig. 208. ( See FAA Form 8130-3. GAH-02A-0088 CRS. XB1R606K) All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details, see W/O #148788 on file at this agency. Garrett Aviation Services, 17250 Chanute Road Houston, Texas 770327 CRS # XB1R606K By: Nick Kyriazis.__________________________ +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 02/24/03 Exxon Mobil Corporation Irregularity report 4978 H 3316 L EMERGENCY BRAKE LOW PRESS WARN SW TIME CHANGE RQMT. CHANGE LEFT AND RIGHT EMERGENCY BRAKE PRESSURE SW DESCRIPTION PN ON SN ON SH OFF LT E BRAKE PRESS SW TP42000 554 1654 LT E BRAKE PRESS SW TP42000 1651 1650 CHANGE #1 AND #2 INVERTER CONTACTOR DESCRIPTION PN ON SN ON SH OFF #1 INVERT CNTR LDA2008-18C 1497 M10128 #2 INVERT CNTR LDA2008-18C F4148 M10122 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 02/27/03 TT 4978.1 LDGS 3316
- 69. Complied with MandatorySB 24-3588, issued Feb 2003. By Inspection/Repair of wire bundles from panel “JA” and pressure bung “DD”. Note, see attached letter from Dave Smith Raytheon Aircraft Co Technical Support rep (Message number 216-03-AE-0083L) Tim Reardon, DOM ExxonMobil A&P 40620562 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 3/07/03 TT 4980.7 LDGS 3320 Intent of AD 2003-04-20. This AD has been accomplished by Raytheon SB 32-3391 dated August 2000 which was completed by Garrett Aviation Services, CRS # XB1R606K, Dec 13, 2000. No further action required. Tim Reardon, DOM ExxonMobil A&P 40620562 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 03/10/03 Exxon Mobil Corporation Irregularity report CHANGE #1 AND CHANGE #2 NAV COMPUTER DESCRIPTION PN ON SN ON SH OFF NAV COMPUTER 7018879-01002 96121251 97011278 NAV COMPUTER 7018879-03104 97011278 96121251 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation Irregularity report CW MANDATORY SB 32-3519, SECTION A, ITEM 1-10, REPLACEMENT OF NLG BEARING BLOCK ASSY DESCRIPTION PN ON SN ON SH OFF PIVOT BEARING BLOCK ASSY 140-810241-0003 NSN CW STRUCTURAL INSP 5300004. 03/17/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 3/20/03 TT 4992.4 LDGS 3324
- 70. AD 2003-04-06 amendment39-13054 Docket 2003-nm-41AD has been accomplished by visual inspection mod “L” is not installed. No further action is required Tim Reardon, DOM ExxonMobil A&P 40620562 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation Irregularity report 4993.9 CYC 3326 LDGS AOA HEAT FAIL LIGHT ILLUM. REPLACED AOA TRANSMITTER, OP CK PER TELEDYNE AVIONICS GLCP7000 OPS CK OK. DESCRIPTION PN ON SN ON SH OFF AOA TRANSMITTER SL77911 DG0021B DG0020B 03/25/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 4/14/03 TT 5007 LDGS 3335 Intent of AD 2003-07-07 Amendment 39-13103 Docket 2002-mn-268 AD complied with by compliance with SB 32-3522 on 8-30-02 Tim Reardon, DOM ExxonMobil A&P 40620562 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 4/30/03 TT 5025.5 LDGS 3347 Complied with AD 74-08-09R2, note next due 06-02-05 Tim Reardon, DOM ExxonMobil A&P 40620562 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 08/04/03 Exxon Mobil Corporation BAE125-800 S/N 2581XX NXXXX August 04, 2003 Aircraft Total Time: 5074. 1 Landings: 3383 COMPLIED WITH THE FOLLOWING CAMP CARD CODES: # 341025 PRESSURE TEST LEFT PITOT SYSTEM # 341026 PRESSURE TEST RIGHT PITOT SYSTEM
- 71. # 341037 SUCTIONTEST LEFT STATIC SYSTEM # 341038 SUCTION TEST RIGHT STATIC SYSTEM # 341085 TEST LEFT ALTIMETER # 341086 TEST RIGHT ALTIMETER # 341103 TEST STANDBY ALTIMETER # 341240 TEST NO. 1 AIR DATA COMPUTER # 341241 TEST NO. 2 AIR DATA COMPUTER # 345229 SYSTEM TEST NO. 1 AIR TRAFFIC CONTROL TRANSPONDER # 345230 SYSTEM TEST NO. 2 AIR TRAFFIC CONTROL TRANSPONDER This certifies that the altimeter and pitot/static system tests and inspections required by FAR 91.411 were performed and found to comply with FAR 43, Appendix "E". The altimeter(s) and Pitot/static system(s) have been tested to 50,000 feet. #1 Altimeter Make: HONEYWELL P/N: 4016341-906 S/N: 88075082 Date: 08 / 04 / 03 #1 Air Data Computer: HONEYWELL P/N: 7000700-968 S/N: 88112967 Date: 08 / 04 / 03 #2 Altimeter Make: HONEYWELL P/N: 4016341-906 S/N: 88125262 Date: 08 / 04 / 03 #2 Air Data Computer: HONEYWELL P/N: 7000700-968 S/N: 89013060 Date: 08 / 04 / 03 Standby Altimeter Make: HONEYWELL P/N: WL1605AM2 S/N: AE576 Date: 08 / 04 / 03 This certifies that the ATC Transponder tests and inspections required by FAR 91.413 were performed and found to comply with FAR 43, Appendix "F". #1 Make: HONEYWELL P/N: 7510700-802 S/N: 89010256 Date: 08 / 04 / 03 #2 Make: HONEYWELL P/N: 7510700-802 S/N: 88070149 Date: 08 / 04 / 03 All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to work performed. For details see W/O # 163443 on file at this agency. Garrett Aviation Services, 17250 Chanute Road, Houston, Texas 77032 CRS # XB1R606K 1-800-877-5411 By KEN MILLER / ________________________ (ROAD TRIP) 08/04/03
- 72. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil CorporationIrregularity report 5081.7 CYC 3388 LDGS CW MANDATORY SB 26-3610 USING KIT 140-3025-0001 REMOVED CONCORDE MAIN BATTS, PN RG390E INSTALLED PER STC SA298430 DATED 8/27/91. INSTALLED HAWKER BATTERIES PN 9750W0640 HAWKER M/M 24-30. APPROVED FOR INSTALLATION PMA# PQ381OCE . DER APPROVED FAA FORM 8110-3 DATED 02/28/02. #1 SN 3227W0014 #2 SN 3227W0015 09/12/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation Irregularity report CHANGED PILOT EMERGENCY O2 MASK FOR TIME DESCRIPTION PN ON SN ON SH OFF EROS MASK MC10-14-51 13604 19244 SCOTT AVIATION OH DATED 10/27/03 09/16/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation Irregularity report REPLACED LH B SCREEN WINDOW WITH NEW FROM RAYTHEON MFG DATE 9/18/03 DESCRIPTION PN ON SN ON SH OFF B WINDOW NH24016-91 L338136 L197184 09/30/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 11/12/03 AFTT CYCLES GENERAL DYNAMICS 11/18/03 RECORD, WO D1901, JOB# 0044703 5144.9 3433 ACCOMPLISHED INSP AFTER SEVERE LANDING GEAR VIBRATION. TORQUE LINK CENTER BUSHING REPLACED. RH MAIN LANDING GEAR PIVOT NUT REPLACED, RH MLG TORQUE LINK REPLACED EDDY CURRENT INSP ON UPPER STEERING PIVOT LINK PN 258UN431-2A, LOWER STEERING PIVOT LINK PN 25-8UN431-1, EDDY CURRENT ISP OF NOSE LANDING GEAR BAY SIDEWALL, NLG GEAR LEG CASTING, DYE PENETRANT INSP OF: LH KNUCKLE PIN PN 25-8UM43-1 SECURED LOOSE NOSE WHEEL AXLE , NEW LH & RH MLG TORQUE LINK UPPER AND LOWER PIN AND
- 73. BUSHINGS AND RAYTHEON SB32-3135, REV 2 INCORPORATED DESCRIPTION PN ON SN ON SN OFF LH & RH MLG TORQUE LINK UPPER PIN 25-8UM131-11A RH MLG TORQUE LINK BUSHINGS 25-8UM525-1 25-8UM527-1 25UM543 RH UPPER LINK 25-8UM9-13A LH & H MLG TORQUE LINK CENTER PIVOT BUSH 25UM543 RH KNUCKLE BOLT 25-8UM43-1 RH AND LH UPPER AND LOWER TORQUE LINK PINS (4 EA) 5-8UM131-11A +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation Irregularity report R&R ELEVATOR TRIM MOTOR FOR TIME DESCRIPTION PN ON SN ON SH OFF 334D6A 622-3260-001 706 40 11/19/03 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation Irregularity report CHANGED COPILOT EMERGENCY O2 MASK FOR TIME DESCRIPTION PN ON SN ON SH OFF EROS MASK MC10-14-51 27722 19244 SCOTT AVIATION OH DATED 10/27/03 11/25/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 1/16/04 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5174.9 3459 MASTER OXYGEN SUPPLY VALVE WILL NOT CLOSE COMPLETELY, REMOVED AND REPLACED MASTER OXYGEN SUPPLY VALVE DESCRIPTION PN ON SN ON SN OFF Oxygen SOV SDV1012 6326 384 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
- 74. Exxon Mobil Corporation BAE125-800S/N 2581XX NXXXX January 21, 2004 Aircraft Total Time: 5180.7 Landings: 3462 COMPLIED WITH THE FOLLOWING CAMP CARD CODES: # 341025 PRESSURE TEST LEFT PITOT SYSTEM # 345229 SYSTEM TEST NO. 1 AIR TRAFFIC CONTROL TRANSPONDER # 341037 SUCTION TEST LEFT STATIC SYSTEM # 341240 TEST NO. 1 AIR DATA COMPUTER This certifies that the altimeter and pitot/static system tests and inspections required by FAR 91.411 were performed and found to comply with FAR 43, Appendix "E". The altimeter(s) and Pitot/static system(s) have been tested to 50,000 feet. This certifies that the ATC Transponder tests and inspections required by FAR 91.413 were performed and found to comply with FAR 43, Appendix "F". #1 Make: HONEYWELL P/N: 7510700-802 S/N: 89010256 Date: 08 / 04 / 03 #2 Make: HONEYWELL P/N: 7510700-802 S/N: 88070149 Date: 08 / 04 / 03 All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to work performed. For details see W/O # 171792 on file at this agency. Garrett Aviation Services, 17250 Chanute Road, Houston, Texas 77032 CRS # XB1R606K 1-800-877-5411 By JOHN GALIK / ________________________ (ROAD TRIP) 1/21/04 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 3/25/04 AFTT CYCLES Transcribed Exxon Mobil Corp CAMP Report 5228.3 3499 ENGINE TIMES 5178.1 3477 REPLACED #2 ENGINE FUEL PUMP FOR FAILURE DESCRIPTION PN ON SN ON SN OFF
- 75. ENG FUEL PUMP3070850-57 MX-491588 MX519224 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Reg.# : NXXXX Date: April 14, 2004 Work Order: FB9V Make: Raytheon Model: BAe 125-800A S/N: 2581XX TAT: 5230.1 Landings: 3500 APU HOBBS: 3587.4 I) The following was performed by Duncan Aviation’s Airframe Department on work order #FB9VA: A) Performed minor alteration by fabricating and installing nutplate rings and nut plate strips for left and right static port installation using .040” 2024-T3 aluminum in accordance with Duncan Drawing # 75016500. II) Accomplished the following to meet the technical requirements for RVSM operations: A) SB 34-3110 R8 Modification No. 25F731A “Navigation – ADC Increased Accuracy (Honeywell)” 1) Removed #1 ADC P/N 7000700-968, S/N 88092843 and installed modified ADC P/N 7000700-668, S/N 88092843. Modification performed by Honeywell Intl., CRS# LV2R992K on work order 390050 dated April 03, 2004. 2) Removed #2 ADC P/N 7000700-968, S/N 89013060 and installed modified ADC P/N 7000700-668, S/N 89013060. Modification performed by Honeywell Intl., CRS# LV2R992K on work order 390050 dated April 8, 2004. B) 24 Month Certification of the #1 and #2 Pitot/Static Systems: 1) The #1 Altimeter (P/N 4016341-906, S/N 88075082) and #2 Altimeter (P/N 4016341-906, S/N 88125262), #1 Air Data (P/N 7000700-668, S/N 88092843) and #2 Air Data (P/N 7000700-668, S/N 89013060) and Static System Test required by 14 CFR 91.411 and #1 and #2 Transponder Tests, including Data Correspondence, required by 14 CFR 91.413 have been performed and found to comply with 14 CFR Part 43, Appendix E & F. (a) The #1 and #2 Altimeters were tested to 50,000 feet on April 13, 2004 (b) The #1 and #2 Transponders were tested on April 13, 2004. (c) The #1 and #2 Encoder Data Correspondence were tested to 50,000 feet on April 13, 2004. (d) The S5 Static System was Leak Tested on April 13, 2004 . (e) The S6, S8, S9 P Vent Static Systems were Leak Tested on April 13, 2004 C) 24 Month Certification of the Standby Static Altimeter System: D) Tested and inspected the Standby altimeter and S8 static system have been tested and found to comply with 14 CFR Part 91.411, Paragraph (a)(2) and 14 CFR 43 Appendix E Para (b). This system and unit are not integrated into an encoding source. 1) The Standby Altimeter P/N WL1605AM2, S/N AE576 was tested to 50,000 feet on April 13, 2004. 2) The Standby Static System was Leak Tested on April 13, 2004. E) The above units and systems meet RVSM required capabilities as per Raytheon SB 34-3110 R8 Steps: 3A 18 through 28. Aircraft maintenance manual Chapters 34-10-17 and 34-11-17. F) Inspected left and right static plates in accordance with Hawker AMM 125-800 34-11-29, measurements as follows: D1 D2 D3 D4 Left Plate .068 .067 .066 .068 Right Plate .069 .069 .067 .065 G) Inspected Nose Avionics Panels, measurements as follows: F Upper Fwd F2 Upper Aft F3 Lower Aft F4 Lower Fwd Left Nose Avionics .000” .001” .000” .000” Right Nose Avionics .001” .001” .003” .001” H) Vertical skin joint forward of static plates dimensions left and right side do not exceed .020” out of wind and .010” into wind. III) Completed the following Service Bulletin: A) SB 22-3577 “Introduction of Improvements to Honeywell FZ-800 Flight Guidance Computer” 1) Removed #1 FGC FZ-800 P/N 7003974-713, S/N 89041674 and installed modified FZ-800 P/N 7003974-732, S/N 89041674. Modification performed by Honeywell CRS# TT1R518K on work order G520810 dated April 6, 2004.
- 76. 2) Removed #2FGC FZ-800 P/N 7003974-713, S/N 87080925 and installed modified FZ-800 P/N 7003974-732, S/N 87080925. Modification performed by Honeywell CRS# TT1R518K on work order G520806 dated April 6, 2004. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FB9VA, FB9VB, FB9VC. Signed__________________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 4/14/04 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 04/30/04 ACTT 5241.6, CYC 3508 REMOVED TCAS PROCESSOR PN 4066010-904, SN 9502286, INSTALLED 4066010-910, SN 92081106, C/W OPS CK, ALL OK. EXXON MX. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation BAE125-800 S/N 2581XX NXXXX May 04, 2004 Aircraft Total Time: 5248.2 Landings: 3510 COMPLIED WITH THE FOLLOWING CAMP CARD CODES: # 341025 PRESSURE TEST LEFT PITOT SYSTEM # 341037 SUCTION TEST LEFT STATIC SYSTEM # 341085 TEST LEFT ALTIMETER This certifies that the pilots altimeter and pitot/static system tests and inspections required by FAR 91.411 were performed and found to comply with FAR 43, Appendix "E". The altimeter(s) and Pitot/static system(s) have been tested to 50,000 feet. All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to work performed. For details see W/O # 177031 on file at this agency. Garrett Aviation Services, 17250 Chanute Road, Houston, Texas 77032 CRS # XB1R606K 1-800-877-5411
- 77. By JOHN GALIK/ ________________________ (ROAD TRIP) MAY 4 2004 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 6/9/04 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5306 3549 NLG RED WARNING LIGHT NOT ILLUMINATED ON GND WITH NLG DOORS OPEN. REPAIRED BROKEN WIRES BETWEEN TB AQ2L AND AQ1L AND NOSE GEAR DOOR STRUT SW. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 06/14/04 AD 2004-12-02 INTENT OF AD CW WITH INCORPORATION OF RAYTHEON MANDATORY SB 24-3588 REV1 ON 02/27/03, (LOGBOOK 2, PG 37 & MANDATORY MOD RECORD PG 10) +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 06/15/04 AD 2004-11-01 INTENT OF AD CW WITH INCORPORATION OF RAYTHEON MANDATORY SB 26-3610 R1 ON 9/12/03, ADDITION OF FIRE EXTINGUISHER MARKING BANDS ( MANDATORY MOD RECORD PG 11) +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 7/1/04 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5306 3549 ELECTROLYTE SPILLED ON AIRCRAFT AND BATT RACK FROM IRS NICAD. REMOVED BATT RACK AND BATT. WASHED BAT RACK, TREATED RACK AND AIRCRAFT IN VICINITY OF BATT WITH MILD ACETIC ACID SOLUTION, BEAD BLASTED RACK TO REMOVE CORROSION. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 8/13/04 AFTT CYCLES
- 78. Transcribed Exxon MobilCorp CAMP Report 5343.6 3571 REPLACED ENGINE FUEL SYNCHRONIZER , TROUBLESHOOTING BOX ON CAMP FORM CHECKED. INSTALLED TIME SINCE NEW 192 MOS, 5490 HRS, 3662 LDGS. DESCRIPTION PN ON SN ON SN OFF ENG FUEL SYNCHRO 2118114-1 18-262 84-140 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 9/9/04 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5395.7 3604 REPLACED #5 BATTERY DESCRIPTION PN ON SN ON SN OFF EMERGENCY BATT RG-126 40045738 CBC419190 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 9/24/04 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5379.99 3593 VENTRAL REFUEL VALVE EMITS LOUD NOISE AND CONTINUES TO RUN AFTER CLOSING. REPLACED VALVE ACTUATOR AND ADJUSTED PER AMM DESCRIPTION PN ON SN ON SN OFF SOV ACTUATOR HTE9044-001 382GB370/H 487GB144/H +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 9/30/04 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5397.1 3606 RT SIDE SCREEN HEAT LIGHT ILLUMINATED REPLACED RIGHT “A” SCREEN THERMAL CONTROLLER MK22 DESCRIPTION PN ON SN ON SN OFF ND0075-2011 L341455 L205411 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 1/25/05 AFTT CYCLES Transcribed Exxon Mobil Corporation CAMP Report UNKN UNKN
- 79. AD 2003-26-14 NA,KIDDE AEROSPACE pn 898052 HAND HELD FIRE EXTINGUISHERS NOT INSTALLED. ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 02/03/05 Reg.# : NXXXX Date: February 3, 2005 Work Order: FB3C Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5487.1 Landings: 3668 IV) Performed the following Manufacturer’s Recommended Maintenance items in accordance with Raytheon Hawker 800 and BAe 125 Series 800A and 800 B Aircraft Flexible Maintenance Schedule Revision 8: A) Routine Inspections: 1) 050570: Inspection E5 2) 050680: Inspection F3 3) 050780: Inspection G (050067) a) Reinstalled altitude switch P/N 1103KSD-BU1 S/N AL928 after inspection performed by Duncan Aviation CRS #JGVR149F under work order #FB3CA. (210018) b) Reinstalled hydraulic overheat temperature switch P/N 150T283 S/N 618 after inspection performed by Duncan Aviation CRS #JGVR194F under work order #FB3CA. (290012) B) Structural Inspections: All X-Ray Inspections performed by Tailwind Inspections, Inc. Tulsa, OK on work order #4339 Dated: January 15, 2005. 1) 320032: 8 Year / 4 Year Left/Right Main Landing Gear Fairing Strut Inspection (NTM 32-10-103). 2) 510001: 4000 Landing Initial / 5000 Landing/12 Year Nose Landing Gear Bay Sidewalls (NTM 53-10-111). 3) 510003: 12 Year / 4 Year Flight Compartment Skin & Window Structure Above Windshields Insp (NTM 53-10-105A). 4) 510005: 15 Year to 18 Year / 8 Year Center Fuselage Structure Below the Floor Inspection (NTM 53-10-108; 53-10-107; 53-10-108B; 53-10- 109) 5) 510006: 8 Year Structure Below Escape Hatch Detailed Inspection. 6) 510007: 8 Year Center Fuselage Structure Below the Floor Frames 13 to 16 Inspection (NTM 53-10-106A) 7) 510008: 15 Year/18 Year Center Fuselage Structure Below the Floor Inspection (NTM 53-10-108A). 8) 510009: 4 Year Entry Door Surround Detailed Inspection. 9) 510010: 15 Year/18 Year / 8 Year Center Fuselage Structure Insp (NTM 53-10-101; 53-10-102; 53-10-103A; 53-10-104; 53-10-106). 10) 520009: 15 Year to 18 Year / 8 Year Escape Hatch Detailed Inspection. 11) 530001: 8 Year / 4 Year Skin Exterior Under the Dorsal Intake Detailed Inspection. 12) 530002: 8 Year / 4 Year Fuselage Skin Under Wing-to-Fuselage Fairings Inspection. 13) 530009: 8 Year Fuselage Skin Covered by the Ventral Fuel Tank Detailed Inspection. 14) 530010: 15 Year to 18 Year / 8 Year Ventral Fuel Tank Detailed Inspection. 15) 530011: 8 Year / 4 Year Front Face of Rear Pressure Bulkhead Inspection. 16) 530012: 8 Year Front Face of Rear Pressure Bulkhead (Frame 19) Inspection. 17) 550001: 1200 Flight Hour/2 Year Horizontal Stabilizer to Vertical Stabilizer Rear Attachment Fitting Inspection. 18) 550002: 8 Year Horizontal Stabilizer Detailed Inspection. 19) 550003: 15 Year to 18 Year / 8 Year Vertical Stab Detailed Inspection (NTM 55-30-101; 55-30-102; 55-30-103). 20) 550004: 8 Year Horizontal Stabilizer to Vertical Stabilizer Attachments Detailed Inspection. 21) 550006: 8 Year / 4 Year Left/Right Elevator Inspection (NTM 55-20-101; 55-20-102). 22) 550007: 4 Year Inspection of Left/Right Elevator Detailed Inspection. 23) 550008: 4 Year Connecting Rods, Left/Right Elevator Trim Tabs Lube/Replace. 24) 550009: 4 Year Rudder Detailed Inspection. 25) 550010: 4 Year Connecting Rods, Rudder Trim Tab and Anti-Servo Tab Lube/Replace. 26) 550011: 8 Year / 4 Year Rudder Inspection (NTM 55-40-101). 27) 550012: 15 Year to 18 Year / 8 Year Horizontal Stabilizer Inspection (NTM 55-10-101; 55-10-102; 55-10-103). 28) 550014: 8 Year Rudder Hinge Brackets and Attachments Detailed Inspection. 29) 550015: 2 Year Left/Right Elevator Mass Balance Weight Inspection. 30) 570007: 8 Year / 4 Year Left/Right Wing Bottom Skins & Stringers Between Front and Rear Spars Insp (NTM 57-30-101) 31) 570008: 4 Year Left/Right Main Landing Gear and Sidestay Attachment Fittings Detailed Inspection. 32) 570009: 4 Year Left/Right Wing Top Skin in the area of the Wing Fence Detailed Inspection. 33) 570011: 4800 Hour/8 Year Wing Front Spar Forward Face Detailed Inspection. 34) 570012: 4800 Hour/8 Year / 2400 Hour/4 Year Left/Right Wing Rear Spar Rear Face Inspection. 35) 570013: 4800 Hour/8 Year / 2400 Hour/4 Year Left/Right Upper/Lower Airbrake Detailed Inspection. 36) 570014: 4800 Hour/8 Year / 2400 Hour/4 Year Left/Right Aileron Inspection (NTM 57-50-107).
- 80. 37) 570015: 2400Hour/4 Year Left/Right Aileron Detailed Inspection. 38) 570016: 2400 Hour/4 Year Connecting Rods, Left/Right Aileron Trim and Servo Tabs Lube/Replace. 39) 570017: 4800 Hour/8 Year / 2400 Hour/4 Year Left/Right Flap and Flap Vanes Insp (NTM 57-50-105; 57-50-106). 40) 570024: 4 Year Inspection Left/Right Aileron Horn Balance Weight Detailed Inspection. 41) 570029: 4800 Hour/8 Year Left/Right Wing Internal Structure Forward of Center Spar Detailed Inspection. 42) 570030: 4 Year Left/Right Aileron at Outboard Hinge Casting Inspection. V) The following was performed by Duncan Aviation’s Airframe Department on work order # FB3CA: A) Repaired Pilot’s outboard seat track IAW Corporate Jets Engineering Repair Instruction #RIL 25 FN 46 and Raytheon Aircraft Company Field Repair #FR-HK-02330 Rev. 1 B) Reinstalled CVR P/N 93-A100-83 S/N 54297 after repair performed by Duncan Aviation CRS #JGVR194F under work order #FB3CA. C) Reinstalled IRS Battery P/N 28002-001 S/N 9701247 after repair performed by Duncan Aviation, CRS #JGVR194F on work order #FB3CA. D) Removed flap control unit P/N 614MK2 S/N H-599 and installed unit P/N 614MK2 S/N 614S231 after overhaul performed by Unipak Aviation CRS #UW2R229L under work order #L1978 dated November 23, 2004. E) Installed new left aileron wing cable P/N 25-8CF109-5A. F) Installed repaired left main gear door strut assy P/N 25-8UM91-1A. Repair performed by Garrett Aviation Services, CRS #XB1R606K on work order #934441 dated November 15, 2000. G) Installed repaired right main gear door strut assy P/N 25-8UM91-1A. Repair performed by Garrett Aviation Services, CRS #XB1R606K on work order #934441 dated November 15, 2000 H) Removed #1 ADF antenna P/N 7510300-901 S/N 88100207 and installed new antenna P/N 7510300-901 S/N 04118911. I) Adjusted left static plate height per Maintenance Manual Chap 34-11-29. D1 D2 D3 D4 Left .073 .075 .072 .070 Right .070 .070 .072 .071 J) Fabricated and installed new left wing inboard, aft, crash panel mounting plate between ribs 3 and 4 per Hawker 800 & 800XP and BAe 125 Series 800A and 800B Structural Repair Manual and Duncan Aviation Engineering Change Order (ECO) number 050115001, dated January 15, 2005 approved on FAA form 8110-3 dated January 17, 2005. Reference FAA form 337 dated February 2, 2005. K) Removed and replaced left and right elevator inboard leading edge skins with new. P/N S25TE4135 and P/N S25TE4136. Painted and balanced left and right elevators. VI) Service Bulletins and Service Information: A) Completed the following British Aerospace/Raytheon Aircraft Service Bulletins: 1) SB 53-73 R2 “Eddy Current Insp of NLG Bay Sidewalls” VII) Researched Airworthiness Directives and had the following results: A) Completed Airworthiness Directives: 1) AD 70-22-04 Amendment 39-1207, effective date May 19, 1971 “Wood Electric Circuit Breakers’. Complied with by inspecting installed circuit breakers, no Wood Electric circuit breakers are currently installed. 2) AD 92-06-05 R1, Amendment 39-8251 effective date April 21, 1992. “Prevent Reduced Structural Integrity of the Fuselage and subsequent Decompression of the Aircraft” 3) AD 98-25-10 R1, Amendment 39-11460 effective date January 14, 2000. Complied with para (a) by visual inspection. Seatbelt locking mechanisms found to be serviceable at this time. B) Found the following Airworthiness Directives are “Not Applicable, affected equipment is currently not installed”: 93-07-05 94-02-02 95-24-10 95-26-15 96-21-03 97-07-12 97-04-15 97-16-10 97-18-03 98-08-20 98-14-03 98-20-17 98-24-27 98-25-02 99-01-14 99-04-10 99-12-06 99-23-24 2000-05-24 2000-07-27 2000-18-04 2001-10-09 2001-10-13 2001-15-17 2001-22-14 2001-23-17 2002-06-05 2002-06-06 2002-13-07 2002-14-19 2002-15-02 2002-20-09 2002-21-01 2002-22-13 2003-26-06 2003-26-14 2004-08-15 2004-08-16 2004-10-15 2004-13-20 2004-16-14 2004-21-04 C) Found the following Airworthiness Directive is “Not Applicable by Aircraft Serial Number” 87-12-10 FLAP MOTOR ELEMENT PN MFHA151A REPLACED, FAIRLEAD PN 28-8CW399-1, LEVER ASSY (TRIM TAB HINGE) PN 25-8WG65-15A The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FB3CA. Signed__________________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 I certify this Aircraft has been inspected in accordance with an E5, F3, G and the above Structural Inspections to comply with the requirements of FAR 91.409 f (3) and is approved for return to service. Details on file under Work Order #FB3CA. 2/03/05
- 81. +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 2/05/05 AFTT CYCLES Transcribed ExxonMobil Corporation Irregularity Report 5497 3672 REPLACED STANDBY ADI HORIZON, FOR VERY SLOW TO POWER UP AND FLAG REMAINS ON. REPLACED STBY ALTIMETER FOR SLUGGISH OPERATION. NOTE INSTALLED SN IS IN QUESTION. INSTALL RECORD INDICATES AE125 DESCRIPTION PN ON SN ON SN OFF STBY HORIZON ADI H341AFM1 5057 5689 STBY ALTIMETER WL1605AM2 AE125 or AF125? AE576 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 2/21/05 TT 5501.2 CYC 3678 AD 2005-03-16 INTENT OF AD CW, WITH INCORPORATION OF RAYTHEON MANDATORY SB 26-3496 (MANDATORY MOD RECORD PG 11)ON 9/12/03 Also Exxon irreg report shows compliance date of 12/3/03 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 3/07/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5518.5 3691 PRESSURE REDUCING VALVE LEAKS DURING FUELING, REPLACED VALVE DESCRIPTION PN ON SN ON SN OFF PRESS VLV 1159000-1 FRTR109/A FR038BA +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 5/10/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5568.6 3727 CABIN FAN VERY LOUD. REPLACED CABIN RECIRCULATION FAN AS PER ARKANSAS AEROSPACE BAE 125-800 MAINTENANCE MANUAL ADDENDUM DATED 4-29-94 CH 21-20 PAGE 2 & 3 DESCRIPTION PN ON SN ON SN OFF RECIRCULATION FAN 0901-2 0161 0607 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
- 82. 5/16/05 AFTT CYCLES Transcribed ExxonMobil Corporation Irregularity Report 5576.4 3732 ENGINE FIRE BOTTLES HYDROSTATIC CK CW. FIRE BOTTLE SQUIBS CHANGED, NEXT DUE 5/17/2015 FMS REVERTS TO ACTIVE MODE SINCE DUAL INOP MESSAGE, FOUND LOOSE SHIELD GROUND ON #1 FMS AFIS “DATA IN”, REPAIRED WIRING, CKS OK. REPLACED REAR BAY DOOR SW DESCRIPTION PN ON SN ON SN OFF FWD BOTTLE 33200009 14266C1 AFT BOTTLE 33200009 14265C1 REAR BAY DOOR SW V3L-3013-DA NSN NSN FIRE BOTTLE SQUIB ON SN 14266C1 M30900000M 02190 MFD 9-04 FIRE BOTTLE SQUIB ON SN 14266C1 M30900000M 02230 MFD 9-04 FIRE BOTTLE SQUIB ON SN 14265C1 M30900000M 02209 MFD 9-04 FIRE BOTTLE SQUIB ON SN 14265C1 M30900000M 02226 MFD 9-04 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 6/29/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5611.3 3749 CHANGED IRS EMERGENCY BATTERY DESCRIPTION PN ON SN ON SN OFF CA54-1 28002-001 10300827 9701247 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 7/5/05 ACTT 5611.3 CYC 3749 REPLACED AFT EXTINGUISHER (LIFE LIMITED) NEXT DUE 7/5/08 (NO PN OR SN DATA IN LOG) +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 7/26/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 561637 3755 TIME CHANGE DUE ON DEFIBRILLATOR. REPLACED BATTERY AND PADS DESCRIPTION PN ON SN ON SN OFF
- 83. BATTERY BT1 NSN DEFRIBPADS Y020105-14 (2 EA) NSN +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 8/02/05 AD 2005-16-02 INTENT OF AD COMPLIED WITH INCORPORATION OF RAYTHEON MANDATORY SERVICE BULLETIN 24- 3272 (LOGBOOK 2, PG 15 & MANDATORY MOD RECORD PG 10) ON 9/14/00 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 9/7/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5641 3774 ELT BATTERY PACK DUE CHANGE, CW IAW ARTEX BULLETIN 571-0406 REV A DATED 7-31-01 DESCRIPTION PN ON SN ON SN OFF BATTERY 452-0133 (same pn as of 1/5/2009) NSN +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 9/10/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5649.2 3778 CREW REPORTS LH WINDSCREEN HAD A SECTION THAT WOULD NOT HEAT. REPLACED LH WINDSCREEN “A” PANEL. ALSO REPLACED WINDOW FRAME SEAL DESCRIPTION PN ON SN ON SN OFF LH “A” SCREEN NG24016-385 OFF NF24016-157 L171139(new screen installed on 3/16/2011 has same sn, different pn) L295549 WINDOW FRAME SEAL 25-8FN277-31 NSN +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Exxon Mobil Corporation BAE125-800 S/N 2581XX NXXXX September 13, 2005 ACTT: 5650.9 Landings: 3780 This certifies that the #2 altimeter and static system tests and inspections required by FAR 91.411 were performed and found to comply with FAR 43, Appendix "E" and RVSM IAW BAE SB 34-3110. The #2 altimeter and static system have been tested to 50,000 feet. #2 Altimeter Make: HONEYWELL P/N: 4016341-906 S/N: 88125262 Date: 09 / 13 / 04 #2 Air Data Computer: HONEYWELL P/N: 7000700-968 S/N: 88123056 Date: 09 / 13 / 04
- 84. This certifies thatthe #2 ATC Transponder tests and inspections required by FAR 91.413 were performed and found to comply with FAR 43, Appendix "F". #2 Make: HONEYWELL P/N: 7510700-802 S/N: 88070149 Date: 09 / 13 / 04 All maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to work performed. For details see W/O # 201451 on file at this agency. Garrett Aviation Services, 17250 Chanute Road, Houston, Texas 77032 CRS # XB1R606K 1-800-877-5411 By STEVE MCVARISH / _____________ 9/13/05 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 10/05/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5660.5 3793 LOWER CABIN LIGHTS INOP. FOUND LH AFT PROTECTED POWER UNIT CAUSING INVERTER TO FAIL. REPLACED PROTECTED POWER UNIT AND INVERTER OPS CK NORMAL . REPLACED UPPER RH CABIN INVERTER, OPS CK NORMAL DESCRIPTION PN ON SN ON SN OFF POWER SUPPLY AL-5112 39442 5328 (LOWER CABIN LIGHT?) INVERTER 18-996 4622 5414 UPPER RH CABIN LIGHT INVERTER 18-996 5283 4048 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 10/05/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity Report 5665.1 3799 RIGHT RADAR CONTROL PANEL INOP. REPLACED FO WEATHER RADAR CONTROLLER PER HONEYWELL SYSTEM MX MANUAL 22-16-00 SEC 4 REPLACED INOP TOP ANTI COLLISION BEACON LIGHT ASSY. DESCRIPTION PN ON SN ON SN OFF CONTROL PANEL 7008471-802 87090259 88010332 TOP ANTI-COLLISION LIGHT ASSY 01-0790044-01 0210 01022 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
- 85. 10/19/05 AFTT CYCLES Transcribed ExxonMobil Corporation Irregularity Report 5679.3 3811 #2 STARTER GEN CHANGED DESCRIPTION PN ON SN ON SN OFF #2 GENERATOR 23080-005 5549 5160 +++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ 11/10/05 AFTT CYCLES Transcribed Exxon Mobil Corporation Irregularity AND CAMP Report 5697.1 3820 CREW REPORTS CABIN TEMP CONTROL PROBLEMS. FOUND TURBINE BYPASS VALVE TAKES EXCESSIVE VOLTAGE FOR MOVEMENT. REPLACED SAME FOUND LOWER AND RIGHT SIDE APU MOUNT HAVE WORN ISOLATOR BUSHINGS. REPLACED SAME. AC PRESSURIZING WHEN TO POWER APPLIED (APPROX 1600 FPM) BACK TO NORMAL RATE AT LIFT OFF. FOUND LH MAIN AIR VALVE LEAKING IN THE CLOSED POSITION AND REPLACED SAME. AT APPROX 2500 FT AIR FLOW INCREASES TO MAX AND THEN AT APPROX 6500 FT INSTANT DECREASE OF AIR FLOW TO NORMAL AMOUNT. REPLACED TURBINE BYPASS VALVE. APU STARTER GEN REPLACED FOR TIME. APU REMOVED AND REPLACED TO COMPLY WITH AD 96-25-12. REPLACED APU FUEL INLET FILTER. REPLACED APU OIL TEMP SW, APU IGNITION EXCITER, APU OIL PRESSURE SW, DESCRIPTION PN ON SN ON SN OFF TURBINE BYPASS VLV 321776-1 986 888 MOUNT H3002 NSN LH MAIN AIR VALVE 321292-1 2032 2210 APU STARTER GEN 23080-005 5768 5550 APU ASSY 62T-40C8D1 877641 897611 APU FUEL INLET FILTER 211-326 00004 07420 APU HI OIL TEMP SW 160260-3 NSN TSN: 202 MO, 2044.7 HRS, 6006 CYC APU IGNITION EXCITER 110418-1 87374772 TSN: 202 MO, 2044.7 HRS, 6006 CYC 88151518 APU LO OIL PRESS SW LOP (NEW) 4950072 4144 1551 AIRCRAFT SOLD TO DUNCAN AVIATION START LOGBOOK # 3
- 86. 1/18/2006 AFTT CYCLES TranscribedLogbook Entry Duncan Aviation Log Entry The following AD were found NA: 77-02-08, 78-14-09, 89-02-05, 93-09-07, 2001-14-51, 2005-01-19, 2005-07-27, 2005-11-05, 2005-20-26, 2005-25- 08 The following SB were found NA: 71-040-3213A R2 2/1/2006 AFTT CYCLES Transcribed Logbook Entry 5718.9 3849 Lee Aerospace, CRS# YLIR8673L, Log Entry REPLACED LH & RH "C" WINDOW PANELS WITH NEW NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LH C WINDSCREEN 25-8FN353-43A L348079 25-8FN353-43A 289062 RH C WINDSCREEN 25-8FN353-44A L351170 25-8FN353-44A L288859 Reg. # NXXXX Date: February 15, 2006 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5718.9 Landings: 3849 APU HOBBS: 2075.9 I find this aircraft meets the requirements for the certification requested and have issued a Multiple Purpose Special Airworthiness Certificate, dated February 15, 2006. This action is in support of Duncan Aviation, Inc., DAS STC project number ST4449WI-T, Installation of Honeywell Primus EPIC CDS/R, Control Display System for Retrofit. This Special Airworthiness Certificate, EXPERIMENTAL, is issued for Research and Development, Market Survey and Show Compliance with the Regulations in accordance with FAA Orders 8130.2F and 8130.29. The Standard Airworthiness Certificate is secured in the Duncan Aviation Records and Research Department. This Special Airworthiness Certificate, dated February 15, 2006, with attached Operating Limitations is valid for Research and Development flights from February 15, 2006, through March 15, 2006, Market Survey flights from March 15, 2006, through July 15, 2006 and Show Compliance with Regulations flights from July 1, 2006 through August 31, 2006. Thomas L. Seidl Designated Airworthiness Representative DARF501357CE 2/27/06
- 87. Reg. # NXXXXDate: February 27, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5718.9 Landings: 3849 APU HOBBS: 2075.9 I) Performed the following Manufacturer’s Recommended Maintenance items in accordance with Raytheon Hawker 800 and BAe 125 Series 800A and 800 B Aircraft Flexible Maintenance Schedule Revision 9: A) Routine Inspections: 1) 050060: Inspection A – A1 through A6 Inclusive (050001, 050002, 050003, 050004, 050005, 050006). 2) 050130: Inspection B – B1 through B12 Inclusive (050007, 050008, 050009, 050010, 050011, 050012, 050013, 050014, 050015, 050016, 050017, 050018) 3) 050260: Inspection C – C1 through C12 Inclusive (050019, 050020, 050021, 050022, 050023, 050024, 050025, 050026, 050027, 050028, 050029, 050030) 4) 050390: Inspection D – D1 through D12 Inclusive (050031, 050032, 050033, 050034, 050035, 050036, 050037, 050038, 050039, 050040, 050041, 050042) 5) 050520: Inspection E – E1 through E12 Inclusive (050043, 050044, 050045, 050046, 050047, 050048, 050049, 050050, 050051, 050052, 050053. 050054) 6) 050650: Inspection F – F1 through F12 Inclusive (050055, 050056, 050057, 050058, 050059, 050060, 050061, 050062, 050063, 050064, 050065, 050066) B) Complied with RAC Hawker 800 Maintenance Manual Addenda Inspection Requirements. C) Structural Inspections 1) 530018: 4800 Hour / 2400 Hour Fuselage Skin Adjacent to Cabin Window Cut-Outs Detailed Inspection. D) Component Requirements: 1) #1 Main Battery Service. a) Reinstalled #1 main battery P/N 9750W0640, S/N 3227W0014 inspected/top charged by Duncan Aviation, CRS #JGVR194F under work order #FHD9A. 2) Replaced cabin fire extinguisher model 225 S/N H00548214 with new P/N A1600 S/N 569075 MFG Date 2005. 3) 5000 Landing/12 Year Landing Gear Overhaul Extension. a) Aircraft S/N 2581XX landing gear overhaul extended until the end of April-2006 / Not To Exceed 5000 Cycles. Reference Raytheon Aircraft Company Support Message No. 211-05-HK-0154E dated 12/05/05 and FAA Approval Letter from Lincoln FSDO dated January 13, 2006. 2) 4000 Landing Left/Right Main Landing Gear Reversing Valve Overhaul. a) Reinstalled LH reversing valve P/N AIR48542/1, S/N 8800109 overhauled by Duncan Aviation, CRS #JGVR194F under work order #FHD9A. b) Reinstalled RH reversing valve P/N AIR48543/1, S/N 8801070 overhauled by Duncan Aviation, CRS #JGVR194F under work order #FHD9A. II) The following was performed by Duncan Aviation under Work Order #FHD9A: 1) Weighed Aircraft using load cell weighing scales in level condition in a closed hangar. 2) Performed Cabin Leak Rate Check IAW Hawker 800 MM Ch 21-30-00, no defects noted at this time. 3) Replaced existing cockpit water separator sock with new sock P/N 800-8234-64. a) Cockpit water separator sock support cone cracked. Fabricated new -3 manifold and -5 plate from 6061-T6 aluminum per Arkansas Modification Center Drawing #800-8234. All welding was done with 5183 filler rod. Performed fluorescent penetrant inspection on weld repair area, no crack indications found. 4) Removed left cabin floor heat linear actuator P/N 1092TH100-47, S/N 1666 and installed actuator P/N 1092TH100-47, S/N 164 repaired by Aero Space Controls Corporation, CRS #OJ2R059L under work order #S.O. 19601 dated 11/11/05. 5) Removed water separator P/N 175050 S/N 18-835 and installed P/N 175050 S/N 16-174 after overhaul by Honeywell CRS #DA2R761K under work order #R061536 on 8/15/05. (8130 RECORD REFLECTS WATER SEPARATOR SOCK IN COCKPIT AIR CONDITIONING LINE, PN 800- 8234-64 REPLACED.) 6) Removed exiting external power over voltage sensor P/N E-311TS S/N CM-73308 and installed new P/N E311TS S/N CP-06114. (8130 RECORD SHOWS SN CM-73308 INSPECTED AND FOUND SERVICEABLE, POSSIBLY ABOVE IS TYPO AND CM-73308 RE-INSTALLED) 7) Removed overvoltage relay P/N E311TS, S/N CP-06114 and installed new relay P/N E311TS, S/N CP-06126. 8) Removed Pilot’s life vest P/N 102MK2BA, S/N 265529 and installed new life vest P/N P201-105, S/N 044932 (date of Mfg; 12/2005). (265529) 9) Removed Co-pilot’s life vest P/N 102MK2BA, S/N 265530 and installed new life vest P/N P0201- 105, S/N C44962 (date of Mfg: 12/2005). (265530) 10) Replaced existing cabin door internal handle dowel pins and attach screws with new P/N 25FC6517 and P/N DUS1463-2DD. 11) Performed under toilet visual inspection; no defects noted. 12) Repaired 2-each cracks on jump seat P/N 7202-981 4130 steel square tube by welding using NS-102 filler rod to match base material specified per e-mail from Raytheon Aircraft Company Technical Support. Performed fluorescent penetrant inspection of repaired area, no crack indication found.
- 88. 13) Removed RHflap screw jack P/N 25-8CW161AB S/N MEC/DHB/149 and installed screw jack P/N 25-8CW161AB, S/N MEC/DHB/136 overhauled by Midcoast Aviation CRS #RO3R822L under work order #D6905076H dated 07/01/05 (screw jack contains ball screw assembly P/N BA22294- OH, S/N 5 overhauled by Beaver Aerospace & Defense, Inc., CRS #MI5R042N under work order #393653 dated 05/13/05). 4000 CYCLE REPLACEMENT DUE 7849 14) Adjusted cable tension on RH flap cables per Hawker 800 MM 27-50-02-501. 15) Removed and installed new airbrake line (above LH flap jackscrew) P/N 25SW65-107. 16) Removed and installed aileron trim cables (upper) P/N 25-8CF113-13A and (lower) P/N 25-8CF113- 15A. Adjusted cables’ tension, rigged and checked travel of aileron trim system. 17) Adjusted elevator trim cable tensions (cables aft of servo motor) to within specified limits. 18) Adjusted forward elevator control cables tension to within specified limits. 19) Adjusted aft elevator cables tension to within specified limits. 20) Removed and installed new RH forward aileron cable P/N 25-8CW201-3A, new RH aft aileron cable P/N 25-8CF109-7A, new LH forward aileron cable P/N 25-8CW201-1A and new LH aft aileron cable P/N 25-8CF-109-5A. Adjusted cables’ tension and rigged. 21) Adjusted rudder primary cable tensions to within specified limits. 22) Replaced 4 each flap jack screw bushings on the left and right sides with new P/N KSF0606P. 23) Removed and installed new hydraulic auxiliary system reservoir filler cap screen P/N 25HC31A. 24) Removed existing LH airbrake cable and installed new P/N 25-CF2203-15. 25) Removed existing RH airbrake cable and installed new P/N 25-CF2203-77. 26) Removed existing interconnect airbrake cable and installed new P/N’s 25-CF2203-25 and P/N 25CF2203-75. 27) Complied with TKS visual tank inspections. No defects noted 28) Removed and installed new pitot left/right selector switch P/N 8A36-01-2-2N. 29) Removed right outboard maxaret P/N AC65216 S/N KR172 and installed serviceable unit P/N AC65216 S/N 30DM with 0 cycles. 30) Removed and installed new LH MLG restrictor valve P/N AIR45444. 31) Reinstalled aft emergency exit light battery power supply P/N 60-0304-51 S/N 27720 inspected by Duncan Aviation CRS #JGVR194F under work order # FHD9A. 32) Reinstalled fwd emergency exit light battery power supply P/N 60-0304-51 S/N 27906 inspected by Duncan Aviation CRS #JGVR194F under work order # FHD9A. 33) 24 Month Certification of the #1 Pitot/Static System: 1. The #1 ADC (P/N 7000700-668, S/N 88092843) and Static System Test required by 14 CFR 91.411 and Transponder Tests, including Data Correspondence, required by 14 CFR 91.413 have been performed and found to comply with 14 CFR Part 43, Appendix E and F. a. The #1 ADC was tested to 45,000 feet on 02/17/06 b. The #1 Transponder was tested on 02/17/06 c. The #1 Encoder Data Correspondence was tested to 45,000 feet on 02/17/06 d. The S5 Static System was Leak Tested on 02/17/06 34) 24 Month Certification of the #2 Pitot/Static System: 1. The #2 ADC (P/N 7000700-668, S/N 88123056) and Static System Test required by 14 CFR 91.411 and Transponder Tests, including Data Correspondence, required by 14 CFR 91.413 have been performed and found to comply with 14 CFR Part 43, Appendix E and F. a. The #2 ADC was tested to 45,000 feet on 02/17/06 b. The #2 Transponder was tested on 02/17/06 c. The #2 Encoder Data Correspondence was tested to 45,000 feet on 02/17/06 d. The S6 Static System was Leak Tested on 02/17/06 35) 24 Month Certification of the Standby Static and Altimeter System: 1. Tested and inspected the standby altimeter and static system IAW 14 CFR 91.411 (a) (1) and found to comply with 14 CFR 43 Appendix E Paragraph (b). This system and/or unit is not integrated into an encoding source. a. The Standby Altimeter P/N WL1605AM2, S/N AF125 was tested to 45,000 feet on 02/17/06. b. The S8 Static System was Leak Tested on 02/17/06 36) Reinstalled HF control unit adapter P/N 071-1268-01, S/N 1690 repaired by Duncan Aviation, CRS #JGVR194F under work order #FHD9A. 37) Reinstalled HF receiver exciter P/N 064-1015-01, S/N 26960 inspected by Duncan Aviation, CRS #JGVR194F under work order #FHD9A. 38) Reinstalled HF control P/N 071-1274-01, S/N 2050 inspected by Duncan Aviation, CRS #JGVR194F under work order #FHD9A. 39) Removed and installed new lavatory oxygen mask P/N C351-2000-205. Date of Mfg: 10/18/05. 40) Repaired LH engine HP pipe per Raytheon Aircraft Company Standard Repair SR-HK-00021 Rev B approved by FAA Form 8110-3 dated 11/04/04. 1. Performed fluorescent penetrant inspection of repaired LH HP pipe, no crack indications found. 41) Performed center aisle floorboard visual inspection; no defects noted. 42) Replaced the following main entry door hardware with new hardware: 1. Bump stop P/N 25FC6553 2. Lower bump stop pin P/N SP4YB23
- 89. 3. Lower bumpstop collar P/N SP121C 4. Distance tube P/N 25FC7475-21 5. Lower attach pins P/N SP121G and P/N SP113G17 43) Repaired fuel leaks consisting of 188 wing fasteners on LH top, 133 wing fasteners on RH top, 20 wing fasteners on LH lower and 39 wing fasteners on RH lower. 44) Replaced existing floor panels F84 and F67 with new floorboard fabricated from NL-410-10233- 250A. Work performed IAW BAe 800 SRM Ch 51-42-00, 51-25-00 and 51-20-11. III) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Removed #2 ADC P/N 7000700-968, S/N 88123056 and reinstalled same unit as P/N 7000700-668, S/N 88123056 modified by Honeywell, CRS #LV2R992K under work order #5000307460 dated 01/16/06. (Unit modified per Raytheon Service Bulletin 34-3110; FAR 91.411 complied with, unit tested to 60,000 feet 01/16/06). B) Reinstalled CD-850 control head P/N 7513000-902, S/N 136 repaired by Honeywell, CRS #FGNR677K under work order #5000317534 dated 01/19/06. C) Removed #2 RMU P/N 7012100-806, S/N 88030146 and installed RMU P/N 7012100-806, S/N 89010294 repaired by Honeywell, CRS #FGNR677K under work order #D300966 dated 12/13/04. IV) Service Bulletins and Service Information: A) Completed the following British Aerospace/Raytheon Aircraft Service Bulletins: Honeywell SB 965-1076-XXX-34-59 (EGPWS) Software Upgrade from P/N 206-206 S/N 2069. P/N installed after modification 965-1076-001-222-222 S/N 2069. Honeywell SB 965-1076-34-66 (EGPWS) Software Upgrade to change to -222 Mod 1. Honeywell SB 965-1076-34-68 (EGPWS) to change Terrain Database to 441. 8130 RECORD REFLECTS IRS FAN FILTER CARTRIDGE INSTALLED NEW, PN 26000790-101 V) Researched Airworthiness Directives and had the following results: A) Completed Airworthiness Directives: 1) AD 2006-01-04 Amendment 39-14443, effective date February 22, 2006 “Fan Operated Venturi”. Inspected current part number installed, found AD not applicable due to part number installed. B) Found the following Airworthiness Directives are “Not Applicable, affected equipment is currently not installed”: 77-02-08 78-14-09 89-02-05 93-09-07 2001-14-51 2005-01-19 2005-07-27 2005-11-05 2005-20-26 2005-25-08 The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9A and #FHD9B. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 I certify this Aircraft has been inspected in accordance with a A1-A6, B1-B12, C1-C12, D1-D12, E1-E12 & F1-F12 Inspection to comply with the requirements of FAR 91.409 f (3) and is approved for return to service. Details on file under Work Order #FHD9A. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 VI) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Removed existing Flight Director System and installed new Honeywell Primus EPIC CDS/R in support of Duncan Aviation, Inc. DAS STC Project # ST4449WI-T. 1) Removed components: Item P/N S/N #1 SG -818 7011674-119 88080266 REMOVED #2 SG-818 7011674-119 01071853 REMOVED Pilot HSI 7003110-902 88072836 REMOVED Stand-By Horizon Gyro H341AGM1 5057 REMOVED MFD Controller 7007062-922 88090477 REMOVED Pilot ADI 7003110-902 85120929 REMOVED Copilot TAS Temp Indicator 4031609-903 88110648 REMOVED Pilot Inst Remote 7011345-902 88110252 REMOVED Copilot Inst Remote 7011345-912 87120166 REMOVED Pilot Display Control 7005819-708 89011050 REMOVED Copilot Display Control 7005819-708 88080903 REMOVED Copilot ADI 7003110-902 88113107 REMOVED
- 90. Copilot HSI 7003110-90288072831 REMOVED MFD 7003110-902 88123237 REMOVED RMI (copilot) 4002963-445 88104172 REMOVED Copilot Altimeter 4016341-906 88125262 REMOVED Symbol Generator 7011675-119 94050613 REMOVED Pilot EFIS Cooling Fan & Mount 011035 SK1392 REMOVED Copilot EFIS Cooling Fan & Mount 011035 SK5511 REMOVED Nose Compartment Fan Monitor NSN NSN REMOVED MG Fan 011035 4574 REMOVED EFIS Fan Monitor Box NSN NSN REMOVED Mapco #2 80037-110V 3690 REMOVED #1 Audio Headphone Panel (Left) DECU-2B 8812191 REMOVED #2 Headphone Panel (Left) DECU-2B 8812192 REMOVED EGPWS 965-1076-001-206-206 2069 REMOVED #1 FMS NZ-2000 7018879-03014 97011278 REMOVED #2 FMS NZ-2000 7018879-03014 96121251 REMOVED #1 RNZ-850 NAV 7510100-711 88020121 REMOVED #2 RNZ-850 NAV 7510100-711 88080165 REMOVED Installed components: Item P/N S/N Status #1 IC-1080 (LH nose) 7017000-20703 5117339 New #2 IC-1080 (RH nose) 7017000-20703 5107247 New #1 DU-1080 (Pilot) 7023460-02004 6022858 New #2 DU-1080 (Copilot) 7023460-02004 6022860 New #3 DU-1080 (MFD) 7023460-02004 6022859 New DC-550 (Pilot) 7016986-115 05086070 New DC-550 (Copilot) 7016986-115 05086071 New RI-553 (Pilot CRS/HDG) 7016954-937 01041109 New RI-553 (Copilot CRS/HDG) 7016954-935 06010001 New MC-800 (MFD CTL) 7007062-966 06013208 New IM-600 (#1 config module) 7025973-02401 5113864 New IM-600 (#2 config module) 7025973-02401 5113865 New MT-1080 (Pilot display rack) 7024324-902 NSN New MT-1080 (Copilot display rack) 7024324-902 NSN New MT-1080 (MFD display rack) 7024324-902 NSN New MT-500 (#1 IC-1080 rack) 7026797-901 NSN New MT-500 (#2 IC-1080 rack) 7026797-901 NSN New EPGWS 965-1076-001-222-222 2069 Modified (ref Honeywell Service Bulletins) Attitude Indicator 501-1197-32 PN ID in Duncan drawings: AI-804BJ 5610 Overhauled by L-3 Communications Avionics Systems, Inc., CRS #NN2R037L, under work order #263313 dated 01/26/06. #1 FMS NZ-2000 7018879-03022 97011278 Modified by Honeywell Inc. Air Transport Systems Phoenix AZ Service Report dated 02/09/06.
- 91. #2 FMS NZ-20007018879-03022 96121251 Modified by Honeywell Inc. Air Transport Systems Phoenix AZ Service Report dated 02/09/06. #1 RNZ-850 NAV 7510100-731 88020121 Modified by Honeywell, CRS #FGNR677K under work order #500313005 dated 01/19/06. #2 RNZ-850 NAV 7510100-731 88080165 Modified by Honeywell, CRS #FGNR677K under work order #5000313002 dated 01/18/06. 2) Electrical aspects were completed in accordance with Duncan Aviation Drawing # 051005003 Rev A. 3) Mechanical aspects were completed as defined in Duncan Aviation Engineering Change Order #060213008 dated 02/13/06. 4) System was ground function tested satisfactorily IAW Document #050809029 Test 6.7. 5) Alteration performed on Work Order #FHD9B. 6) The aircraft equipment list was revised to reflect this installation. 7) The aircraft weight and balance record has been revised. 8) Replaced Coffee Thermos PN 80037-110, SN 29502, installed spigot reseal kit, PN 25- 0446k, SN 29503 (based on 8130 records). The above Honeywell Primus EPIC CDS/R System installation in support of Duncan Aviation, Inc. DAS Project # ST4449WI-T and associated equipment has been inspected and determined to be airworthy and in a condition for safe operation. A detailed record is on file under Work Order #FHD9B. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 February 27, 2006 Reg. # NXXXX Date: March 1, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5719.8 Landings: 3850 APU HOBBS: 2075.9 VII) Performed the following Manufacturer’s Recommended Maintenance items in accordance with Raytheon Hawker 800 and BAe 125 Series 800A and 800 B Aircraft Flexible Maintenance Schedule Revision 9: A) Component Requirements: 1) 5 Years from Fill Date, Overhaul of Turbomach Auxiliary Power Unit Fire Extinguisher. 1. Removed APU fire bottle P/N 30402104, S/N 23614131 and installed fire bottle P/N 30402104, S/N 20376B2 overhauled by Pacific Scientific, CRS #P94D580N under work order #512233 dated 02/22/06. Hydrostatic test next due 02/2011; cartridges P/N 13083-5 S/N ESD05L136-001, S/D 11/05 (2-each). The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9A. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 Reg. # NXXXX Date: March 9, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5721.8 Landings: 3851 I) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Reinstalled IC-1080 #1 P/N 7017000-20703, S/N 05107247 and #2 IC-1080 P/N 7017000-20703, S/N 05117339
- 92. in support ofDuncan Aviation, Inc. DAS STC Project # ST4449WI-T. The above Honeywell Primus EPIC CDS/R System installation in support of Duncan Aviation, Inc. DAS Project # ST4449WI-T and associated equipment has been inspected and determined to be airworthy and in a condition for safe operation. A detailed record is on file under Work Order #FHD9B. Signed___________________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX March 9, 2006 Reg. # NXXXX Date: 29 June 2006 Make: Raytheon Model: Hawker 800A S/N: 2581XX TAT: 5738.0 Landings: 3863 I certify that the prescribed flight test, as specified in Duncan Aviation Flight Test Procedure, Document number 050809026 Rev. Ǿ, has been completed and the aircraft is controllable throughout its normal range of speeds and throughout all maneuvers to be executed, has no hazardous operational characteristics or design features and is safe for operation. Signed_____________________________________________________ Name: Sam S. Douglass JR. Certificate # ATP 1724615 Reg. # NXXXX Date: June 23, 2006 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5730.0 Landings: 3855 Research and Development Operating Limitations changed to Rev. A, dated 6-23-06. Flight Limitations for flight hours 0 through 11 revised and Expiration Date of R & D operation is extended to July 31, 2006. Operating Limitations, Experimental, Research and Development Rev. A dated 6-23-06 has been attached to the Special Airworthiness Certificate, FAA Form 8130-7. Thomas L. Seidl Designated Airworthiness Representative DARF501357CE 6/23/06 Reg. # NXXXX Date: __6/29/06________ Work Order: __________ Make: British Aerospace Model: BAE series 800A S/N: 2581XX TAT: ________ Landings: __________ A) After satisfactory flight evaluation, Honeywell Primus EPIC CDS/R System installed under Duncan Aviation DAS project #__________ is approved per Duncan Aviation STC #______________. 1) FAA Approved Flight Manual Supplement, Duncan Aviation document # _____________ Rev _____ has been inserted into the Airplane Flight Manual. 2) Instructions for Continued Airworthiness, Duncan Aviation document # ______________ Rev ___ has been provided to the operator. 3) Reference FAA form 337 dated ____________. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #____________. Signed_____________________________________________________
- 93. For Duncan AviationCRS JGVR194F Phone: 800-228-4277/ 6/29/06 7/21/06 Reg. # NXXXX Date: July 21, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX TAT: 5730.0 Landings: 3855 APU TT: 2075.9 (Events: 6057) I) Performed the following Manufacturer’s Recommended Maintenance items in accordance with Raytheon Hawker 800 and BAe 125 Series 800A and 800 B Aircraft Flexible Maintenance Schedule Revision 9: A) Minor Inspections: 1) 050020: Thrust Reverser Inspections a) 150-200 Hour LH and RH Dee Howard Thrust Reverser Inspection b) 050020: 150 / 300 / 600 / 1200 Hour Left / Right Thrust Reverser i) Performed eddy current inspection of external surfaces of door link rods and welded areas, door fitting link attach lugs, and hinge pivot fitting IAW Dee Howard Maintenance Manual. Inspection revealed no crack indications. B) Structural Inspections 1) 550015: 2 Year Left/Right Elevator Mass Balance Weight Inspection. C) Out Of Phase Inspections: 1) 320036: 75 Landing Left/Right Inboard/Outboard Brake Unit Wear Check 2) 340015: Static Plates Inspection (RVSM Requirement). a) Reinstalled Static plates LH P/N E4202Y/1 S/N 1117E and RH P/N E4202Y/2 S/N 1076E after paint. D) Component Requirements: 1) 6 Year Underwater Locator Beacon Overhaul a) Removed P/N DK100 S/N DG3146 and installed P/N DK100 S/N DP6948 overhauled by Dukane Corporation CRS# D3KR791J under work order 508332 dated January 24, 2006. Note: Battery due replacement: 04/2012 2) #1 / #2 Battery Service. a) Reinstalled #1 Main Battery P/N 9750W0640, S/N 3227W0014 inspected by Duncan Aviation, CRS #JGVR194F, under work order # FHD9G. b) Reinstalled #2 Main Battery P/N 9750W0640, S/N 3227W0015 inspected by Duncan Aviation, CRS #JGVR194F, under work order # FHD9G. 3) Removed #4 Emergency Power Supply Battery P/N RG-126, S/N CBC-404425 and installed new battery P/N RG-126, S/N 40126243 inspected by Duncan Aviation, CRS #JGVR194F, under work order # FHD9G. 4) Reinstalled FWD Emergency exit light battery P/N 60-0304-51 S/N 27906 inspected by Duncan Aviation CRS #JGVR194F under work order FHD9G. 5) Reinstalled AFT Emergency Lights Power Supply P/N 60-0304-51, S/N 27720 repaired by Duncan Aviation, CRS #JGVR194F, under work order # FHD9G. 6) 5 Year Portable Oxygen Cylinder Overhaul. a) Reinstalled P/N 176965-SMB3 S/N 620814 overhauled by Compressed Aviation Gases CRS# OD1R370K under work order 0405042 dated May 14, 2004. Next Hydro due: May 2009 7) 5000 Landing/12 Year Left Main Landing Gear Assembly Overhaul: a) Removed Left Leg Assembly P/N 25-8UM1-181A, S/N DHL/DH/1503 and installed P/N 25-8UM523-181A S/N DHL/DH/1503 overhauled by Duncan Aviation CRS# JGVR194F on work order FHD9G. i) Upper Torque Link P/N 25-9UM9-13A, S/N 2908DA (CSN: 3855) ii) Lower Torque Link 25-9UM11-17A, S/N 2909DA (CSN: 3855) iii) Upper Casing 25-8UM169-31A, S/N BB789 (CSN: 3855) iv) Retraction Arm P/N 25-8UM63-1A, S/N 2910DA (CSN: 3855) v) Retract Arm Pin P/N 25UM787, S/N 2911DA (CSN: 0.0) vi) Plunger Tube P/N 25-8UM5, S/N BB157L. (CSN: 3855) vii) Complied with Mod 253804A. 8) 5000 Landing/12 Year Left Main Gear Side Stay Assembly Overhaul: a) Removed left Sidestay P/N 25-8UM3-125A, S/N DHL/DH/1481 and installed P/N 25-8UM3-209A S/N 1481 overhauled by Duncan Aviation CRS# JGVR194F on work order # FHD9G. i) Upper Arm P/N 25-8UM71/3, S/N BB3L. (CSN: 3855) ii) Lower Arm P/N 25-8UM73/1, S/N BB50. (CSN: 3855) iii) Distance Pin P/N 25UM423, S/N 2959DA. (CSN: 0) iv) Pivot Assembly Bolt P/N 25UM153A, S/N 2926DA (CSN: 3855) v) Complied with Mods 253549A, 253597A, 253800AB, 7239, 7042 9) 5000 Landing/12 Year Right Main Landing Gear Assembly Overhaul: a) Removed Right Leg Assembly P/N 25-8UM1-182A, S/N DHL/DH/1490 and installed strut P/N 25-8UM523-182A S/N DHL/DH/1490 overhauled by Duncan Aviation CRS# JGVR194F on work order FHD9G. i) Upper Torque Link P/N 25-9UM9-13A, S/N SAM5605 (CSN: 3855) ii) Lower Torque Link P/N 25-9UM11-17A, S/N 2912DA (CSN: 3855) iii) Casing P/N 25-8UM169-32A, S/N BB711 (CSN: 3855) iv) Retraction Arm P/N 25-8UM63-2A, S/N 2913DA (CSN: 3855) v) Retraction Arm Pin P/N 25UM787, S/N 2914DA (CSN: 3855)
- 94. vi) Plunger TubeP/N 25-8UM6, S/N BB167R (CSN: 3855) vii) Complied with Mods 253804A. 10) 5000 Landing/12 Year Right Main Gear Side Stay Assembly Overhaul: a) Removed Right Sidestay P/N 25-8UM3-126A, S/N DHL/DH/1488 and installed P/N 25-8UM3-210A S/N DHL/DH/1488 overhauled by Duncan Aviation CRS# JGVR194F on work order FHD9G. i) Upper Arm P/N 25-8UM71-4, S/N DHL424. (CSN: 3855) ii) Lower Arm P/N 25-8UM73-2A, S/N BB265 (CSN: 3119) iii) Distance Pin P/N 25UM423, S/N 2960DA. (CSN: 0) iv) Pivot Assembly Bolt P/N 25UM153A, S/N 2961DA (CSN: 0) v) Complied with Mods 253549B, 253597B, 253800A/B, 11) 5000 Landing/12 Year Nose Gear Assembly Overhaul: a) Removed Nose Landing Gear Strut P/N 25-8UN1-357A, S/N DHL/DH/742 and installed strut P/N 25-8UN1-636A S/N DHL/DH/742 overhauled by Duncan Aviation CRS# JGVR194F on work order FHD9G. i) Pivot Pin P/N 25UN645A S/N R336710 (CSN: 3855) ii) Lower Jack Pivot Pin P/N 25UN597 S/N R543858 (CSN: 3855) iii) Main Casing Bolt P/N 25UN603 S/N R514022 (CSN: 3855) iv) Plunger Tube P/N 25 UN649 S/N BA486 (CSN: 3855) v) Axle Barrel P/N 25-8 UN257-27A S/N BA930 (CSN: 3855) vi) Upper Torque Link P/N 25-8 UN267-3A S/N BB805 (CSN: 3855) vii) Lower Torque Link P/N 25-8 UN269-27A S/N 663 (CSN: 3855) viii) Torque Links Pick-up Sleeve P/N 25-8 UN455-9, S/N BA964 (CSN: 3855) ix) Connecting Rod P/N 25 UN113A/B S/N R325199 (CSN: 3855) x) Drag Strut Pick-UP P/N 25-8 UN265-1A, S/N BA886 (CSN: 3855) xi) Trunnion Bolts P/N DHS1432-28J (CSN: 0.0) xii) Steering Pin P/N 25 UN605, S/N 2866DA (CSN: 0.0) xiii) Steering Main Member P/N 25-8 UN431-1A, S/N R550258 (CSN: 3855) xiv) Steering Main Member P/N 25-8 UN431-2A, S/N R565552 (CSN: 3855) xv) Steering Sleeve P/N 25-8 UN439-1A, S/N BB22 (CSN: 3855) xvi) Jack Pick-up P/N 25-8UN263-1A, S/N R344921 (CSN: 3855) xvii)Reinstalled steering actuator P/N AIR45396/5, S/N LK0472 after repair performed by Duncan Aviation CRS# JGVR194F on work order FGHHA. xviii) Complied Mod 253803A. Spigot Ring PN 25-8un429-5 chromed/repaired per Duncan records 12) 5000 Landing/12 Year Nose Landing Gear Drag Stay Assembly Overhaul: a) Removed Nose Gear Drag Stay P/N 25-8UN3-143, S/N DHL/DH/732 and installed P/N 25-8 UN3-143A, S/N DHL/DH/732 overhauled by Duncan Aviation CRS# JGVR194F on work order FHD9G. i) Bridge Casting P/N 25-8 UN487-1A, S/N BA101. (CSN: 3855) ii) Mount Bolts P/N A102-21J. (CSN: 0.0) iii) NOTE: Out of Phase Inspection #320037 Nose Landing Drag Stay Clearances Check is due within the next 25 to 50 landings. 13) 4000 Landing Left/Right Main Landing Gear Sequence Valve Overhaul. a) Removed LH Sequence valve P/N AIR48540/1 S/N LK8801180 and installed P/N AIR48540/1 S/N LK8708628 overhauled by Midcoast Aviation Inc CRS# RO3R822L under work order 523145 dated April 4, 2006. b) Removed RH Sequence valve P/N AIR48540/1 S/N LK8802247 and installed P/N AIR48540/1 S/N APB93272 overhauled by Airight Products Inc CRS# OU2R070L under work order 508890 dated March 24, 2006. II) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Installed “Airshow 400” IAW “Duncan Aviation” Drawing # 060323011 and FAA Approved Document Dun-A-1 Rev10. 1) Removed components: Item P/N S/N Entertainment System AM80C-12 01473 Entertainment System AM80C-12 03608 2) Installed components: Item P/N S/N Status Airshow 400 R/T 920050 1145 Modified by Rockwell Collins, Inc., CRS #NZ2R049L, under PO #510499 dated 01/30/06. (NOTE FOR INFO: SW MOD STATUS FOR THIS UNIT: F, G, H, J, K, M, N, P, T, Y, Z. Out SB config: F, G, H, J, K, M,N, P, T, Y, AD) CMOS BATTERY: 3.6V, TL-5186P, PN 103001 Airshow Controller 922000-2 248 Serviceable 3) The manufacturer’s continued airworthiness inspection requirements do not change with this alteration. 4) Reference FAA Form 337 dated July 21, 2006. B) Removed existing “Entertainment” systems and installed “Honeywell/Baker MH series Audio/Video” system IAW “Duncan Aviation” Drawing #’s 060323011, 060330013, 060323010, 060330014, and 060711012. 1) Removed components: Item P/N S/N
- 95. Baker Chime BoxM1050-A382-01 8812145 Equalizer EQL/CV-1 24461 Stereo Relay Box N/A N/A Audio Amp AM80C-12 01473 Audio Amp AS80C-12 03608 CD Player SDX-1150 104877 Audio Amp M1080B 881233 2) Installed components: Item P/N S/N Status Rosen Monitor 1042-005 0604F003 New Flight Display DVD Player FD932DVD-4 55180 New M1021D Audio AMP 990-4132-005 06040027153 New M1084 Audio AMP 990-3393-001 06010024547 New ICM1000 Temp Module 990-8000-002 06050027644 New MHP Cabin Management System 990-6820-001 06040026746 New MHEC Cabin Management System 990-6801-002 06050027649 New 3) The manufacturer’s continued airworthiness inspection requirements do not change with this alteration. 4) Reference FAA Form 337 dated July 21, 2006. C) The following was installed under Work Order # FHD9B in support of Duncan Aviation DAS Project# ST4449WI-T. 1) Honeywell Primus Epic CDS/R a) Removed components: Item P/N S/N #1 IC-1080 7017000-20703 5117339 #2 IC-1080 7017000-20703 5107247 RI-553 7016954-937 01041109 b) Installed components: Item P/N S/N Status #1 DC-550 Display Controller 7016986-108 06036287 New #2 DC-550 Display Controller 7016986-108 06036289 New #1 RI-553 Remote Inst Controller 7016954-938 06032390 New MC-800 MFD Controller 7007062966 06013208 New IC-1080 Integrated Avionics Computer 7017000-21701 ENG-009 New IC-1080 Integrated Avionics Computer 7017000-21702 05047077 New Nav Computer (FMS NZ- 2000) 7018879-03022 96121251 New Nav Computer (FMS NZ- 2000) 7018879-03022 97011278 New Display Unit #1 (DU1) 7023472-902 86021021 New Display Unit #2 (DU2) 7023460-902 06021022 New Display Unit #3 (DU3) 7023460-902 06021023 New c) All systems were ground function tested satisfactorily IAW Duncan Aviation Ground Test Procedure. d) Alteration performed on Work Order #FHD9B. e) The aircraft equipment list was revised to reflect this installation f) The aircraft weight and balance record has been revised. g) The above Honeywell Primus Epic CDS/R System installation under Duncan Aviation DAS Project #ST4449WI-T and associated equipment has been conformed and determined to be in a condition for safe operation. D) Reinstalled Copilot WX Controller P/N 7008471-804, S/N 88100501 repaired by Honeywell, CRS #LV2R992K, under work order #5000392808 dated 05/12/06. E) Removed and installed new PS2 Bus Circuit Breaker CB12 P/N MS25244-25. F) Reinstalled PS9 Dimmer Module (U) P/N 25-8NF761-41 repaired by Duncan Aviation, CRS #JGVR194F, under work order FHD9B. G) Removed Flight Guidance Controller P/N 7011702-916 S/N 89050190 and installed P/N 7011702-916 S/N 88060148 repaired by Honeywell CRS# LV2R992K under work order 5000457734 dated May 5, 2006. H) Reinstalled Chime warning unit P/N M1285AC S/N 881020 repaired by Baker Electronics CRS# OJ4R416M under work order 524758 dated April 17, 2006.
- 96. I) Removed TCASunit P/N 4066010-910 S/N 920811. III) The following was performed by Duncan Aviation under Work Order #FHD9E: A) Reinstalled the following cabin seat actuators overhauled by Aviation Fabricators CRS #GVRR304K under work order #19735/13430 Dated May 1, 2006: Seat Part Number Serial Number LH/1 SLO2300-21 29273 LH/2 SLO2300-21 29274 LH/3 SLO2300-21 29275 RH/1 SLO2300-21 29276 RH/2 SLO2300-21 29277 B) Reinstalled Seat belts repaired by Aircraft Belts Inc CRS# YB1R632K under work order 69147 dated May 15, 2006 as follows: Part Number Quantity MDA2131-A-013 5 1101612 2 0108168 1 C) Performed a complete interior refurbishment. The materials used meet the Test Criteria of Part 25 Appendix F Part I (a) as required by FAR 25.853 (a) and FAA form 8110-3 detailing the specific test performed and approving the results have been provided to the operator for each of the materials used in this refurbishment. (Reference Interior 8110-3 binder). The Passenger Seat cushions and seatbacks were refurbished and tested in support of FAA Project Number SP0256WI-Q-DA1848 approved per FAA Form 8110-3 dated 05/28/06 and found to meet the Test Criteria of Part 25 Appendix F Part II (a) as required by FAR 25.853 (c) (fire blocking qualifications for cabin seating materials. D) Modified existing aircraft interior IAW Duncan Aviation drawings and Duncan Aviation engineering change orders (ECO) as follows: Description Drawing/ECO # Drawing Rev. FAA Form 8110-3 Approval Date Placard Installation 060607016 A July 18, 2006 Floorplan 060607015 A July 18, 2006 (ECO) Potty Modification 060601013 N/A Deemed Minor by Duncan Aviation Eng. (ECO) Lav Modifications 060601012 N/A Deemed Minor by Duncan Aviation Eng. (ECO) Speaker Install 060601011 N/A Deemed Minor by Duncan Aviation Eng. Switching/Outlet Install (ECO) 060601010 N/A Deemed Minor by Duncan Aviation Eng. Subwoofer Assembly & Install (ECO) 060601009 N/A June 28, 2006 Subwoofer Cabinet Assembly & Install 040831001 Ø June 28, 2006 (ECO) LH Fwd Galley Mods 060601008 Ø Deemed Minor by Duncan Aviation Eng. RH/LH Armrest Cabinet Assy. 051031009 Ø June 28, 2006 Divan/Armrest Cabinet Installation 051206014 A June 28, 2006 Cardtable Modification 051014003 Ø June 28, 2006 Headliner 02 Box Installation (ECO) 8130 RECORD SHOWS OXYGEN MASK DROP DOWN BOX P/N 175222-11 051107017 N/A Deemed Minor by Duncan Aviation Eng. (ECO) Entertainment Equipment Install 051116008 N/A Deemed Minor by Duncan Aviation Eng. RH Aft PSU Panel Extension (ECO) 051031010 N/A Deemed Minor by Duncan Aviation Eng. Lower Sidewall Modification (ECO) 051031011 N/A Deemed Minor by Duncan Aviation Eng. Lav Door Modification (ECO) 060615005 N/A June 28, 2006 Fire Extinguisher Installation (ECO) 060615004 N/A June 28, 2006 Cardtable Mount Relocate & Air Plenum Mod. 060404003 Ø June 28, 2006 AC Outlets (2ea) 1374-1W 060512003 Deemed Minor by Duncan Aviation Eng. RH FWD Monitor Installation 051031012 Ø June 28, 2006 E) Complied with Pilot’s and Copilot’s IPECO Crew Seat Bottom and Backrest Foam Replacement IAW Duncan Aviation ECO #060601015, dated 06/01/06, approved by FAA Form 8110-3 dated 06/06/06. 1) Pilot’s Seat P/N 3A026-0013-00-2, S/N 10533. 2) Copilot’s Seat P/N 3A026-0014-00-2, S/N 10535. 3) The materials used meet the Test Criteria of Part 25 Appendix F Part I as required by FAR 25.853 (a). 4) The manufacture’s continued airworthiness inspection requirements do not change with this repair. 5) Reference FAA Form 337 dated July 20, 2006. F) Installed new baggage nets fabricated by Cargo Systems Inc IAW Aerodesign Aircraft Engineering Report #6246-1/IR and 1911-2/S to include the following: 1) P/N CS-HS800-71 S/N 062431, P/N CS-HS800-72 S/N 062432, P/N S3HH33BB12AB-17. 2) Reference FAA Form 337 dated July 20, 2006 G) Installed new Cabin seat switches in side wall panels IAW Duncan Aviation Minor ECO# 060601010 to include the following: Position Part Number Serial Number
- 97. RH 1 990-9107-00606050027685 RH 2 990-9107-006 06050027688 RH FWD divan armrest 990-9107-006 06050027684 Center Divan seat 990-9107-006 06050027682 RH AFT Divan Armrest 990-9107-006 0605002683 LH 1 990-9107-006 06050027686 LH 2 Top 990-9204-032 06050027753 LH 2 Bottom 990-9206-009 06050027690 LH 3 990-9107-006 06050027687 Entry Switch 990-9102-080 06050027651 Galley Switch 990-9103-061 06050027650 Lav Switch 990-9105-037 06050027675 IV) The following was performed by Duncan Aviation under Work Order #FHD9F: A) Completed overall strip and paint of aircraft fuselage, nose, and tail following Duncan Aviation Approved Procedures Manual AP-34-002-96. 1) Overall Color Snow White #570-566 (Jet Glo) 2) Stripe Color Flag Red #P-1202HL (DuPont) 3) Stripe Color Gloss Black #P-2333HL (DuPont) NOTE: 9/12/2006 log entry states: "....Painted wings using Matterhorn White #570-535 (Jet-Glo)" B) Ailerons were removed, painted, and balanced per Raytheon 800A SRM 51-60-00 and reinstalled per Raytheon 800A MM 27-10-31. C) Elevators were removed, painted, and balanced per Raytheon 800A SRM 51-60-00 and reinstalled per Raytheon 800A MM 27-30-22. D) Rudder was removed, painted, and balanced per Raytheon 800A SRM 51-60-00 and reinstalled per Raytheon 800A MM 27-20-23. E) Disconnected and reinstalled aft nose gear door for painting access per Raytheon 800A MM 32-20-42. F) Installed required external placards per British Aerospace GEOG Ref. #25-8GA-55. G) Installed clear vinyl radome erosion boot, P/N PM-81, per Duncan Aviation Paint Shop SOP AP-34-002-96. H) Maintenance Note: Current configuration wings and flaps are primer painted. I) Performed Post Paint Gear Swing IAW Hawker 800 Maintenance Manual. J) Visual inspection of under head radiused rivet per 800 SRM Ch 51-43-00-001 Fig. 3&4. Rivets are within tolerance per 800 SRM 51-41-00. V) The following was performed by Duncan Aviation under Work Order #FHD9G: A) Weighed Aircraft using load cell weighing scales in level condition in a closed hangar. B) Reinstalled #1 Oxygen Cylinder P/N WKA37447 S/N 14510X and Reg. Valve P/N WKA31424 S/N 162 overhauled by Ameron Global Product Support CRS# RU2R148L under work order #521338 dated 04/07/06. C) Reinstalled #2 Oxygen Cylinder P/N WKA37447 S/N 560655 and Reg. Valve P/N WKA31424 S/N 1143 overhauled by Ameron Global Product Support CRS# RU2R148L under work order #521338 dated 04/07/06. D) Reinstalled #5 Emergency Power Supply Battery P/N RG-126 S/N CBC-404429 Inspected by Duncan Aviation CRS #JGVR194F under work order # FHD9G. E) Reinstalled #3 Emergency Power Supply Battery P/N RG-126 S/N CBC-404424 Inspected by Duncan Aviation CRS #JGVR194F under work order # FHD9G. F) Tested and inspected the S5 and S6 static system IAW 14 CFR 91.411 (a)(2). G) Reinstalled INS battery P/N 28002-001 S/N 10300827 inspected by Duncan Aviation CRS #JGVR194F under work order FHD9G. H) Removed External Power Over voltage Sensor P/N E311TS SN CP-06126 and installed new P/N E311TS S/N CP-050704. (8130 RECORD SHOWS SN CP-06126, SENSOR, NEW. POSSIBLY ABOVE IS TYPO AND CP-06126 INSTALLED) I) Removed LH Flap Sync. Input Arm, drilled new lever arm P/N 25-8CW383-1A, and installed with new pin P/N DHS1293-5-90. 1) Completed internal rigging of LH flap sync position transmitter per Raytheon CMM 27-50-05. J) Removed Flap Control Unit P/N 614MK2 S/N 614S231 and installed P/N 614MK2 S/N 614-G-567 overhauled by Unipak Aviation CRS# UW2R229L under work order M2262 dated January 31, 2006. K) Removed Emergency Hydraulic Press pipe assy P/N 25SF1875-71 S/N UNK and installed P/N 25SF1875-71 S/N YECLH22 inspected by Arnoni Aviation Services CRS# Y8AR872N under work order W102534 dated July 5, 2006. L) Removed Flap Sync. Receiver unit P/N 617MK4 S/N H-613 IAW Hawker 800 M/M 27-50-162 and installed P/N 617MK4 S/N U950 overhauled by Unipak Aviation CRS# UW2R229L under work order P1428 dated May 10, 2006. 1) Performed Flap function test, checked flap travels, adjusted flap position transmitter and performed AOA angle verification check. VI) Service Bulletins and Service Information: A) Completed the following Raytheon Aircraft Service Bulletins: 1) SB 32-217 “Nose Landing Gear Pivot Pin Crack Test”. Inspection was complied with during nose gear overhaul. B) Completed the following Safety Communiqué: 1) Raytheon #262 “Isle Width and Emergency Egress compliance.” VII) Researched Airworthiness Directives and had the following results: A) Completed Airworthiness Directives: 1) AD 74-08-09 R2 effective date July 29, 1996 “Lavatory Receptacles” a) Complied with Paragraph (e), no defects noted. Re-inspection per paragraph (e) is due again prior to 1,000 hours time in service (6730.0 Aircraft total time). B) Found the following Airworthiness Directives are “Not Applicable, affected equipment currently not installed”: 1) AD 2006-04-04 (effective 03/24/06) “Meggitt Model 602 Smoke Detector Lock-up.” 2) AD2006-12-20 Raytheon Aircraft Company (effective 07/03/06) “Prevent Current Limiters From Opening Just Hours After Installation”.
- 98. The above describedrepair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FHD9B, FHD9E, FHD9F and FHD9G. 8130 RECORD REFLECTS INSTALL OF NEW APU FUEL INLET FILTER, PN 211-326. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 7/21/06 07/21/06 Reg. # NXXXX Date: July 21, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX TAT: 5730.9 Landings: 3856 VIII) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Completed the installation of Collins “Airshow 400” IAW “Duncan Aviation” B) Drawing #’s 060323011. 1) Electrical aspects of the installation were completed in accordance with Duncan 2) Aviation Drawing # 060323011 approved on 8110-3 dated July 21, 2006. a) NOTE: System was provisioned for electrical see log entry dated 07/20/06. b) Mechanical aspects of alteration previously approvals documented on FAA form c) 337 dated 07/20/06. 3) System was ground function tested satisfactorily IAW Airshow Installation Manual. 4) Alteration performed on Work Order # FHD9B. 5) The manufacturer’s continued airworthiness inspection requirements do not change with 6) this alteration. 7) Reference FAA Form 337 dated July 21, 2006. 8) System currently disabled by removed by pulling and collaring circuit breakers. C) Completed the installation of “Honeywell/Baker MH series Audio/Video” system IAW “ D) Duncan Aviation” Drawing #’s 060323011, 060330013, 060323010, 060330014. 1) Electrical aspects of the installation were completed in accordance with Duncan Aviation 2) Drawing #s 060323011, 060330013, 060323010, and 060330014 approved on 8110-3 dated July 21, 2006. a) NOTE: System was provisioned for electrical see log entry dated 07/20/06. b) Mechanical aspects of alteration previously approvals documented on FAA form 337 c) dated 07/20/06. 3) System was ground function tested satisfactorily IAW Honeywell Manual 762-1033-001. 4) Alteration performed on Work Order #FHD9B. 5) The aircraft equipment list was revised to reflect this installation 6) The aircraft weight and balance record has been revised. 7) The manufacturer’s continued airworthiness inspection requirements do not change 8) with this alteration. 9) Reference FAA Form 337 dated July 21, 2006 10) System currently disabled by pulling and collaring circuit breakers. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FHD9B. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 07/21/06
- 99. Reg. # NXXXXDate: July 26, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX TAT: 5733.0 Landings: 3858 APU TT: 2088.9 (Events: 6073) IX) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Reinstalled RT-910 TCAS II Computer Unit P/N 4066010-910, S/N 92081106 repaired by ACSS Repair and Overhaul, CRS #L3ZR029X, under work order #CQ-16712 dated 07/18/06. (NOTE FOR INFO: SW MOD STATUS FOR THIS UNIT: A, B, C, D, E, G, H, J, K, L) The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FHD9B. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 7/26/06 Reg. # NXXXX Date: August 25, 2006 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5738.0 Landings: 3863 Amended the Special Airworthiness Certificate issued on February 15, 2006 to extend the expiration date to February 14, 2007. Revised the Research and Development and Market Survey Operating Limitations to extend the expiration date to February 14, 2007. Revised the Show Compliance Operating Limitations to extend the expiration date to February 14, 2007 and added limitations for the required stall flight for leading edge removal/installation during the winglet installation (STC SA01411SE) This amended Special Airworthiness Certificate, EXPERIMENTAL, is valid for one year from the original issue date and will expire on February 14, 2007. Thomas L. Seidl Designated Airworthiness Representative DARF501357CE 8/25/06 9/12/06 Reg. # NXXXX Date: September 12, 2006 Work Order: FKW3 Make: BAe 125 Model: 800A S/N: 2581XX TAT: 5738.0 Landings: 3863 I) The following was performed by Duncan Aviation under Work Order #FKW3A: A) Out of Phase Inspections: 1) 340013: 36 Month Check #1/#2/Standby Compass Swing. B) Installed Winglets, Associated Changes in Wing and Aileron Structures and Related
- 100. Systems Changes onRaytheon Aircraft Company Model BAe 125 Series 800A IAW Aviation Partners Inc., STC # ST01411SE and API Master Drawing List APH-610 Rev B: 1) Installed Components: Description: Part Number: S/N: LH winglet H800-0310-5 0043 RH winglet H800-0310-6 0043 2) No electrical deviations. 3) No mechanical deviations. 4) Instructions for Continued Airworthiness are identified under Aviation Partners Inc.: (a) Airworthiness Limitations, APH-0608, Rev. E, dated March 14, 2005 (b) Maintenance Planning Document- Non-Damage Tolerance Related Inspections (c) APH-0611 Rev. A dated January 23, 2005. (d) Structural Repair Manual Supplement APH-0602 Initial Release dated Nov.11, 2004 (e) Airplane Maintenance Manual Supplement APH-0600 Rev. F dated February 1, 2005 Reference FAA Form 337 dated August 23, 2006. C) Removed #2 flux valve P/N 7010133, S/N 88100684 and installed valve P/N 7010133, S/N 98054125 repaired by Honeywell Intl Inc., CRS# P7XR821N on work order H203804 dated 07-27-06. D) Removed RH aileron bearing plate assembly P/N 25-8WS2141-9A and installed bearing plate assembly P/N 25-8WS2141-9A, S/N 258148 overhauled by Arnoni Aviation Services, Inc. CRS# Y8AAR872N on work order W102236 dated 06-22-06. E) Installed new inbd aileron cable pulley on LH wing P/N CP48100B. F) Reinstalled hydraulic overtemp switch P/N 150T283, S/N 618 inspected by Duncan Aviation CRS# JGVR194F on work order FKW3A. G) Installed a removed serviceable LH aileron trim tab P/N 25-8WG57-47A, NSN (three hinge). Performed weight and balance check after tab installation. H) Completed the angle verification check on the LH and RH air flow sensors. I) Performed stall warning and identification system adjustment/test. J) Installed new LH Winglet LED light assembly P/N H800-0350-3, S/N 041. K) Installed new RH Winglet LED light assembly P/N H800-0350-4, S/N 041. L) Repaired right aileron P/N 25-8WG1-118A S/N DHB160 by removing corrosion from aileron frame leading edge in recessed pockets by mechanical means described in BAe 125 series 800A Structural Repair Manual Ch. 51-10-02. and Raytheon Aircraft Company Field Repair Drawing No. FR-HK-03020 approved by FAA Form 8110-3 dated August 18, 2006. Performed ultra sonic thickness inspection of blended areas applied alodine and primer to bare metal areas installed aileron frame leading edge balance weights in accordance with Aviation Partners Incorporated STC# STO1411SE instructions. Reference FAA Form 337 dated August 24, 2006. M) Balanced LH and RH ailerons. Painted wings using Matterhorn White #570-535 (Jet-Glo) II) The following was performed by Duncan Aviation under Work Order #FKW3B: A) Reinstalled FMS NZ-2000 Navigation Control Unit P/N 7018879-03022, S/N 96121251 modified by Honeywell International Inc., CRS #HQ7R766N, under work order #Y187839 dated 08/28/06. B) Reinstalled FMS NZ-2000 Navigation Control Unit P/N 7018879-03022, S/N 97011278 modified by Honeywell International Inc., CRS #HQ7R766N, under work order #Y187836 dated 08/28/06. III) Researched Airworthiness Directives and had the following results: A) Found the following Airworthiness Directives are “Not Applicable, affected equipment is currently not installed”: 1) AD 2006-16-18, AD 2006-17-13 (FROM 8130 RECORDS) REPLACED APU FUEL NOZZLE, PN 169046-1, NSN The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FJW3A. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 Inspected aircraft and found to be in a condition for safe operation and is appropriate for the purpose of showing compliance with the regulations. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX September 12, 2006 9/12/06
- 101. Reg. # NXXXXDate: September 12, 2006 Make: BAe 125-800A Model: Hawker 800A S/N: 2581XX TAT: 5739.0 Landings: 3866 I certify that the prescribed stall test requirements, as specified in British Aerospace BAe series 800A Flight Manual and Hawker 800 series Aircraft Maintenance Manual chapter 57 has been completed and the aircraft is controllable throughout its normal range of speeds and throughout all maneuvers to be executed, has no hazardous operational characteristics or design features and is safe for operation. Signed_____________________________________________________ Name: _Larry Bartlett ______ Certificate # ATP2144044 _ Reg. # NXXXX Date: September 26, 2006 Work Order: FHD9 Make: BAe 125 Model: 800A S/N: 2581XX TAT: 5739.0 Landings: 3866 I) The following was performed by Duncan Aviation under Work Order #FHD9B IN Support of Duncan Aviation FAA Project ST4449WI-T: A) Completed Duncan Aviation Company CDS/R Conformity for STC Project #ST4449WI-T, Reference FAA Form 8130-9 dated September 26, 2006 Honeywell Primus EPIC Installation: Description P/N S/N Status DU-1080 Display Unit 7023460-02004 06093736 New DU-1080 Display Unit 7023460-02004 06093729 New DU-1080 Display Unit 7023460-02004 06093737 New Integrated Computer 7017000-20703 06097714 New Integrated Computer 7017000-20703 06097692 New B) Completed Bezel Modifications for Display Installation for CDS/R: 1) Installed 2-each #8-32 C/S Screws MS24694S IAW Duncan Aviation ECO #060921012 and mechanical drawing # 050923014. C) Completed Ground Test for the CDS/R System IAW Duncan Grnd Test Doc #050809029 Rev B. II) The following was performed by Duncan Aviation under Work Order #FHD9J: A) Removed Co-Pilots seat belt buckle pn F/A 1101167-9 with new buckle pn 1101550-01. B) Installed entertainment system wiring provisions for 12” monitor in RH aft position IAW Duncan Aviation drawing #060330013(deemed minor by Duncan Engineering III) Airworthiness Directives: A) Found the following AD are “Not Applicable, affected equipment is currently not installed”: 2006-18-08 2006-19-04 Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX September 26, 2006 Inspected Aircraft and found to be in a condition for safe operation and is appropriate for the purpose of showing compliance with the Regulations. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX September 28, 2006
- 102. Reg. # NXXXXDate: September 28, 2006 Work Order: FHD9B Make: BAe 125 Model: 800A S/N: 2581XX TAT: 5743.0 Landings: 3870 Inspected Aircraft and found to be in a condition for safe operation and is appropriate for the purpose of showing compliance with the Regulations. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX September 28, 2006 Reg. # NXXXX Date: October 6, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5746.5 Landings: 3872 IV) The following was performed by Duncan Aviation under Work Order #FHD9J and #FHD9K: A) Installed 12” Rosen Monitor in Right Forward Partition and installed 15” Rosen Monitor in Forward Divan Armrest in accordance with Duncan Aviation Drawings #060929018, #060330013 And Duncan Aviation ECO #060919011: 1) Installed components: Item P/N S/N Status 12” Rosen Monitor AI-LCD121-01-1 090600921 New 15” Rosen Monitor 1500-084 0609L016 New 2) The manufacturer’s continued airworthiness inspection requirements do not change with this alteration. 3) Reference FAA Form 337 dated 10/06/06. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9J and #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 10/06/06 Date: October 08, 2006 Reg. # NXXXX Make: BAe 125 Model: 800A S/N: 2581XX TAT: 5747.1 Landings: 3873 I certify that the prescribed flight test, as specified in Duncan Aviation Inc., Flight Test Procedure, Document Number 050809026, Rev. A, has been completed and the aircraft is controllable throughout its normal range of speeds and throughout all maneuvers to be executed, has no hazardous operating characteristics or design features and is safe for operation. Signed ___________________________________________ Pilot in Command: David Groller - 3161281 10/8/06 Reg. # NXXXX Date: October 13, 2006
- 103. Make: Raytheon Model:BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5147.1 Landings: 3873 I find this aircraft meets the requirements for the reinstatement of the STANDARD Airworthiness Certificate and the inspection was performed based on the installation and modifications related to Supplemental Type Certification project ST4449WI-T, Installation of the Honeywell Primus EPIC Control Display System/Retrofit (CDS/R). Performed from February 15, 2006 to October 13, 2006 This certification process does not replace or change any due dated or times of any scheduled inspection requirements for Raytheon Bae 800A, S/N 2581XX (NA04XX). The next A1 through A6 inspection is due at 6018.9 aircraft total time or E1 through E12 inspection is due on February 27, 2007, whichever occurs first. Thomas L. Seidl Designated Airworthiness Representative DARF501357CE 10/13/06 10/16/06 Reg. # NXXXX Date: October 16, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5747.1 Landings: 3873 V) The following was performed by Duncan Aviation under Work Order #FHD9K: A) Installed Honeywell Primus EPIC Control Display System/Retrofit (CDS/R) in accordance with Duncan Aviation STC #ST01406WI-D and Duncan Aviation Drawing List #050908016 as follows: 1) Removed components: Item P/N S/N Pilot’s Altimeter 4016341-906 88075082 Copilot’s Altimeter 4016341-906 88125262 2) The Instructions for Continued Airworthiness are identified under Duncan Aviation Document #050908018 Rev Ø. A copy of the Instructions has been provided to the operator. 3) Reference FAA Form 337 dated October 13, 2006. B) The following Flight Manual Supplements are in conjunction with the Honeywell Primus EPIC Control Display System (CDS/R) and are approved on Field Approved FAA Form 337’s: 1) The existing Honeywell MK VII Enhanced Ground Proximity Warning System ( EGPWS ) Airplane Flight Manual Supplement, Garrett Aviation Document No. AFMS221 has been superseded. Duncan Aviation Airplane Flight Manual Supplement, Document No. 060614012 has been created, approved and issued to reflect the MK VII EGPWS operation as a result of the installation of a Honeywell Control Display System for Retrofit (CDS-R). The installation of the Honeywell CDS-R System is documented on a separate FAA Form 337. a) Note: The MK VII GPWS was originally installed under Garrett Aviation STC ST00837CH-D. 2) The existing Dual Honeywell FMZ-2000 FMS was upgraded to software NZ 6.X. In addition, FMS remote annunciator and wiring modifications were completed as a result of the installation of a Honeywell Control Display System for Retrofit (CDS-R). These alterations were completed in accordance with Duncan Aviation Electrical Drawing 060120015, Instrument Panel Modification Wiring Diagram, as part of the CDS-R STC development for installation in the Hawker 800A under FAA Project No. ST4449WI-T. a) FAA Approved Airplane Flight Manual Supplement, Duncan Aviation Document No. 060614011 has been inserted into the Airplane Flight Manual. b) Note: The Dual FMZ-2000 was originally installed under Duncan Aviation STC ST00545WI. c) Instructions for Continued Airworthiness (ICA) have been created concurrently with this software upgrade for the Dual FMZ-2000. A copy of the Instructions for Continued Airworthiness, Duncan Aviation Document No. 060928016 has been provided to the operator for incorporation into the aircraft inspection/maintenance program. 3) The existing Honeywell TCZ-910 (TCAS 2000) TCAS II System Airplane Flight Manual Supplement, Duncan Aviation Document No. 40005600 has been superseded. Duncan Aviation Document No. 060614013 has been created, approved and issued to reflect the TCZ-910 System operation as a result of the installation of a Honeywell Control Display System for Retrofit (CDS-R). The installation of the Honeywell CDS-R System is documented on a separate FAA Form 337. a) Note: The TCZ-910 was originally installed in accordance with STC ST00302WI. C) Installed customer supplied defibrillator P/N 3011790-000114, S/N 13349806 (mfg 2001) inside RH forward closet. Infant/child defibrillator pads expire 02/28/08; adult defibrillator pads expire 01/28/08. Note: battery expiration is on- condition as indicated by the “low battery indicator icon”. Installation of the defibrillator is deemed minor by Duncan Aviation Engineering. D) Completed 24 Month Remove/Inspect Upper and Lower TCAS Antennas for Corrosion (342561). 1) Inspected areas under upper and lower TCAS antennas IAW Instructions for Continued Airworthiness for cracks
- 104. and corrosion perDuncan Aviation Document #44504900. Re-inspection due again October-2008. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 Reg. # NXXXX Date: October 18, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5748.8 Landings: 3874 VI) The following was performed by Duncan Aviation under Work Order #FHD9K: A) Removed down wash light power supplies P/N 18-996, S/N 4622 and S/N 5283 and installed power supplies P/N18-996 S/N 7007 and S/N 1111 repaired by B/E Aerospace, CRS #EO1R120K under PO #522470 and PO #52251 {respectively} dated 08/07/06. B) Performed a compass swing, tested satisfactorily. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX October 18, 2006
- 105. Reg. # NXXXXDate: October 30, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5750.1 Landings: 3875 VII) The following was performed by Duncan Aviation under Work Order #FHD9B: A) Removed flight guidance controller P/N 7011702-916, S/N 88060148 and installed controller P/N 7011702-916, S/N 89050190 repaired by Honeywell, CRS #LV2R992K under work order #5000570940 dated 07/19/06.. VIII) The following was performed by Duncan Aviation under Work Order #FHD9K: A) Installed Limitation placard above Flight Guidance Panel per Duncan Aviation ECO #061024009 (deemed minor by Duncan Aviation Engineering). 1) Installation of placard coordinated with Wichita ACO. Placard must be maintained (viewable/legible) until further disposition by Duncan Aviation. B) Removed LH #1 upwash light power supply P/N AL-5112, S/N 5321 and installed new power supply P/N AL-5112, S/N 42063. C) Removed LH #3 upwash light power supply P/N AL-5112, S/N 5327 and installed new power supply P/N AL-5112, S/N 42065. D) Removed RH #3 upwash light power supply P/N AL-5112, S/N 5319 and installed new power supply P/N AL-5112, S/N 42067. E) Replaced RH landing light lens assembly with new lens assembly P/N 251W00129-2, S/N PPA3172. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9B and #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 Reg. # NXXXX Date: November 1, 2006Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5750.1 Landings: 3875 IX) The following was performed by Duncan Aviation under Work Order #FHD9K: A) Removed CDC controller P/N 7513000-902, S/N 136. Placarded and installed blanking plate “System Disabled”, tied off system circuit breaker per Duncan Aviation ECO# 061024009, deemed minor. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX November 1, 2006
- 106. Reg. # NXXXXDate: November 6, 2006Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5750.1 Landings: 3875 X) The following was performed by Duncan Aviation under Work Order #FHD9K: A) Removed GC-810 AFCS Control Panel system limitation placard from Co-Pilot Armrest and removed Tie wrap from Circuit breaker. B) Reinstalled CD 850 Control Head P/N 7513000-902 S/N 136 repaired by Honeywell CRS# FGNR677K under work order 5000755567 dated November 2, 2006. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX November 6, 2006 Reg. # NXXXX Date: November 8, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5750.1 Landings: 3875 XI) The following was performed by Duncan Aviation under Work Order #FHD9K: A) 12 Month Inspection of Emergency Locator Transmitter System to meet the requirement of FAR 91.207 Paragraph (d). The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX November 8, 2006 11/15/2006 AFTT CYCLES Transcribed Logbook Entry 5750.1 3875 Reg. # NXXXX Date: November 15, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5751.1 Landings: 3876 XII) The following was performed by Duncan Aviation under Work Order #FHD9K: A) Reconnected copilot’s push to talk button wire at pin 5, glareshield connector G2. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FHD9K. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 NXXXX November 15, 2006 11/15/06 11/22/2006 AFTT CYCLES Transcribed Logbook Entry 5751.1 3876
- 107. SUPPLEMENTAL LOGBOOK ENTRY Reg.# NXXXX Date: November 22, 2006 Work Order: FHD9 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5751.1 Landings: 3876 Removed and replaced #2 FMS CDU with repaired exchanged unit. Performed system operational test and system operationally checks normal. Repaired replacement CDU was ordered from Honeywell, Certificate No.: LV2R99K Dated 11/03/2006 under WO# 5000752617 and is approved for return to service P/N OFF: 7004403-902 S/N OFF: 86090164 P/N ON : 7004403-902 S/N ON: 92010631 ACTUAL LOG ENTRY HAS WRONG PN (70044003-902) AND LISTS BOTH SERIAL NUMBERS AS "OFF" I certify the above described maintenance is airworthy with respect to the work performed, per the requirements of FAR 145.213(a) and is approved for return to service. A detailed record is on file under Word Order # EBA0A Signed_____________________________________________________ For Duncan Avionics - Teterboro CRS XJRR155L NXXXX November 22, 2006 11/22/06 Reg. #NXXXX Date: January 9, 2007 Make: British Aerospace Model: BAE 125 800A S/N: NA04XX TAT: 5810.6 Landings: 3925 I find that the aircraft meets the requirements for the certification requested and have issued a Standard Airworthiness Certificate, dated R-9/19/88 for new registration number “NXXGS ”. Signed:________________________________________________________________________ Ken Norseen ODART 501013-CE for Duncan Aviation JGVR194F 800-228-4277 1/9/2007 Reg. # NXXXX Date: January 9, 2007 Work Order: FMFL Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5810.6 Landings: 3925 XIII) The following was performed by Duncan Aviation under Work Order #FMFLA: A) Re-strap/certified XPDR’S for registration change 1) Function checked per FAR43, Appendix E, para. C. No defects noted per FAR 91.411 and 91.413. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FMFLA. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 1/9/2007 Reg. # NXXGS Date: January 10, 2007 Work Order: FMFL Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5810.6 Landings: 3925 XIV) The following was performed by Duncan Aviation under Work Order #FMFLA: A) Removed #1 NZ2000 NCU P/N 7018879-03022, S/N 97011278 and installed NZ2000 P/N 7018879-03022, S/N 96091165 repaired by Honeywell CRS# under work order 5000808187 dated 12/06/2006. B) Removed #2 NZ2000 NCU P/N 7018879-03022, S/N 96121251 and installed NZ2000 P/N 7018879-03022, S/N 98082029 Modified by Honeywell CRS# LV2R99K under work order 5000816680 dated 12/13/2006. (NOTE by G. Stultz FOR INFORMATION ONLY: NEW UNITS FROM ICH REPAIR FACILITY (LV2R99K). CUSTOMER SERVICE REPS THERE ARE: Norm Newton 316-771-4508, Donna Harkness 316-771-4510 Steve Seely 4540 steveseely@honeywell.com) C) Installed a 28 VDC Aux power source IAW Duncan DWG 061228004. Deemed a minor repair per Duncan Engineering. INFO: For powering Garmin 496. Male plug pn: 206434-1, Digi-Key pn A1371-ND, Receptacle Digi- Key pn 206433-3-ND.
- 108. D) Removed defective#1 IC-1080 P/N 7017000-20703, S/N 06097692 and installed a new IC-1080 P/N 7017000-20703, S/N 06117846. E) Removed defective cockpit headset P/N 300-09623-0501, S/N 1284 and installed a new headset P/N 300-09623-0501, S/N 1481. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FMFLA. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 1/10/2007 3/14/2007 Landmark APU SERVICE RECORD ENTRY Customer: Easton S/N: H800SP 2581XX Work Order Number: 224589 ACTT: 5846.0 Date: March 14, 2007 APU Serial Number: 877641 APU Time: 2296.3 H, 6226 C APU Hobbs:4184.7 H, 6218 C 1. C/W 6mo/125hr/250cyc, 6mo/250hr/500CYC inspections IAW Sundstrand SB-T-62T-49- 77 Rev. 9. 2. Inspected and functional tested fuel restrictor p/n 179290-1 s/n 0505419. 3. Cleaned and flow tested fuel nozzle p/n 169046-1. 4. Accomplished required operational and leak checks. I certify this APU has been inspected in accordance with an 6mo/125hr/250cyc, 6mo/250hr/500CYC inspection under FAR 91-409F(3) and approved for return to service. Details under W/O# 224589, Date March 14, 2007 Signed Brian J. Zicari for LANDMARK AVIATION, CRS# GW4R221M, Augusta, GA. 30906
- 109. 3/14/2007 Landmark Aircraft Logbook Entry EastonFlying Partners DATE: March 14, 2007 Hawker 800A ACTT: 5846.0 NXXGS LDGS: 3946 S/N: 2581XX W/O#: 224589 1. C/W the following Maintenance Schedule Inspection items: 12 Month “E1-E12” Manufacturer’s routine inspection. 2. C/W the following Maintenance Schedule Minor Inspection items: 150 Hour landing gear lubrication 75 Landing brake wear check in accordance with Hawker 800 AMM chp 32-40 and determined all brakes to be within serviceable limits. 3. C/W the following MS Structural inspection requirements: 550001 1200 Hour/2 Year horizontal stabilizer rear attachment fitting. 570010 1200 Hour wing bottom skin (LH & RH) adjacent to flap outboard hinge at rib 8. 570027 4 Year wing leading edges under TKS panels. Camp code 579301 Removed panels W502 and W503, inspected wing fairing avionics seals, no defects noted and reinstalled panels W502 and W503. 4. Addressed the following Airworthiness Directives and MFG Service Bulletins: AD 93-12-04 Amendment 39-8610 Precise Flight Inc Pulselite units model 1210-2405-2 N/A by model of unit installed. SB 25-3823 Replacement of seat belt shackle N/A by seat manufacturer. SB 32-3746 R1 Main landing gear wheel tie bolt and nut retirement life. Performed minimum breakaway torque test on wheel p/n AHA1814#1 s/n LC290 & #2 s/n WW032 #3 s/n LR164 & #4 s/n SL105 tie bolts and nuts. Installed 48 each new nuts p/n FN522A524.Note: This is the 2nd tire change on s/n’s LC290 & WW032 and the 1st tire change on s/n’s LR164 & #4 s/n SL105. 5. C/W the following MS Life Limited/Component Overhaul requirements: 12 Month ELT inspection & functional test IAW requirements of FAR 91.207 para.(d) & Artex Doc. # 570-5500. Battery exp date Aug 2010 2 Year #1 and #2 navigation computer back up battery (2ea.) p/n 7020116-1 replaced with new batteries of the same p/n. Due again by Mar 2009. 2 Year Cockpit voice recorder ULB battery p/n DK100, s/n DP6948 clean and test. Note: Battery exp date Apr 2012. 3 Year Left and right shot gone indicators p/n A1003(1) removed and replaced with new indicators of the same p/n. DOM July 2006. 5 Year APU fuel pump box thermal switch p/n W1004-503(wrong pn? Actual pn installed is 160275-1, sn 144606) functional test. 5 Year APU hot section thermal switch p/n 67100-1-350F functional test. 5 Year APU generator thermal switch p/n 17343-62 functional test. 240005 Deep cycled #1 IRS backup battery p/n CA-54-1 s/n 10300827 IAW Marathon CMM.. Capacity tested #1 and #2 main battery p/n 9750W0640 s/n’s 3227W0014 & 3227W0015 in
- 110. accordance with HawkerCMM. 24-32-35. Installed 12 each new passenger oxygen masks p/n C351-2000-205 with MFG date August 2006. Installed 8 each inspected life vests p/n 0201-105 s/n C44962, p/n P0201 s/n C44932, p/n P0723E105P s/n 566053, p/n P0723E105P s/n 566043, p/n 3505-101 s/n 00806591, p/n 3505-101 s/n 00806589, p/n 3505-101 s/n LM0904911 and p/n 3505-101 s/n 00806590. Ref Safetech USA CRS# UZYR394Y FAA form 8130-3 tracking #’s AG13284 dated 03/02/2007 for inspection details. 6. Performed the following miscellaneous maintenance: Complied with first aid kit inspection. Removed inoperative bulbs 6839 in #2 fire cancel switch and installed new bulbs of the same p/n. Removed landing gear position indicator module p/n 99-230 and installed new indicator module of the same p/n. Adjusted toilet dump cable to allow proper operation. Disassembled left nose wheel assembly p/n AH52339, s/n SO063 to removed worn tire p/n 181K63-2, s/n 50480972. Performed NDT check on wheel halves and wheel bolts. Reassembled same wheel with new tire p/n 181K63-2, s/n 50610938 using new through bolt nuts 12 each p/n FN22A-428 and 6 each p/n 130909N32 in accordance with Dunlop CMM AH52339 32-44-49 and Hawker 800 AMM 32-40-21. Disassembled right nose wheel assembly p/n AH52339, s/n SO064 to removed worn tire p/n 181K63-2, s/n 50460969. Performed NDT check on wheel halves and wheel bolts. Reassembled same wheel with new tire p/n 181K63-2, s/n 50640941 using new through bolt nuts 12 each p/n FN22A-428 and 6 each p/n 130909N32 in accordance with Dunlop CMM AH52339 32-44-49 and Hawker 800 AMM 32-40-21. Replaced 2ea. missing / loose right wing vortex generators p/n 25-8WA33-2 and installed 2ea. new vortex generators in accordance with Hawker 800 AMM chp 57-10-00. Removed and disassembled #1 wheel p/n AHA1814, s/n LC290 to remove worn tire p/n 237K23- 2, s/n 52730968. Performed NDT on wheel halves and bolts with no defects noted. Assembled same wheel with new tire p/n 237K23-2, s/n 61771011 in accordance with Dunlop AHA1814 CMM 32-40- 92 R10 and Hawker 800 AMM 32-40-12-41-00. Removed unserviceable #1 main wheel inbd bearing race p/n L610510 and bearing p/n L610549. Installed new race and bearing of the same p/n’s. Removed and disassembled #2 wheel p/n AHA1814, s/n WW032 to remove worn tire p/n 237K23-2, s/n 52720948. Performed NDT on wheel halves and bolts with no defects noted. Assembled same wheel with new tire p/n 237K23-2, s/n 61731039 in accordance with Dunlop AHA1814 CMM 32-40-92 R10 and Hawker 800 AMM 32-40-12-41-00. Removed 3ea. unserviceable #2 main wheel fuse plugs p/n AH088942 and installed 3ea. new fuse plugs of the same p/n. Removed and disassembled #3 wheel p/n AHA1814, s/n LR165 to remove worn tire p/n 237K23- 2, s/n 50920914. Performed NDT on wheel halves and bolts with no defects noted. Assembled same wheel with new tire p/n 237K23-2, s/n 61721032 in accordance with Dunlop AHA1814 CMM 32-40- 92 R10 and Hawker 800 AMM 32-40-12-41-00. Removed unserviceable #3 main wheel inbd bearing race p/n L610510 and bearing p/n L610549. Installed new race and bearing of the same p/n’s. Removed 2ea. unserviceable #3 main wheel fuse plugs p/n AH088942 and installed 2ea. new fuse plugs of the same p/n. Removed and disassembled #4 wheel p/n AHA1814, s/n SL105 to remove worn tire p/n 237K23- 2, s/n 50920922. Performed NDT on wheel halves and bolts with no defects noted. Assembled same wheel with new tire p/n 237K23-2, s/n 61741021 in accordance with Dunlop AHA1814 CMM 32-40- 92 R10 and Hawker 800 AMM 32-40-12-41-00. Removed unserviceable #4 main wheel otbd bearing race p/n L610510 and bearing p/n L610549. Installed new race and bearing of the same p/n’s. Removed unserviceable cabin entrance door aft side door cap (BUMPER) p/n 25FC2943 and installed new cap of the same p/n. Replaced 8 ea. missing nut caps p/n BACC50H23 with new nut caps of the same p/n. Removed mislabeled placard on cabin oxygen valve and installed new placard reading “cabin
- 111. oxygen valve”. Removedunserviceable oxygen barometric valve p/n K38002/1, s/n 116 and installed overhauled valve p/n K38002/1, s/n 196. Operationally and leak checked normal. Ref Omnigas Systems Inc FAA form 8130-3 tracking # 115223 dated 02/19/2007 for overhaul details. Removed unserviceable cabin #4 dual oxygen mask drop down box p/n 175222-11 and installed new box of the same p/n. Leak checked and operationally checked normal. Removed left rudder bias actuator p/n ACA1218, s/n LB160 and installed overhauled actuator p/n ACA1218, s/n RN146 in accordance with H800 AMM chp 27-20-51. Ref Aero Trades Inc CRS# HH1R192K FAA form 8130-3 tracking # JA15621 dated Oct 16, 2006 for overhaul details. Removed right rudder bias actuator p/n ACA1218, s/n KS445 and installed overhauled actuator p/n ACA1218, s/n EAM193 in accordance with H800 AMM chp 27-20-51. Ref Aero Trades Inc CRS# HH1R192K FAA form 8130-3 tracking # JA15721 dated Dec 14, 2006 for overhaul details. Removed unserviceable oxygen service port p/n DC550, s/n 10605 and installed new port same p/n s/n 14969. Removed unserviceable left wing #2 TKS panel p/n 25-8WS1513-25, s/n 87-1-J33 and installed repaired panel p/n 25-8WS1513-55, s/n RM13917, operationally and leak checked normal. Ref CAV Aerospace CRS# U.145.00765 EASA Form 1 tracking # 150602 dated May 26, 2006 for repair details. Removed, repaired, treated, epoxy primed and painted left and right wing leading edges IAW Raytheon SB 57-77 R1 and repair instruction RIL no. 25WS279. Performed backflow of all wing TKS panels. Installed new reblock kit p/n 9250-0083, s/n WC00161 in #2 battery p/n 9750W0640, s/n 3227W0015, Removed unserviceable APU electric fuel pump p/n 150-00-63, s/n 0076 and installed overhauled pump p/n 150-00-63, s/n 0222. Operationally checked normal. Ref Dukes INC CRS# WU2R279L FAA form 8130-3 tracking # R66944 dated Nov 30, 2006 for overhaul details. Removed 4 ea. main entrance door tensator springs p/n N2441 DOT3 and installed new springs of the same p/n IAW 800 AMM 52-11-11. Removed 2ea. unserviceable APU start bypass valve sleeves p/n BAS160-3-4-16-12 and installed 2ea new sleeves of the same p/n. Gained access to left and right main non return valves, removed and installed same valves in correct orientation, operational and leak check normal. Repaired incorrectly wire engine sync switch to correct wiring in accordance with Hawker 800 drawing 25-8NA5-363A. Performed operational check of engine sync and APR in accordance with Hawker 800 AMM chp 71-00-00 with no defects noted. I certify this aircraft has been inspected in accordance with a “E” inspection under FAR 91.409F(3) and approved for return to service. Details under W/O# 224589 Date March 14, 2007 ACTT: 5846.0 Signed Brian J. Zicari for LANDMARK AVIATION, CRS# GW4R221M, Augusta , GA. 30906 3/14/2007 3/22/2007 AFTT CYCLES Transcribed Logbook Entry 5858.7 3961
- 112. Duncan Aviation WorkOrder: FNPB REMOVED EXISTING #1 IC-1080 (CDS-R) PN 7017000-20703 SN 06117846 REMOVED EXISTING #2 IC-1080 (CDS-R) PN 7017000-20703 SN 06097714 REMOVED EXISTING #1 PFD PN 7023460-02004 SN 06093736 REMOVED EXISTING #2 PFD PN 7023460-02004 SN 06093737 REMOVED EXISTING MFD PN 7023460-02004 SN 06093729. INSTALLED REPAIRED #1 IC-1080 PN 7017000-20703 SN 06097692 INSTALLED NEW (#2?) IC-1080 PN 7017000-20703 SN 06117845 INSTALLED REPAIRED #1 PFD PN 7023460-02004, SN 07024024 INSTALLED REPAIRED #2 PFD PN 7023460-02004, SN 07024026 INSTALLED REPAIRED MFD PN 7023460-02004, SN 07014012 SIGNED SEAN DAVENPORT FOR DUNCAN AVIATION CRS# JGVR194F 4/19/2007 AFTT CYCLES Transcribed Logbook Entry 5858.7 3961
- 113. 4/19/2007 Reg. # NXXGSDate: April 19, 2007 Work Order: FNS8 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5880.0 Landings: 3982 I. I) The following was performed by Duncan Aviation under Work Order #FNS8A: A. A) Upgraded existing Honeywell EPIC CDS/R system in accordance with Duncan Aviation STC #ST01406WI-D to Master Drawing List Rev G, and the following Duncan Drawing #’s: 051005003 Rev. E FAA Form 8100-9 dated 4/17/07, 050810012 Rev. A FAA Form 8100-9 dated 4/18/07, and 050809029 Rev. E FAA Form 8100-9 dated 4/17/07. 1. 2. 1) Removed components: Item P/N S/N Pilot’s PFD 7023460-02004 07024024 Pilot’s MFD 7023460-02004 07014012 Copilot’s PFD 7023460-02004 07024026 #1 IC-1080 7017000-20703 06097692 #2 IC-1080 7017000-20703 06117845 2. 3. 2) Installed components: Item P/N S/N Status Pilot’s PFD 7023460-02006 06093736 Inspected by Honeywell International Inc., CRS #HQ7R766N under work order #Y198784 dated 04/14/07 Pilot’s MFD 7023460-02006 06093737 Inspected by Honeywell International Inc., CRS #HQ7R766N under work order #Y198782 dated 04/14/07 Copilot’s PFD 7023460-02006 06093729 Inspected by Honeywell International Inc., CRS #HQ7R766N under work order #Y198783 dated 04/14/07 #1 IC-1080 7017000-20704 06097714 Inspected by Honeywell International Inc., CRS #HQ7R766N under work order #Y198786 dated 04/14/07 #2 IC-1080 7017000-20704 06117846 Inspected by Honeywell International Inc., CRS #HQ7R766N under work order #Y198785 dated 04/14/07 The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FNS8A. Signed__________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 4/19/2007 4/26/2007 Eng TT CYCLES Transcribed Engine #1 P-91363 Logbook Entry 5705.5 3884
- 114. Transcription from Duncanlog entry, #1 Engine, SN P-91363, AFTT 5882.6, Eng TTSN 5705.5 Cycles: 3884. 150-200 HOUR ROUTINE PERIODIC. 300-400 HOUR ROUTINE PERIODIC. 1000-1500 HOUR ROUTINE PERIODIC. 2100 HOUR MAJOR PERIODIC (MPI) 2100 HOUR PLENUM CASE. REMOVED FROM #1 POSITION. Transcription from Duncan log entry, #2 Engine, SN P-91371, AFTT 5882.6, Eng TTSN 5835.7 Cycles: 3955. 150-200 HOUR ROUTINE PERIODIC. 300-400 HOUR ROUTINE PERIODIC. 1000-1500 HOUR ROUTINE PERIODIC. 2100 HOUR MAJOR PERIODIC (MPI) 2100 HOUR PLENUM CASE. REINSTALLED IN #2 POSITION. POST MPI 5 POINT JEDA PERFORMANCE RUN, POST MPI VIBRATION SURVEY, OIL CHANGED, SERVICED WITH MOBIL 254 POST GRND RUN LEAK CHECK, OVER SPEED SHUTDOWN, COMPUTER SETUP, M/M ADJUSTMENT, M/M TRANSFER AND GEARBOX PRESSURES, FAN BALANCE. 4/26/2007 Eng TT CYCLES Transcribed Engine #2 P-913171 Logbook Entry 5835.7 3955 ENGINE MODEL S/N POSITION TSN CSN WO # TFE731-5R-1H P-91371 2 5,835.7 3,955 FNS8C COMPONENT P/N OFF S/N OFF P/N ON S/N ON STATUS DEEC 2118002-6 96-564 2119010-8000 126-BY0861 New #6 BEARING OIL SCAVENGE ELBOW 3075240-1 - 3075240-2 - NEW OIL TUBE/FLEX HOSE 3074814-1 - 3074377-1 - NEW DRIVE SPLINE ADAPTERS (2) 3072869-2 - 3072869-2 - NEW IGNITERS (2) 3074541-1 - 3074541-4 - NEW SPINNER 3074623-3 2385 3074623-3 7-01734-319 OVERHAUL #6 BEARING 358750-3 97-19914-19528 358750-2 MS060633112313 NEW #6 BEARING SCAVENGE SCREEN 3073827-1 - 3073728-1 - NEW 2ND LPT ROTOR ASSEMBLY 3074753-5 7-23315-237 3075426-3 060322903753 NEW 1ST LPT NOZZLE ASSEMBLY 3075225-4 7-01345-1455 3075225-5 7-01345-1455 ALTERED FUEL FILTER ELEMENT 897513-1 - 897830-1 - NEW N1 TRANSDUCER 3073827-5 - 3073827-5 - NEW HPT SHROUD SEGMENTS (2) 3072344-3 - 3073374-9 - NEW HPT SHROUD SEGMENT (1) 3072344-3 - 3073374-10 - NEW HPT SHROUD SEGMENT (1) 3072344-11 - 3073374-6 - NEW HPT SHROUD SEGMENT (1) 3072344-11 - 3073374-12 - NEW HPT SHROUD SEGMENT (1) 3072344-11 - 3073374-2 - NEW SURGE BLEED VALVE 978812-5-1 6530 978812-5-1 P-1719C OVERHAUL FUEL MANIFOLD ASSEMBLY 3074873-5 95-119 3075368-2 90-430C OVERHAUL #1 CARBON SEAL 3075675-2 060515871559 3075675-2 060515870292 NEW #1 CARBON SEAL RUNNER 3075657-1 062141800716 3075657-1 072141800908 NEW
- 115. #3 CARBON SEAL3075719-1 070515878202 3075719-1 070515878225 NEW FWD DAMPER RING 3075280-2 - 3075280-2 - NEW AFT DAMPER RING 3075280-1 - 3085280-1 - NEW #3 BEARING 3072866-1 97-19914-20910 3072866-1 MS070233000387 NEW #3 BEARING SPRING WASHER 3000005-64 - 3000005-64 - NEW 1ST LPT BLADE (1) 3074746-4 - 3074746-4 - NEW ITT HARNESS 3073605-1 0-20219-438 3073605-1 072021901827 NEW COMBUSTION LINER 3075583-2 98P05898 3075583-1 960740403151 OVERHAUL DESWIRL VANE RING 3075126-1 - 3075126-1 - NEW A4 NOZZLE SEGMENTS (7) 3074785-5 - 3074783-5 - INSPECTED A4 NOZZLE SEGMENT (1) 3074783-6 - 3074783-6 - INSPECTED A4 NOZZLE SEGMENT (1) 3074783-6 - 3075584-11 - INSPECTED A4 NOZZLE SEGMENT (1) 3075584-11 - 3075584-16 - NEW HPT PISTON RING SEAL 3000002-10 - 3000002-10 - NEW PLANETARY GEARSHAFT 3074651 -3 8P7137 3074651-3 06P35895 NEW 4/26/2007 Eng TT CYCLES Transcribed Engine #1 P-91363 Logbook Entry 5705 3884 ENGINE MODEL S/N POSITION TSN CSN WO # TFE731-5R-1H P-91363 1 5705 3884 FNS8B/E COMPONENT P/N OFF S/N OFF P/N ON S/N ON STATUS DEEC 2118002-6 96-568 2119010-8000 126-BY0859 NEW #6 BEARING OIL SCAVENGE ELBOW 3075240-1 - 3075240-2 - NEW IGNITERS (2) 3074541-4 - 3074541 -4 - NEW N1 TRANSDUCER SPEED GEAR 3071872-1 - 3071872-1 - NEW 1ST LPT NOZZLE ASSEMBLY 3075225-4 7-01345-1467 3075271-4 07P02954 NEW HPT SHROUD RETAINING SLEEVE 3070023-7 - 3070023-7 - OVERHAUL ITT HARNESS 3073605-1 982021900310 3073605-1 07021901829 NEW HPT BLADES (62) 3074785-8 - 3074785-8 - NEW OIL FILTER COVER 3072231-1 - 3072231-4 - ALTERED FUEL FILTER ELEMENT 897513-1 - 897830-1 - NEW N1 TRANSDUCER 3073827-3 630 3073827-5 NSN NEW OIL TUBE/FLEX HOSE 3074814-1 - 3074377-1 - NEW 6 O'CLOCK IGNITER LEAD ASSY 3071590-11 - 3071590-11 - NEW 7 O'CLOCK IGNITER LEAD ASSY 3071590-10 - 3071590-10 - NEW FUEL MANIFOLD ASSY 3074873-5 7-241 3075368-2 02-122C OVERHAUL #1 CARBON SEAL 3075675-2 971936804003 3075675-2 060515871554 NEW #1 CARBON SEAL RUNNER 3075657-1 982141802603 6075657-1 072141800899 NEW #3 CARBON SEAL 3075644-1 980515821856 3075719-1 070515878203 NEW
- 116. #1 BEARING 358763-187-1994-9368 358763-1 070633106710 NEW #1 BEARING SPACER 3071985-1 - 3071985-1 - NEW DAMPER RING 3075280-1 - 3075280-1 - NEW DAMPER RING 3075280-2 - 3075280-2 - NEW #6 CARBON SEAL 3071383-2 8P-5253 3071383-2 060365000502 NEW DESWIRL VANE RING 3075126-1 - 3075126-1 - NEW DRIVE SPLINE ADAPTERS (2) 3072869-2 - 3072869-2 - NEW SURGE BLEED VALVE 978812-5-1 6742 978812-5-1 P-2248C OVERHAUL COMBUSTION LINER 3075583-2 98P21896 3075583-1 96P10704 OVERHAUL FUEL FILTER CAP 395533 - 3070919-1 - NEW #6 BEARING OIL TUBE 3073736-1 - 3073736-1 - NEW A4 NOZZLE SEGMENTS (5) 3074783-6 - 3075584-16 - NEW A4 NOZZLE SEGMENTS (3) 3075584-10 - 3075584-16 - NEW 2ND LPT ROTOR ASSEMBLY 3074753-5 7-23315-315 3075426-3 060322906213 NEW HPT SHROUD SEGMENT (1) 3073374-3 - 3073374-5 - NEW HPT SHROUD SEGMENTS (2) 3073374-5 - 3073374-10 - NEW HPT SHROUD SEGMENTS {3) 3073374-5 - 3073374-2 - NEW 4/30/2007 AFTT CYCLES Transcribed Logbook Entry 5882.6 3983 Engine #1 SN P-91151 TSN 5551.3 CSN 3668 INSTALLED ENG SN P-91151 IN THE #1 POSITION. OIL CHANGED, SERVICED WITH MOBIL 254, POST GROUND RUN LEAK CK, OVER SPEED SHUTDOWN, COMPUTER SETUP, M/M ADJUSTMENT, M/M TRANSFER. DESCRIPTION PN ON SN ON SN OFF RH FUEL TEMP SW 60010 0279TW 0281TW RH FUEL LO PRESS SW HTE690014-1 0207 0061
- 117. 5/1/2007 Reg. # NXXGSDate: May 1, 2007 Work Order: FNS8 Make: Raytheon Model: BAe 125-800A S/N: 2581XX (NA04XX) TAT: 5882.6 Landings: 3983 I) Performed the following Manufacturer’s Recommended Maintenance items in accordance with Raytheon Hawker 800 and BAe 125 Series 800A and 800 B Aircraft Flexible Maintenance Schedule Revision 10: A) Structural Inspections 1) 530017: #1 and #2 Forward Engine Mounting Bracket Inspection. a) Reinstalled #1 engine forward mounts (2-ea) P/N 3071071-3 magnetic particle inspected by Duncan Aviation, CRS #JGVR194F under work order #FNS8B. b) Reinstalled #2 engine forward mounts (2-ea) P/N 3071071-3 magnetic particle inspected by Duncan Aviation, CRS #JGVR194F under work order #FNS8C. B) Out of Phase Inspections: 1) 320037: Nose Landing Gear Drag Stay Clearances Check. (322061) 2) 720002: At MPI, #1 and #2 Engine Aft Cowling Inner Fan Duct and Exhaust Duct Inspection. 3) 720003: At MPI, #1 and #2 Exhaust Nozzle/Exhaust Pipe V Clamp Detailed Inspection. a) Reinstalled #1 engine tailpipe clamp P/N C46SCP107-1 fluorescent penetrant inspected by Duncan Aviation, CRS #JGVR194F under work order #FNS8B. b) Reinstalled #2 engine tailpipe clamp P/N C46SCP107-1 fluorescent penetrant inspected by Duncan Aviation, CRS #JGVR194F under work order #FNS8C. C) Component Requirements: 1) 1000 Hour #1 Starter/Generator Overhaul. a) Reinstalled #1 Starter/Generator P/N 23080-005 S/N 6949 overhauled by Duncan Aviation, CRS #JGVR194F under work order #FNS8B. D) Lubrication Requirements: 1) #1 Engine Thrust Control Teleflex Cable and Disconnect Coupling Lubrication. (Work Order #FNS8B) 2) #2 Engine Thrust Control Teleflex Cable and Disconnect Coupling Lubrication. (Work Order #FNS8C) II) The following was performed by Duncan Aviation under Work Order #FNS8A: A) Reinstalled HF receiver exciter P/N 064-1015-01 S/N 26960 repaired by Duncan Aviation, CRS #JGVR194F under work order #FNS8A. B) Reinstalled HF power amp antenna coupler P/N 064-1017-02 S/N 11724 repaired by Duncan Aviation, CRS #JGVR194F under work order #FNS8A. C) Reinstalled bridging amp P/N 071-0019-00 S/N 1942 inspected by Duncan Aviation, CRS #JGVR194F under work order #FNS8A. D) Removed copilot’s WC-870 control head assy P/N 7008471-804 S/N 88100501 and installed assy P/N 7008471- 804 S/N 89100794 repaired by Honeywell, CRS #FGNR677K under work order #5000708640 dated 10/17/06. E) Removed existing #2 yoke transmit switch P/N C9500-11-15A S/N 477 and installed a switch P/N C9500-11- 15A S/N 1241 repaired by Page Aerospace Limited CRS #UK.145.00208 on work order 4501915725 dated 01- 23-07. F) Removed Sat Phone Switching Box P/N DA80-000291 S/N 008 and installed a new switching box P/N DA80- 000291 S/N 095. III) The following was performed by Duncan Aviation under Work Order #FNS8B: A) Removed #1 engine S/N P-91363 (TSN: 5705.0, CSN: 3884) and installed engine S/N P-91151 (TSN: 5551.3, CSN: 3668) in the #1 position. B) Removed #1 engine fire loop P/N 3001-112 S/N 62608 and installed new fire loop P/N 3001-112 S/N 89494. C) Removed existing fuel computers and installed new Honeywell N1 Digital Electronic Engine Control ( DEEC ) system in accordance with Garrett Aviation Services STC #ST0142CH-D and Honeywell SB #TFE-731-76- 3065 R9 as follows: 1) Removed components: Item P/N S/N #1 fuel computer 2118002-6 96-568 #2 fuel computer 2118002-6 96-564 2) Installed components: Item P/N S/N Status #1 N1 DEEC 2119010-8000 126-BY0859 New #2 N1 DEEC 2119010-8000 126BY0861 New J2 Extension Cable 4243811-5 017-0542 New J2 Extension Cable 4243811-5 017-0541 New 3) The Instructions for Continued Airworthiness are identified under Garrett Aviation Services Document #43- 8027-002, Rev B. A copy of the Instructions has been provided to the operator.
- 118. 4) Reference FAAForm 337 dated 04/30/07. IV) The following was performed by Duncan Aviation under Work Order #FNS8C: A) Reinstalled #2 engine S/N P-91371 (TSN: 5835.7, CSN: 3855) after MPI. V) Service Bulletins and Service Information: A) Completed Service Bulletins: 1) Honeywell SB TFE-731-76-3065 R9 "Installation of N1 DEEC”. Complied with on #1 engine S/N P- 91363 and #2 engine S/N P-91371. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order #FNS8A, #FNS8B and #FNS8C. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277 05/01/07 XX XXX LLC MAINTENANCE LOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.HomeKey unit:=wdStory Selection.MoveDown unit:=wdLine, Count:=4 Selection.HomeKey unit:=wdLine Selection.MoveDown unit:=wdLine, Count:=2 Selection.MoveRight unit:=wdCell Selection = "" Selection.MoveRight unit:=wdCell Selection = "" Selection.MoveRight unit:=wdCell, Count:=2 Selection = "" Selection.MoveDown unit:=wdLine LDGS APU HRS EVENT DATE 05/14/07 AC 8109.5 8109.5 5905.8 3993 Total 2238.9 INDEX NUMBER 01 EN1 7988.2 7988.2N1 5704.9 3884 EN2 5820 8012.2N2 5850.8 3966 PER 14 CFR PT 91.409(f)(3) THIS OPERATOR SELECTS TO USE THE CURRENT INSPECTION PROGRAM RECOMENDED BY THE MANUFACTURER. COMPLETED 150 HR AIRFRAME LUBRICATION, AFMS TASK NUMBER 050050. NEXT DUE IN CONJUNCTION WITH “A” CHECK AT 6000 HOURS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 05/14/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 119. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.Ho meKey unit:=wdStory Selection.Mo veDown unit:=wdLine, Count:=4 Selection.Ho meKey unit:=wdLine Selection.Mo veDown unit:=wdLine, Count:=2 Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell, Count:=2 Selection = "" Selection.Mo LDGS APU HRS EVENT DATE 06/04/07 AC 810 9.5 810 9.5 5932.4 4010.0 Total 2253.7 INDEX NUMBER 02 EN1 798 8.2 798 8.2 N1 5704.9 3885.0 EN2 582 0 801 2.2 N2 5877.4 3983.0 MAINTENANCE LOG ENTRY'S TRANSFERRED TO XX XXX LLC “NXXGS MAINTENANCE LOG” BINDER #1 THIS DATE. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 06/04/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 120. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.Ho meKey unit:=wdStory Selection.Mo veDown unit:=wdLine, Count:=4 Selection.Ho meKey unit:=wdLine Selection.Mo veDown unit:=wdLine, Count:=2 Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell, Count:=2 Selection = "" Selection.Mo veDown unit:=wdLine LDGS APU HRS EVENT DATE 06/04/07 AC 810 9.5 810 9.5 5932.4 4010.0 Total 2253.7 INDEX NUMBER 03 EN1 798 8.2 798 8.2 N1 5704.9 3885.0 EN2 582 0 801 2.2 N2 5877.4 3983.0 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4085 LANDINGS. UPDATED CAMP SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 06/04/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 121. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.Ho meKey unit:=wdStory Selection.Mo veDown unit:=wdLine, Count:=4 Selection.Ho meKey unit:=wdLine Selection.Mo veDown unit:=wdLine, Count:=2 Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell, Count:=2 Selection = "" Selection.Mo veDown unit:=wdLine LDGS APU HRS EVENT DATE 06/04/07 AC 810 9.5 810 9.5 5932.4 4010.0 Total 2253.7 INDEX NUMBER 04 EN1 798 8.2 798 8.2 N1 5704.9 3885.0 EN2 582 0 801 2.2 N2 5877.4 3983.0 AFMS TASK NUMBER 050020, 150-200 HOUR THRUST REVERSER INSPECTIONS COMPLETED ON #1 AND #2 ENGINES PER NORDAM MM 78-30-00 TABLE 602. OK FOR SERVICE. UPDATED CAMP SYSTEM RECORDS. NEXT DUE IN CONJUNCTION WITH 300-400 HOUR INSPECTION AT 6030 AH. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 06/04/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 122. 6/15/2007 Eng TTCYCLES Transcribed Engine #1 P-91363 Logbook Entry 5705 3884 Premier Turbines Service Record dated 6/15/07 ENGINE INSPECTED AND REPAIRED FOR PLENUM REPLACEMENT. ALL WORK PERFORMED IAW TFE731 LMM 72-02-75, REV 7 DATED 12-01-06 AND HMM 72-02-71, REV. 10 DATED 02-28-07. THIS ENGINE HAS BEEN INSPECTED REPAIRED AND TESTED IAW THE CURRENT REGULATION OF THE FAA AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO WORK PERFORMED. REFERENCE WORK ORDER NO. 42250. DEEC S. G. SETTING (WITH JET A TYPE FUEL): 3.50. ENGINE N1 COMPENSATOR PN 3074135-1. IF FAN SN 6-12172-1771 IS REMOVED FROM ENGINE SN P91363 THEN FAN COMPENSATOR PN 3074135- 1 IS REQUIRED TO BE TRANSFERRED WITH THE FAN. ENGINE FUEL SYSTEM HAS BEEN PRESERVED. FUEL SYSTEM MUST BE DE-PRESERVED IAW LMM 72-00-00, “SERVICING” PRIOR TO OPERATION. SIGNED: PATRICK N. MEREDITH, PREMIER TURBINES, 3551 DONIPHAN DR, NEOSHO, MISSOURI 64850, FAA CRS # NZUR892L. ENGINE MODEL S/N POSITION TSN CSN WO # TFE731-5R-1H P-91363 1 5705 3884 42250 COMPONENT P/N ON S/N OFF S/N ON STATUS ENGINE INSP AND REPAIRED FOR PLENUM REPLACEMENT. 3074600-1 P-91363 INSPECTED STAGE 2 COMPRESSOR WHEEL SHROUD 3070289-2 07590-400366-001R REPAIRED STAGE 3 COMPRESSOR WHEEL SHROUD 3070292-4 LOT 1793 REPAIRED STAGE 2 COMPRESSOR ROTOR SHROUD 3072403-1 07590-7769 REPAIRED STAGE 3 COMPRESSOR ROTOR SHROUD 30721404-1 07590-225813-001R REPAIRED STAGE 4 COMPRESSOR ROTOR SHROUD 3072405-1 LOT2231 REPAIRED STAGE 4 COMPRESSOR STATOR 3074555-8 LT0015004 REPAIRED SHROUD IMPELLER 3077047-12 4P-528 REPAIRED CASE ASSY PLENUM 3072443-5 5-22151-1132 REPAIRED TFE731 FUEL CONTROL UNIT ( FCU )WITH FOLLOWING SB’s INC:TFE731-73-SB09 L- 17, TFE731-73-3125RWK, TFE731-73-3134, TFE731-73-3116RWK, TFE731-73-3131, TFE731-73-SB07 3070800-24 A8417C OVERHAUL ED OIL PUMP 3060785-2 061405701006 NEW HIGH PRESSURE TURBINE SHROUD SEGMENT (TWO) 3073374-2 NEW HIGH PRESSURE TURBINE SHROUD SEGMENT (TWO) 3073374-5 NEW TUBE ASSEMBLY 3073736-1 NEW BALL BEARING 358752-3 070233002542 NEW #4 CARBON SEAL 3074573-2 060515873878 NEW #5 CARBON SEAL 3074574-2 061936802303 NEW
- 123. 06/15/2007 AFTT CYCLES Transcribed#1 Engine, SN P-91363 logbook 871 380 SB TFE731-72-3001 R51 LIFE LIMITS OF CRITICAL PARTS CW 72-3263 R14 VERIFIED PERIODIC INSPECTIONS CW 72-3397 R2 INITIATE COMPONENT RECORDS CW 72-3641 R6 EDDY CURRENT INSPECTION OF IMPELLER 72-3662 R6 REPLACE #4 AND #5 CARBON SEALS 73-3115 R1 INSTALL FUEL CONTROL 79-3065 R2 INSTALL METAL #6 BEARING OIL IN TUBE ASSY 79-3066 R1 INSTALL LUBE WITH REGULATOR AND SCAVENGE PUMP DESCRIPTION PN ON SN ON SN OFF PREMIER TURBINES 3551 DONIPHAN DR, NEOSHO, MISSOURI CRS NZUR829L
- 124. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.Ho meKey unit:=wdStory Selection.Mo veDown unit:=wdLine, Count:=4 Selection.Ho meKey unit:=wdLine Selection.Mo veDown unit:=wdLine, Count:=2 Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell, Count:=2 Selection = "" Selection.Mo veDown unit:=wdLine Selection.Mo LDGS APU HRS EVENT DATE 06/24/07 AC 8109. 5 8109. 5 5942.5 4019 Total 2258.4 INDEX NUMBER 05 EN1 7988. 2 7988. 2N1 5705.0 3889 EN2 5820 8012. 2N2 5887.5 3992 Airframe Log Entry Reg. # NXXGS Date: June 24, 2007 Work Order: FPEPA Make: Raytheon Model: 125-800A S/N: 2581XX A/C TT: 5942.5 Landings: 4019 Engine Position: #1 Rental Eng. S/N: 91151 Eng.TSN: 5569.6 Eng. CSN: 3676 Customer Eng. S/N: 91363 Eng. TSN: 5705.0 Eng. CSN: 3889 1) Removed rental engine s/n 91151 from #1 position. 2) Installed customer’s post MPI Inspection & core repaired engine s/n 91363 into #1 position (See engine log for details). 3) Accomplished the following engine removal items: - Inspected AFT cowling, inner fan duct, and exhaust duct (M/M 72-00-02). - Inspected exhaust pipe V-Band clamp (M/M 72-00-03) - Lubrication of #1 engine Teleflex assembly. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FPEPA Signed: Lloyd Kasten_____________________________________________________ For Duncan Aviation CRS#JGVR194F Phone: 800-228-4277 Engine Log Entry Reg. # NXXGS Date: June 24, 2007 Work Order: FPEPA Make: Raytheon Model: 125-800A S/N: 2581XX A/C TT: 5942.5 Landings: 4019 Engine Position: #1 Rental Eng. S/N: 91151 Eng.TSN: 5569.6 Eng. CSN: 3676 Customer Eng. S/N: 91363 Eng. TSN: 5705.0 Eng. CSN: 3889 1) Installed customer’s engine s/n 91363 in #1 position after MPI Inspection & core repair. 2) Accomplished oil change, Serviced with Mobil Jet 254 oil. (@ 5942.5 AFTT) 3) Accomplished ground run, leak and ops checks, manual mode transfer and overspeed shutdown checks I/A/W Honeywell LMM. Note: Oil SOAP sample due in 25 hours. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FPEPA Signed: Lloyd Kasten_____________________________________________________ For Duncan Aviation CRS#JGVR194F Phone: 800-228-4277
- 125. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.Ho meKey unit:=wdStory Selection.Mo veDown unit:=wdLine, Count:=4 Selection.Ho meKey unit:=wdLine Selection.Mo veDown unit:=wdLine, Count:=2 Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell Selection = "" Selection.Mo veRight unit:=wdCell, Count:=2 Selection = "" Selection.Mo veDown unit:=wdLine LDGS APU HRS EVENT DATE 06/29/07 AC 810 9.5 810 9.5 5942.5 4021 Total 2259 INDEX NUMBER EN1 798 8.2 798 8.2 N1 5707 3891 EN2 582 0 801 2.2 N2 5889.5 3994 TOOK SOAP SAMPLE #2 ENGINE, RAN ENG TO LEAK TEST NEW OIL FILTER, PN 3070945-1, NO LEAKS NOTED, OK FOR SERVICE. NEXT DUE AT 150-200 HR ENG INSPECTION: 6092 AF TT, 6039 ENG TT ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 06/29/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 126. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.002 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 7/21/07 AC 810 9.5 810 9.5 5951.7 4028 Total 2265 6334 INDEX NUMBER 06 EN1 798 8.2 798 8.2 N1 5714.2 3898 EN2 582 0 801 2.2 N2 5896.7 4001 C/W SEMI-ANNUAL, 125 HOUR/250 CYCLE APU INSPECTION IAW HAMILTON SUNDSTRAND T-62T-40C8D1 ENGINE MANUAL, REVISION 4 (REISSUE) DATED 15 MARCH, 2006. C/W SEMI-ANNUAL, 250 HOUR/500 CYCLE APU INSPECTION IAW HAMILTON SUNDSTRAND T-62T-40C8D1 ENGINE MANUAL, REVISION 4 (REISSUE) DATED 15 MARCH, 2006. NEXT SEMI-ANNUAL INSPECTION DUE AT 2/21/08 C/W ANNUAL, 500 HOUR/1000 CYCLE APU INSPECTION IAW HAMILTON SUNDSTRAND T-62T-40C8D1 ENGINE MANUAL, REVISION 4 (REISSUE) DATED 15 MARCH, 2006. C/W ANNUAL, 1000 HOUR/2000 CYCLE APU INSPECTION IAW HAMILTON SUNDSTRAND T-62T-40C8D1 ENGINE MANUAL, REVISION 4 (REISSUE) DATED 15 MARCH, 2006. NEXT ANNUAL INSPECTION DUE 7/21/08 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 07/21/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 127. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 7/27/07 AC 810 9.5 810 9.5 5954.7 4031 Total 2267.1 6337 INDEX NUMBER 07 EN1 798 8.2 798 8.2 N1 5717.2 3901 EN2 582 0 801 2.2 N2 5899.7 4004 FIRST OFFICER “A” SCREEN WINDSHIELD IS DELAMINATED BEYOND ALLOWABLE LIMITS. REMOVED OLD WINDSHIELD AND INSTALLED REPAIRED WINDSHIELD PER AMM 56-10-11, OP CHECKS OK. PART NUMBER ON SERIAL NUMBER ON PART NUMBER OFF SERIAL NUMBER OFF NF24016-416 ISSUE 1 L323412 NF24016-336 ISSUE 2 L218246 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 07/27/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 128. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 08/11/07 AC 810 9.5 810 9.5 5964.6 4042 Total 2275.5 6352 INDEX NUMBER 08 EN1 798 8.2 798 8.2 N1 5727.1 3912 EN2 582 0 801 2.2 N2 5909.6 4015 REMOVED MAIN BATTERY #1 AND #2 FOR CAPACITY CHECK AND SERVICE BY EL CORTA, INC, 2000 BRETT RD, NEW CASTLE DE, 19720, CRS XZAR763L, UNDER WO # 07184 PER HAWKER CMM 24-32-35, REV A, DATED 04-08-05. REINSTALLED MAIN BATTERY PER AMM 24-30-150. POSITION P/N ON S/N ON #1 9750W0640 3227W0014 #2 9750W0640 3227W0015 REMOVED AUX BATTERY #3, #4 AND #5 FOR CAPACITY CHECK AND SERVICE BY EL CORTA, INC, 2000 BRETT RD, NEW CASTLE DE, 19720, CRS XZAR763L, UNDER WO # 07184 PER CONCORDE ICA’S, DRAWING # 5-0143, REV E, DATED 02/20/07. REINSTALLED AUX BATTERIES IN POSITIONS SHOWN BELOW. INSTALLED NEW RG-126, SN 4018460 TO REPLACE REMOVED UNSERVICEABLE BATTERY SN CBC-404424. POSITION P/N ON S/N ON P/N OFF S/N OFF #3 UJ RG-126 40126243 RG-126 #4 UK RG-126 CBC-404429 RG-126 #5 UL RG-126 40184860 RG-126 CBC-404424 REMOVED AND REINSTALLED IRS BATTERY FOR CAPACITY CHECK AND SERVICE BY EL CORTA, INC, 2000 BRETT RD, NEW CASTLE DE, 19720, CRS XZAR763L, UNDER WO # 07184 PER MARATHON OMM 24-34-00, REV 7 DATED 04/15/06, POSITION P/N ON S/N ON IRS CA-54-1 10300827 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/11/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 129. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 08/11/07 AC 810 9.5 810 9.5 5964.6 4042 Total 2275.5 6352 INDEX NUMBER 09 EN1 798 8.2 798 8.2 N1 5727.1 3912 EN2 582 0 801 2.2 N2 5909.6 4015 REPLACED FWD AND AFT EMERGENCY EXIT LIGHT POWER SUPPLY “D” CELL NI-CAD BATTERIES, AVIALL PN 25503-025, NO SN. EMERGENCY LIGHT SYS OP CKS OK. NEXT DUE REPLACEMENT 8/11/09. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/11/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 130. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 08/18/07 AC 810 9.5 810 9.5 5973.5 4049 Total 2282.1 6365 INDEX NUMBER 10 EN1 798 8.2 798 8.2 N1 5736.0 3919 EN2 582 0 801 2.2 N2 5918.5 4022 TOOK SOAP SAMPLE #1 ENGINE, RAN ENG TO LEAK TEST NEW OIL FILTER, PN 3070945-1, NO LEAKS NOTED, OK FOR SERVICE. NEXT DUE AT 5886 ENGINE TIME. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/18/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 131. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" LDGS APU HRS CYCLES EVENT DATE 08/23/07 AC 810 9.5 810 9.5 5981.5 4056 Total 2288.7 6376 INDEX NUMBER 11 EN1 798 8.2 798 8.2 N1 5744 3926 EN2 582 0 801 2.2 N2 5926.5 4029 AIR CONDITIONING SYSTEM TEMP CONTROL PROBLEM: OPS NORMAL IN “MANUAL” MODE AND IN “AUTO” WHEN COCKPIT/CABIN TEMP CONTROL SELECT SW ON COCKPIT PEDESTAL SELECTED TO “CABIN”; UNABLE TO CONTROL TEMP IN AUTO WITH PEDESTAL SW SELECTED TO “COCKPIT”; TEMP DRIVES TO FULL HOT. TRIED NEW TEMP CONTROL SELECTOR, NO HELP, RE-INSTALLED ORIGINAL PART AND REPLACED RELAY K18; OP CKS OK. POS NOMENCLATURE P/N ON S/N ON K18 RELAY MHLO-12D-26.5 0726 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/23/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 132. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 08/23/07 AC 810 9.5 810 9.5 5981.5 4056 Total 2288.7 6376 INDEX NUMBER 12 EN1 798 8.2 798 8.2 N1 5744 3926 EN2 582 0 801 2.2 N2 5926.5 4029 TIME CHANGE ITEM (3000 HOURS): LEFT AIRBRAKE DUE REPLACEMENT AT 5998 HOURS. REPLACED UNSERVICEABLE JACK CONTROL ARM BUSHING, PN 25CW899, NSN, WITH NEW BUSHING. REMOVED AND REPLACED LT AIRBRAKE JACK ASSY (WITH AIRBRAKE JACK EYE END) PER AMM27-61-31-401. AIRBRAKE OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF AIRBRAKE JACK AIR46520-1 APB001752 AIR46520-1 LK0454 AIRBRAKE JACK EYE END AIR122016 NSN AIR122016 NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/23/2007 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 133. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 09/07/07 AC 810 9.5 810 9.5 5981.5 4056 Total 2288.7 6376 INDEX NUMBER 13 EN1 798 8.2 798 8.2 N1 5744 3926 EN2 582 0 801 2.2 N2 5926.5 4029 REMOVED AND REPLACED #1 AND #2 MAIN SHIP BATTERIES. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN BATTERY RG-390E 40195945 9750W0640 3227W0014 #2 MAIN BATTERY RG-390E 40195945 9750W0640 3227W0015 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 09/07/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 134. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 09/23/07 AC 810 9.5 810 9.5 6000.8 4073 Total 2302.6 6404 INDEX NUMBER 14 EN1 798 8.2 798 8.2 N1 5763.3 3943 EN2 582 0 801 2.2 N2 5945.8 4046 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4148 LANDINGS. UPDATED CAMP SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 09/23/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 135. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 09/26/07 AC 810 9.5 810 9.5 6006.5 4079 Total 2305.9 6412 INDEX NUMBER 15 EN1 798 8.2 798 8.2 N1 5770 3950 EN2 582 0 801 2.2 N2 5952.5 4053 APU DC GEN WILL NOT COME ON LINE. STARTS AND OPERATES OK IN ALL OTHER RESPECTS. REPLACED K2 RELAY IN APU ELECTRICAL SUPPLY CIRCUIT, OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RELAY BR14X150A18 NSN BR14X150A18 NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 09/26/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 136. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 10/04/07 AC 810 9.5 810 9.5 6014.3 4085 Total 2311.9 6424 INDEX NUMBER 16 EN1 798 8.2 798 8.2 N1 5777.8 3956 EN2 582 0 801 2.2 N2 5960.3 4059 COMPLETED “A” INSPECTION THIS DATE PER HAWKER BEECHCRAFT AFMS REV 11. NEXT DUE “A” INSPECTION AT 6315 AF HOURS. NEXT DUE “B” INSPECTION AT 6318 AF HOURS, LAST COMPLETED 2/27/2006. COMPLETED 150 AND 300 HOUR LUBRICATION THIS DATE PER HAWKER BEECHCRAFT AFMS REV 11. NEXT DUE 150 HOUR LUBE DUE AT 6165 AF HOURS. NEXT DUE 300/600 HOUR LUBE DUE AT 6315 AF HOURS. COMPLETED 150-200 AND 300-400 HOUR THRUST REVERSER INSPECTION PER NORDAM MAINT MANUAL REV 4. NEXT DUE 150-200 HOUR TR INSPECTION AT 6165 AF HOURS. NEXT DUE 300-400 HOUR TR INSPECTION AT 6315 AF HOURS. NEXT DUE 600-800 HOUR TR INSPECTION AT 6330 AF HOURS. LAST COMPLETED 600-800 HOUR TR INSPECTION 7/21/06 AT 5730 AF HOURS. NEXT DUE 1200-1400 HOUR TR INSPECTION AT 6930 AF HOURS. LAST COMPLETED 1200-1400 HOUR TR INSPECTION 7/21/06 AT 5730 AF HOURS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/04/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 137. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 10/11/07 AC 810 9.5 810 9.5 6022.4 4091 Total 2322.3 6433 INDEX NUMBER 17 EN1 798 8.2 798 8.2 N1 5785.9 3962 EN2 582 0 801 2.2 N2 5968.4 4065 APU GENERATOR WILL NOT COME ON LINE. FOUND APU GENERATOR CONTROL UNIT BAD. REPLACED WITH OH UNIT, OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF DC GENERATOR CONTROL UNIT 51509-006C 5686A 51509-006C 15912A INSTALLED UNIT PURCHASED FROM DUNCAN AVIATION, OVERHAULED BY WECO AEROSPACE, INC., 1501 AVIATION BLVD, LINCOLN, CA 95648, CRS UQ3R902L, UNDER WO# L32705 DATED 5 SEPT, 2007. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/11/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 138. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 10/28/07 AC 810 9.5 810 9.5 6047.4 4112 Total 2338.3 6466 INDEX NUMBER 18 EN1 798 8.2 798 8.2 N1 5810.9 4086 EN2 582 0 801 2.2 N2 5993.4 4086 #1 MAIN WHEEL AND TIRE ASSY REPLACED FOR TIRE WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA 1814 XB003 AHA1814 LC290 #1 MAIN TIRE ASSY 23X7.00-12 53030053 INSTALLED UNIT PURCHASED FROM ALL WEST AVIATION. WHEEL OH’D BY CORPAIR SUPPLY COMPANY, 827 TEXAS COURT, O’FALLON, MISSOURI, CRS# SE2R158L, UNDER WO 72984, DATED 1/17/07 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/11/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 139. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 10/28/07 AC 810 9.5 810 9.5 6047.4 4112 Total 2338.3 6466 INDEX NUMBER 19 EN1 798 8.2 798 8.2 N1 5810.9 4086 EN2 582 0 801 2.2 N2 5993.4 4086 #2 MAIN WHEEL AND TIRE ASSY REPLACED FOR TIRE WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 MAIN WHEEL ASSY AHA 1814 XB007 AHA1814 WW032 #2 MAIN TIRE ASSY 23X7.00-12 53060592 INSTALLED UNIT PURCHASED FROM ALL WEST AVIATION. WHEELS OH’D BY CORPAIR SUPPLY COMPANY, 827 TEXAS COURT, O’FALLON, MISSOURI, CRS# SE2R158L, UNDER WO 72985 DATED 1/17/07 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/28/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 140. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 10/31/07 AC 810 9.5 810 9.5 6047.4 4112 Total 2338.3 6466 INDEX NUMBER 20 EN1 798 8.2 798 8.2 N1 5810.9 4086 EN2 582 0 801 2.2 N2 5993.4 4086 #1 ENG MAIN AIR VALVE LIGHT REMAINS ON AT ALL TIMES. FOUND #1 MAIN AIR VALVE “CLOSED” INDICATION SW INOP. VALVE FULLY CLOSED WITH SW NOT INDICATING CLOSED. REPLACED #1 MAIN AIR VALVE PER AMM 21-10-25-401, INSTALLED NEW SEALS, RAN ENG, LEAK AND OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF BLEED AIR VALVE 321292-1 P-1689 321292-1 2032 SEAL 24096-200A NSN SEAL 6-464-1PAR NSN INSTALLED UNIT PURCHASED FROM DUNCAN AVIATION. VALVE ASSY OH’D BY DUNCAN AVIATION, LINCOLN AIRPORT, LINCOLN, NE 68524, CRS# JGVR194F, UNDER WO EQGVA DATED 6/13/07. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/31/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 141. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 11/19/07 AC 810 9.5 810 9.5 6062.9 4125 Total 2359.5 6486 INDEX NUMBER 21 EN1 798 8.2 798 8.2 N1 5826.4 3996 EN2 582 0 801 2.2 N2 6008.9 4099 #3 AND #4 MAIN WHEEL AND TIRE ASSYS REPLACED FOR TIRE WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 MAIN WHEEL ASSY AHA 1814 LC290 AHA1814 LR165 #3 MAIN TIRE ASSY 23X7.00-12 70651035 #4 MAIN WHEEL ASSY AHA 1814 WWO32 AHA1814 SL105 #4 MAIN TIRE ASSY 23X7.00-12 70660835 INSTALLED WHEELS OH’D BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3317, DATED 11/12/07 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 11/19/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 142. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 11/28/07 AC 810 9.5 810 9.5 6062.9 4125 Total 2359.5 6486 INDEX NUMBER 22 EN1 798 8.2 798 8.2 N1 5826.4 3996 EN2 582 0 801 2.2 N2 6008.9 4099 CREW REPORTS #1 ALTERNATOR TRIPS OFF LINE REPEATEDLY UNDER LOAD. REMOVED AND REPLACED #1 ALTERNATOR PER AMM 24-22-21 AND TESTED SAME PER AMM 24-21-17, OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 ALTERNATOR (AC GENERATOR) BA02801-1 1304 BA02801-1 1311 INSTALLED AC GENERATOR OH’D BY WECO AEROSPACE, 1501 AVIATION BLVD, LINCOLN, CA 95648, CRSUQ3R902L, UNDER WO# L22892, DATED 11/18/05. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 11/28/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 143. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 12/10/07 AC 810 9.5 810 9.5 6085.2 4143 Total 2373.7 6510 INDEX NUMBER 23 EN1 798 8.2 798 8.2 N1 5847.7 4014 EN2 582 0 801 2.2 N2 6030.2 4117 CREW REPORTS RUMBLING, SURGING SOUND FROM #2 ENGINE. VERIFIED PROBLEM. VISUALLY INSPECTED ENGINE, NOTED #2 ENGINE STARTER GENERATOR VERY HOT TO TOUCH AND THE COOLING EXHAUST HAS A BURNT ELECTRICAL ODOR. REPLACED STARTER GENERATOR PER AMM 24-30-21, RAN ENGINE, OP CHECKS OK, RUMBLE SOUND GONE. OK FOR SERVICE. REMOVED STARTER GEN ACCRUED 410 HOURS BEFORE FAILURE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 STARTER GENERATOR 23080-005 3237 23080-005 5549 INSTALLED DC STARTER GENERATOR OH’D BY WECO AEROSPACE, 1501 AVIATION BLVD, LINCOLN, CA 95648, CRSUQ3R902L, UNDER WO# C9170, DATED 9/06/2007. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/10/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 144. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 12/13/07 AC 810 9.5 810 9.5 6090.2 4150 Total 2378 6519 INDEX NUMBER 24 EN1 798 8.2 798 8.2 N1 5852.7 4021 EN2 582 0 801 2.2 N2 6035.2 4124 INSTALLED AND RIGGED OVERHAULED MAIN ENTRY DOOR HANDRAIL ASSY PER AMM 52-11-00. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF DOOR STAY ASSY UPPER 25FC7477AB NSN 25FC7477AB NSN INSTALLED MAIN DOOR UPPER STAY ASSY OH’D BY APPH ARNONI, 15555 VICKERY, SUITE 125, HOUSTON, TX 77032, CRS Y8AR872N, UNDER WO# W104667, DATED 12/05/2007. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/13/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 145. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 12/13/07 AC 810 9.5 810 9.5 6090.2 4150 Total 2378 6519 INDEX NUMBER 25 EN1 798 8.2 798 8.2 N1 5852.7 4021 EN2 582 0 801 2.2 N2 6035.2 4124 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4225 LANDINGS. UPDATED AVTRAK SYSTEM RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/13/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 146. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 12/13/07 AC 810 9.5 810 9.5 6090.2 4150 Total 2378 6519 INDEX NUMBER 26 EN1 798 8.2 798 8.2 N1 5852.7 4021 EN2 582 0 801 2.2 N2 6035.2 4124 COMPLETED 150-200 HOUR ENGINE INSPECTION INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES, RAN ENGINES, LEAK CKS OK. WORK PERFORMED IAW HONEYWELL AMM 79-20-03 AND 79-20-01. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. UPDATED AVTRAK SYSTEM RECORDS NEXT 150-200 HOUR ENGINE INSPECTION DUE AT 6240 AFTT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/13/07 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 147. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 01/04/08 AC 810 9.5 810 9.5 6099.7 4157 Total 2385.6 6528 INDEX NUMBER 27 EN1 798 8.2 798 8.2 N1 5862.2 4028 EN2 582 0 801 2.2 N2 604437 4131 FLT CREW REPORTS “GEAR WARN CTL” CIRCUIT BREAKER (K4-DAD) POPS, WILL NOT RESET. VERIFIED FAULT. ISOLATED PROBLEM TO DEFECTIVE RH MLG DOWNLOCK STANDBY MICROSWITCH (KM). REPLACED AND RIGGED RH MLG DOWNLOCK STANDBY MICROSWITCH (KM) PER AMM 32-60-00, OK FOR SERVICE. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 01/04/08 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 148. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 01/04/08 AC 810 9.5 810 9.5 6099.7 4157 Total 2385.6 6528 INDEX NUMBER 28 EN1 798 8.2 798 8.2 N1 5862.2 4028 EN2 582 0 801 2.2 N2 604437 4131 REPLACED LT AND RT NLG WHEEL AND TIRE ASSY’S FOR NORMAL WEAR PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LT NLG WHEEL AND TIRE ASSY 52339 DW061 52339 LS063 RT NLG WHEEL AND TIRE ASSY 52339 149-1045 52339 LS064 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 01/04/08 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 149. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 01/07/08 AC 810 9.5 810 9.5 6099.7 4157 Total 2385.6 6528 INDEX NUMBER 29 EN1 798 8.2 798 8.2 N1 5862.2 4028 EN2 582 0 801 2.2 N2 604437 4131 CREW REPORTS #1 ALTERNATOR FAIL ANNUNCIATOR ON INTERMITTENTLY. SWAPPED ALTERNATOR GENERATOR CONTROL UNITS. PROBLEM FOLLOWS TO #2 SIDE. REPLACED #2 ENGINE AC ALTERNATOR GENERATOR CONTROL UNIT (QC). RAN ENGINE TO VERIFY OPERATION PER AMM 24-21-17. OK FOR SERVICE. #1 ALTERNATOR GCU, PN CB02701 SERIAL NUMBER IS: 5536. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 AC GEN CONTROL UNIT CB02701 2247 CB02701 1007 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 01/07/08 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 150. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 01/09/08 AC 810 9.5 810 9.5 6099.7 4157 Total 2385.6 6528 INDEX NUMBER 30 EN1 798 8.2 798 8.2 N1 5862.2 4028 EN2 582 0 801 2.2 N2 604437 4131 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4232 LANDINGS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 01/09/08 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 151. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 1/24/2008 AC 810 9.5 810 9.5 6121.8 4170 Total 2394.2 6545 INDEX NUMBER 31 EN1 798 8.2 798 8.2 N1 5884.3 4041 EN2 582 0 801 2.2 N2 6066.8 4144 C/W SEMI-ANNUAL, 125 HOUR/250 CYCLE APU INSPECTION IAW HAMILTON SUNDSTRAND T-62T-40C8D1 ENGINE MANUAL, REVISION 4 (REISSUE) DATED 15 MARCH, 2006. NEXT DUE AT 2515 APU TACH OR 7/23/08 C/W SEMI-ANNUAL, 250 HOUR/500 CYCLE APU INSPECTION IAW HAMILTON SUNDSTRAND T-62T-40C8D1 ENGINE MANUAL, REVISION 4 (REISSUE) DATED 15 MARCH, 2006. NEXT SEMI-ANNUAL INSPECTION DUE AT 7/23/08 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 1/24/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 152. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 1/24/2008 AC 810 9.5 810 9.5 6121.8 4170 Total 2394.2 6545 INDEX NUMBER 32 EN1 798 8.2 798 8.2 N1 5884.3 4041 EN2 582 0 801 2.2 N2 6066.8 4144 AD 2007-26-11. THIS AD DOES NOT APPLY THIS AC SINCE AT TIME OF PRODUCTION WAS NOT OPTIONALLY OR STANDARD EQUIPPED WITH INTERTECHNIQUE ZODIAC AIRCRAFT SYSTEMS, OXYGEN RESERVE CYLINDERS, MODEL F5341AA5283. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 1/24/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 153. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 02/05/2008 AC 810 9.5 810 9.5 6128.6 4178 Total 2399.7 6555 INDEX NUMBER 33 EN1 798 8.2 798 8.2 N1 5891.1 4049 EN2 582 0 801 2.2 N2 6073.6 4152 2/5/08 Workorder No. 6898 NXXGS TT: 6128.6 Landings: 4178.0 1.) Performed 24-Month RVSM Certification consisting of the following: a. Tested #1 ADZ-810 ADC (P/N: 7000700-668, S/N: 88092843) b. Tested #2 ADZ-810 ADC (P/N: 7000700-668, S/N: 88123056) c. Tested Standby Altimeter (P/N: WL1605AM2, S/N: AF125) d. Tested #1 RCZ-851 Transponder (P/N: 7510700-802, S/N: 99010256) e. Tested #2 RCZ-851 Transponder (P/N: 7510700-802, S/N: 88070149) 2.) Testing was performed in accordance with the following Federal Aviation 3.) Regulations and Manufacturer’s Specifications: a. FAR 43, Appendix E, Paragraph (b) as required by FAR 91.411 b. FAR 43, Appendix F as required by FAR 91.413 c. Hawker 800 Maintenance Manual, 34-10-17-501, Rev. 39, 1/2008 d. Reference was made to Raytheon Aircraft SB 34-3110, Rev. 9, 2/2005 4.) Aircraft is approved for return to service with regard to the work performed. Red Eagle Avionics, LLC CRS # EHER536D _______________________________ Jason D. Barron
- 154. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 02/06/2008 AC 810 9.5 810 9.5 6128.6 4178 Total 2399.7 6555 INDEX NUMBER 34 EN1 798 8.2 798 8.2 N1 5891.1 4049 EN2 582 0 801 2.2 N2 6073.6 4152 AD 2008-02-19. THIS AD DOES NOT APPLY TO ENG SN P-91363 AND P-91371 BECAUSE PART NUMBERS CALLED OUT IN AD ARE NOT INSTALLED, PER SB TFE731-72-3720. ENTERED AD COMPLIANCE STATEMENT IN BOTH ENG’S LOGBOOK AD COMPLIANCE RECORD SECTION. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 02/06/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ Reference only: Parts in Toilet area Monogram Toilet PN 4620-17, SN 80, Flush timer pn 11059-60, sn 4-3280, dump valve assy, pn 4650-16, flush motor assy, pn 3500-14, sn a-318, flush motor only, pn 4910-33, sn a318, lav aft floro light pwr unit AL5117, SN 2095, Electonic Air Temp Control Box pn 617452-3, TB “ DL “
- 155. TFE 731-5R-1H XX XXXLLC MAINTENANCE LOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 03/11/2008 AC 810 9.5 810 9.5 6157.9 4199 Total 2415.4 6579 INDEX NUMBER 35 EN1 798 8.2 798 8.2 N1 5920.4 4070 TIMES AND CYCLES AS OF 3/11/2008 EN2 582 0 801 2.2 N2 6102.9 4173 TRANSCRIPTION OF HAWKER BEECH TPA MAINTENANCE ACTIONS COMPLETED B, E AND F INSP C/W LUBE RQMT AS SPECIFIED BY INSPECTION B, E, AND F INSPECTION RQMTS ONLY. NO OTHER LUBE PERFORMED. C/W ELT INSPECTION IAW FAR 91.207, BATTERY EXP DATE: AUGUST, 2010, ELT PN 453- 0421-999, SN 01201 C/W 12 MO COCKPIT PN BA51015-3, SN 033897 AND CABIN, PN 1600, SN A569075C, FIRE EXTINGUISHER WEIGHT CHECK C/W 1500 HR/150 HR TAIL STROBE INTENSITY CHECK, CANDLE POWER MEASURED AT 240, ABOVE 100 MIN, DUE AGAIN IN 150 HRS (6308). CW 12 MO API LH AND RH WINGLET NAV LIGHT LENSE INSP IAW APH-0611, TABLE 1.3 CW 12 MO API LH AND RH WINGLET STROBE ASSY INSP IAW APH-0611, TABLE 1.3 AD COMPLIANCE AD 2007-07-12, HONEYWELL NAV COMPUTERS, DOES NOT APPLY DUE TO ONLY 1 IRS INSTALLED. SB COMPLIANCE CW MSB 24-3793, INSPECT REPLACE UAM100 CURRENT LIMITERS, FOUND AD 2006-12-20, PCW ON 7/21/06 @ 5730 HOURS, NO FURTHER ACTION RQD. CW MSB 25-3823 R1, DECRANE SEAT BELT SHACKLES, MSB 25-3823 PCW ON 3/14/2007 @ 5846 HOURS, NO FURTHER ACTION RQD CW API SBH-07-001, INSPECTION OF THE WINGLETS, NO DISCREPANCIES NOTED, NO FURTHER ACTION RQD. COMPONENT REPLACED HYDRAULIC PRESSURE MAINTAINING VALVE WITH OH UNIT, PN AIR45474/0, SN OFF 8709366, SN ON, LK0487. OH BY UNIPAK AVIATION, CRS # UW2R229L. OPS, LEAK, AND DISSIPATION TEST SATISFACTORY TOUCHED UP PAINT ADJUSTED MAIN ENTRY DOOR CABLE GUIDE AS RQD, AND LUBED DOOR. REMOVED, CLEANED AND RESEALED TOP AFT ADF ANTENNAS, GROUND PRESSURIZED AIRCRAFT. LEAK CK GOOD.
- 156. REPLACED AFT BAYLIGHTING FIXTURE WITH NEW, PN 15-0188-11, OP CKS GOOD REPLACED FO PTT SW WITH NEW PN 96F1638, OP CKS GOOD REPAIRED SEVERED WIRE AT OBSERVERS PHONE JACK. REPLACED MED DOOR STEPS AIRSTAIR TREAD AND LANDING MATS WITH NEW PN ST VINYL BLACK AERMAT PN 1003/1003/20R/54 REPLACED LAV DUMP CABLE WITH NEW PN 565-552-80 AND FLEX HOSE WITH NEW PN CK4X13X1-5 SERVICED NOSE AND BOTH MAIN STRUTS REPLACED HP HYDRAULIC FILTER PN 51143 REPLACED LIGHT TRAP FOR THE AFT INBD FASTEN SEAT BELT/NO SMOKING SIGN WITH NEW PN 1202-100 SEALED VOIDS IN LH WING TKS PANEL AS RQD USING DP-110 REPLACED JUMP SEAT O2 MASK WITH NEW PN C351-2000-205 REPLACED LH AILERON TRIM TAB AFT ROD END BEARINGS WITH NEW, CN6-35MESP56G ADJUSTED MOUNTING POS OF THE #2, #3, AND #4 CABIN OXYGEN MASK BOXES TO ALLOW PROPER CLOSING OF THE BOX COVER PANELS REPLACED AIRBRAKE HYDRAULIC LINE IN RH WHEEL WELL PN 25SW265-159 WITH NEW AND NEW CLIP PN AS4580-2 REPLACED REAR FUSELAGE DRAIN TUBE BOOT WITH NEW PN DO182119-9 PERFORMED DISTRIBUTION CK OF TKS PANELS REPLACED LEFT AND RIGHT ELEVATOR LEADING EDGES WITH NEW LEFT, PN S25TE41365 AND RIGHT PN S25TE4136. PAINTED, BALANCED CK’S BOTH ELEVATORS REPLACED 9 PULLEYS IN THE FLAP SYNCHRONIZATION SYSTEM WITH NEW PN AS111 REPLACED LT AND RT MLG UPPER TORQUE LINK PINS WITH NEW, PN 25-8UM131-11A REPLACED BUSHING, BOLT AND WASHER IN RH MLG REVERSING VALVE LINKAGE, WITH NEW PN S25WS4007, DHS1437-8E, A11OES, AND SP122E REPLACED FH AC GEN BONDING STRAP ASSY PN 25-8EK21-1A Go See maint notes on additional mx documented in Work Order 3123 at Hawker Beech with parts change documented by 8130 records: Replaced APU oil filter pn 179411 Replaced 6 UAM100 fuses Replaced Main Hydraulic system filter PN MFHA189/1A Replaced TKS Filter, PN 19295 Replaced Pn C46P18155-1, #1 engine oil line that supplies reference oil pressure to transducers. 3/11/2008
- 157. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 4/1/2008 AC 810 9.5 810 9.5 6162.8 4203 Total 2423.4 6588 INDEX NUMBER 36 EN1 798 8.2 798 8.2 N1 5925.3 4074 EN2 582 0 801 2.2 N2 6107.8 4177 VENDOR LOG ENTRY READS AS FOLLOWS: WITHAM FIELD AIRCRAFT SERVICES, INC. 2555 SE DIXIE HWY, HANGAR 2 STUART, FL 34996 MAKE: BAE MODEL: 800 SN NA04XX NXXGS DATE: 4/1/2008 LANDINGS: 4199 ACTT: 6157.9 AIRFRAME Replaced #2 static inverter with customer supplied “repaired” unit IAW AMM. Removed P/N 501-1235-01, SN 1709. Installed P/N 501-1235-01, SN 1215. Performed functional test procedure IAW AMM chapter 24-21-17-501, ops cks normal. Signed Joseph Yeft AP 3130427
- 158. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 04/05/2008 AC 810 9.5 810 9.5 6166.3 4207 Total 2426.4 6594 INDEX NUMBER 37 EN1 798 8.2 798 8.2 N1 5928.8 4078 EN2 582 0 801 2.2 N2 6111.3 4181 REPLACED #1 ENGINE OIL FILTER AND PERFORMED S.O.A.P. SAMPLE ON #1 ENGINE, RAN ENGINE, LEAK CKS OK. SOAP SAMPLE SENT TO JET CARE FOR ANALYSIS. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 04/05/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 159. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 04/05/2008 AC 810 9.5 810 9.5 6166.3 4207 Total 2426.4 6594 INDEX NUMBER 38 EN1 798 8.2 798 8.2 N1 5928.8 4078 EN2 582 0 801 2.2 N2 6111.3 4181 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4282 LANDINGS. COMPLETED AFMS TASK 120001, 150 HOUR LUBRICATION THIS DATE PER HAWKER BEECHCRAFT AFMS REV 12. NEXT DUE 150 HOUR LUBE DUE AT 6315 AF HOURS. NEXT DUE 300/600 HOUR LUBE DUE AT 6315 AF HOURS. COMPLETED 150-200 AND THRUST REVERSER INSPECTION PER NORDAM MAINT MANUAL REV 4. NEXT DUE 150-200 HOUR TR INSPECTION AT 6315 AF HOURS. NEXT DUE 300-400 HOUR TR INSPECTION AT 6315 AF HOURS. NEXT DUE 600-800 HOUR TR INSPECTION AT 6330 AF HOURS. LAST COMPLETED 600-800 HOUR TR INSPECTION 7/21/06 AT 5730 AF HOURS. NEXT DUE 1200-1400 HOUR TR INSPECTION AT 6930 AF HOURS. LAST COMPLETED 1200-1400 HOUR TR INSPECTION 7/21/06 AT 5730 AF HOURS. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 04/05/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 160. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 04/10/2008 AC 810 9.5 810 9.5 6172.4 4212 Total 2429.9 6600 INDEX NUMBER 39 EN1 798 8.2 798 8.2 N1 5934.5 4083 EN2 582 0 801 2.2 N2 6117.4 4186 REMOVED AND REPLACED #1 COMM UNIT BECAUSE WEAKER SIGNAL VHF STATIONS DO NOT BREAK SQUELCH. NEW UNIT OP CKS NORMAL. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RCZ-851 7510700-802 95061573 7510700-802 89010256 INSTALLED UNIT PURCHASED FROM DUNCAN AVIATION. COMM UNIT ASSY REPAIRED BY HONEYWELL, 8370 DOW CIRCLE, STRONGSVILLE, OH 44136, CRS# FGNR677K, UNDER WO 5001482997 DATED 1/15/2008. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 04/10/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 161. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 04/11/2008 AC 810 9.5 810 9.5 6180.2 4217 Total 2433.6 6611 INDEX NUMBER 40 EN1 798 8.2 798 8.2 N1 5942.7 4088 EN2 582 0 801 2.2 N2 6125.2 4191 REMOVED AND REPLACED #1 AND #2 MAIN WHEEL BRAKE HEAT PACK ASSY’S PER AMM 32-40-114. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 HEAT PACK AHO89881 122006H AHO89881 NSN #2 HEAT PACK AHO89881 122006I AHO89881 NSN REMOVED #1 AND #2 HEAT PACKS HAD 786 LANDINGS AT REPLACEMENT. INSTALLED ASSY’S PURCHASED FROM ALL WEST AVIATION, OVERHAULED BY RAPCO, INC., 445 CARDINAL LANE, HARTLAND, WI 53029, CRS NE5RO64N, UNDER WO 122006H AND 122006I, BOTH DATED 12/20/2006. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 04/11/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 162. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 04/21/2008 AC 810 9.5 810 9.5 6197.9 4232 Total 2443.6 6632 INDEX NUMBER 41 EN1 798 8.2 798 8.2 N1 5960.4 4103 EN2 582 0 801 2.2 N2 6142.9 4206 REMOVED AND REPLACED #1 RADIO MANAGEMENT UNIT (RMU) BECAUSE LINE SELECT KEY 1L INOP. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RM-850 7012100-806 92030861 7012100-806 89010294 INSTALLED OH RMU PURCHASED FROM DUNCAN AVIATION, OVERHAULED BY HONEYWELL, 8370 DOW CIRCLE, STRONGSVILLE OH, 44136, CRS FGNR677K, UNDER WO 5001420246 DATED 4/18/2008.. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 04/21/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 163. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 04/21/2008 AC 810 9.5 810 9.5 6197.9 4232 Total 2443.6 6632 INDEX NUMBER 42 EN1 798 8.2 798 8.2 N1 5960.4 4103 EN2 582 0 801 2.2 N2 6142.9 4206 REMOVED AND REPLACED #1 FLUX VALVE FOR INTERMITTENT AHARS HDG FLAG. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF FX-600 7010133 88100687 7010133 881000682 INSTALLED FLUX VALVE PURCHASED FROM DUNCAN AVIATION, OVERHAULED BY PACIFIC SOUTHWEST INSTRUMENTS, 1721 RAILROAD ST., CORONA, CA 92880, CRS# KD3R627L, UNDER WO 224511 DATED 4/16/2008. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 04/21/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 164. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" LDGS APU HRS CYCLES EVENT DATE 05/06/2008 AC 810 9.5 810 9.5 6212.5 4245 Total 2457.9 6647 INDEX NUMBER 43 EN1 798 8.2 798 8.2 N1 5975 4116 EN2 582 0 801 2.2 N2 6157.5 4219 REPLACED INOP BEACON/STROBE SW, PN 2TP1-1 WITH NEW, OP CKS OK. REPLACED INOP INSTRUMENT COOLING FAN, BRAILSFORD CO. PN TBL-2.5, OP CKS OK. ACCOMPLISHED 36 MO COMPASS CHECK AFMS TASK 340013. NO DEVIATIONS WITH PRESENT COMPASS CORRECTION CARD FOUND. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 05/06/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 165. Hawker Beechcraft Airframe LogEntry WO# AircraftReg No Aircraft Serial No Hobbs AirframeTT AirframeTC STC A/C TT Date Page 14043999 NXXGS 2581XX 6216.0 4248 5/16/2008 1of1 WO# Sqk_________ - __________________________7) Maintenance Notes____________ ______________________ 14043999 12 REPLACED LAV DUMP CABLE WITH NEW P/N 565-552-80. 14043999 13 RESEALED#1 BRAKE ASSY BY REPLACING P/N DAS2118-9 "O'RINGS. OPS AND LEAK CKED WITH SATISFACTORY RESULTS I certify that with respect to the work performed, this aircraft was repaired and inspected in accordance with current FAA regulations. Only those items specified in the Work Order have been inspected and found to be Airworthy and Returned to Service. No other representations concerning Airworthiness are expressed or implied. Authorized Signature ____________________ printed Name Michael Greer Date 5/16/2008 FAA CRS# VG4R595M EASA U&58BA. Brazllian CHE # 04.10-01/ANAC, Venezuelan OMAC-E #268 Hawker Beechcraft Services Inc., 2450 N. Westshore Blvd., Tampa Florida 33607
- 166. 5/23/2008 TT CYCLES Transcribed#2 Engine Logbook Entry 6167.6 4228 STANDARD AERO AGS DATED 5/23/2008, WORK ORDER #242691 REPAIR STATION GW4R221M DISASSEMBLED #2 ENG AS NECESSARY TO COMPLY WITH SB 72-3558, (CHANGE TURBINE REAR BEARING SUPPORT ASSY) N1 MONOPOLE ASSY., #6 OIL PRESSURE AND SCAVENGE LINES. REASSEMBLED #2 ENGINE, OPERATIONAL CK, LEAK CK; ALL MAINTENANCE AND CHECKS COMPLIED WITH I/A/W FTE 731 L.M.M. AND HAWKER MM PARTS CHANGED #2 ENG (FROM #2 ENG LOG-G. STULTZ) NOMENCLATURE P/N ON S/N ON QTY SEAL RING AS1097-4 NSN 2 TUBE ASSY 3074394-1 NSN 1 TUBE ASSY 3075780-1 NSN 1 PACKING S9413-010 NSN 1 TUBE ASSY BRG SCAVENGE 3074383-1 NSN 1 SUPPORT REAR BEARING 3075444-2 08P04681 1 TRANSDUCER N1 3075388-2 NSN 1 CAMLOCK RECEPTACLE 631-504-9002 8 STUD 682-502-9006 5 WASHER 791-501-9002 5 GASKET 6070461-1 1 RETAINING RING 40G26-1 12 GASKET 3071418-2 1 PACKING M83248/1-010 9 NUTPLATE MS21047L3 1 STUD ASSY AND RECEPTACLE 4002-3SW 1 DUCT BE709-4-30-6 1 THIS AIRCRAFT OR COMPONENT HAS BEEN INSPECTED AND WORK DESCRIBED ABOVE FOUND AIRWORTHY FOR RETURN TO SERVICE. DATED 5/23/2008, WORK ORDER #242691 STANDARD AERO AGS REPAIR STATION GW4R221M 5/23/2008 HAWKER BEECHCRAFT RIGHT ENGINE LOG ENTRY WO# Aircraft Reg No Aircraft Serial No Hobbs AirframeTT AirframeTC Engine S/N ENGINE T.C. Date Page 14044039 NXXGS 2581XX 6222.6 4254 P-91371 4228 5/23/2008 1of1 WO# Sqk MAINTENANCE NOTES 14044039 12 CW #2 ENG DEEC DOWNLOAD 14044039 13 REPLACED R/H ENGINE IGNITER ACCESS PANEL CAMLOCKS PN 682- 502-9006 AND RETAINERS PN 791-501-9002 WITH NEW CAMLOCKS AND RETAINER SAME PNs
- 167. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" LDGS APU HRS CYCLES EVENT DATE 05/28/2008 AC 810 9.5 810 9.5 6230.7 4261 Total 2468.1 6669 INDEX NUMBER 44 EN1 798 8.2 798 8.2 N1 5993.2 4132 EN2 582 0 801 2.2 N2 6175.7 4235 SOAP SAMPLES TAKEN FOR #1 AND #2 ENGINES, NEW OIL FILTERS, PN 3070945-1, O RING PN S9413-06 INSTALLED, RAN BOTH ENGINES TO LEAK CHECK NEW FILTERS, CKS OK. SERVICED OIL LEVEL TO FULL. DEEC DOWNLOAD THIS DATE, NEXT DUE ~6270 AFTT UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 05/28/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 168. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 05/28/2008 AC 810 9.5 810 9.5 6230.7 4261 Total 2468.1 6669 INDEX NUMBER 45 EN1 798 8.2 798 8.2 N1 5993.2 4132 EN2 582 0 801 2.2 N2 6175.7 4235 REPLACED LEAKING #1 BRAKE PISTON CYLINDER ASSY, FORWARD MIDDLE POSITION. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF CYLINDER LINER ASSY AHO88413 NSN AHO88413 NSN INSTALLED CYLINDER LINER ASSY PURCHASED FROM ALL WEST AVIATION, OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3151, DATED 6/10/07. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 05/28/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 169. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 05/28/2008 AC 810 9.5 810 9.5 6230.7 4261 Total 2468.1 6669 INDEX NUMBER 46 EN1 798 8.2 798 8.2 N1 5993.2 4132 EN2 582 0 801 2.2 N2 6175.7 4235 #1 AND #2 MAIN WHEEL AND TIRE ASSYS REPLACED FOR TIRE WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA 1814 SL105 AHA1814 XB003 #2 MAIN WHEEL ASSY AHA 1814 LR165 AHA1814 XB007 INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3435, DATED 02/29/2008 UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 05/28/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 170. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 05/28/2008 AC 810 9.5 810 9.5 6230.7 4261 Total 2468.1 6669 INDEX NUMBER 47 EN1 798 8.2 798 8.2 N1 5993.2 4132 EN2 582 0 801 2.2 N2 6175.7 4235 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4336 LANDINGS. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 05/28/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 171. 6/14/2008 TT CYCLES Transcribed#1 Engine Logbook Entry 6005.4 4141 Disassembled Engine As Necessary To Perform The Following Maintenance Due To Bad Soap: o Removed Accessory Gear Box Drive Shafts, Cleaned, and Inspected. o C/W S/B TFE731-72-3696 Installed 1 Each New Air-Oil Separator Element P/N 3075781-1 and Reassembled Accessory Gearbox. o C/W S/B TFE731-72-3739, Installed 1Each New No.1 Carbon Seal P/N 3060457-1, S/N 08- 05158-13844. o C/W S/B TFE731-72-3739, Installed 1Each New No.3 Carbon Seal P/N 3060458-1, S/N 08- 05158-15895. o Installed 1Each New No.3 Bearing Spacer P/N 3070119-2. o Installed 2 Each New Pinion Gear Damper Rings, 1 Each P/N 3075280-1 and 3075280-2. Balanced As Required. o Installed 1 Each Overhauled Ring Gear P/N 3077075-1, S/N 7P-13349, and 1 Each New Ring Gear Retainer P/N 3075377-1. o Performed Engine Oil Change, and Oil Filter Change; Serviced Engine With Mobil 254 Oil. o Reassembled Engine, Performed Ground Run, Ops and Leak Checks, Breather Pressure Checks, and Performed A Vibration Survey With All Results Satisfactory. o All Work Accomplished Per TFE731-5 and Hawker 800 Maintenance Manuals. This aircraft or component has been inspected and work described above found airworthy for return to service. Date: June 14, 2008, Signed: Ronald M Herndon for StandardAero CRS# GW4R221M Augusta , GA 30906 THIS AIRCRAFT OR COMPONENT HAS BEEN INSPECTED AND WORK DESCRIBED ABOVE FOUND AIRWORTHY FOR RETURN TO SERVICE. DATED 5/23/2008, WORK ORDER #242691 STANDARD AERO AGS REPAIR STATION GW4R221M 6/14/2008
- 172. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 07/25/2008 AC 810 9.5 810 9.5 6268.4 4292 Total 2491.6 6717 INDEX NUMBER 48 EN1 798 8.2 798 8.2 N1 6030.9 4163 EN2 582 0 801 2.2 N2 6213.4 4266 FWD AND AFT EMERGENCY EXIT LIGHT POWER SUPPLY NI-CAD D CELLS (4) REPLACED WITH NEW, PN 25503-025, NSN, SYSTEM TESTED. C/W AFMS TASK 335010 PERFORMED 400 HOUR DETAILED WALK AROUND INSPECTION C/W AFMS TASK 050800 ICE PROTECTION SYSTEM RQMTS OF AFMS TASK 3000007 MET BY CREW USE OF TKS SYSTEM. APU SEMI ANNUAL/125 HR/250 CYCLE INSPECTION C/W AFMS TASK 492001 APU SEMI ANNUAL/250 HR/500 CYCLE INSPECTION C/W AFMS TASK 492001 AD 2008-06-28, REGARDING AVIDYNE PRIMARY FLIGHT DISPLAYS, RESEARCHED AND FOUND NA TO INSTALLED SYSTEMS. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 07/25/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 173. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 07/28/2008 AC 810 9.5 810 9.5 6268.4 4292 Total 2491.6 6717 INDEX NUMBER 49 EN1 798 8.2 798 8.2 N1 6030.9 4163 EN2 582 0 801 2.2 N2 6213.4 4266 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4367 LANDINGS. FIRST OFFICER “B” SCREEN WINDOW IS DELAMINATED BEYOND ALLOWABLE LIMITS. REMOVED OLD WINDOW AND INSTALLED NEW WINDOW PER AMM 56-10- 22, OP AND LEAK CKS UNDER PRESSURIZATION OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF WINDSCREEN, RH NH24016-92 L369711 NH24016-92 L292142M INSTALLED WINDSHIELD PURCHASED FROM DUNCAN AVIATION, MANUFACTURED NEW BY GKN AEROSPACE TRANSPARENCY SYSTEMS, LONDON LUTON AIRPORT, LUTON BEDFORDSHIRE LU2 9PQ, CERTIFICATE/APPROVAL NO. UK.145.01142, UNDER WO 37/140928 DATED 17/12/2007. OLD WINDOW WAS INSTALLED ON 6/27/1997 AND HAD 2943 HOUR LIFE. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 07/28/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 174. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 07/28/2008 AC 810 9.5 810 9.5 6268.4 4292 Total 2491.6 6717 INDEX NUMBER 50 EN1 798 8.2 798 8.2 N1 6030.9 4163 EN2 582 0 801 2.2 N2 6213.4 4266 SOAP SAMPLES TAKEN FOR #1 AND #2 ENGINES, NEW OIL FILTERS, PN 3070945-1, O RING PN S9413-06 INSTALLED, RAN BOTH ENGINES TO LEAK CHECK NEW FILTERS, CKS OK. SERVICED OIL LEVEL TO FULL. NORMAL RESAMPLE DUE AT AFTT 6418 DEEC DOWNLOAD THIS DATE, NEXT DUE ~AFTT 6308 UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 07/28/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 175. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 08/05/2008 AC 810 9.5 810 9.5 6269.3 4295 Total 2492.6 6720 INDEX NUMBER 51 EN1 798 8.2 798 8.2 N1 6031.8 4166 EN2 582 0 801 2.2 N2 6214.3 4269 COMPLETED AFMS TASK 320036, BRAKE WEAR CHECK POSITIONS #1, #2, #3 & #4, ALL UNITS WITHIN WEAR LIMITS PER AFMS 32-20-114. NEXT DUE AT 4370 LANDINGS. REMOVED AND REPLACED #3 AND #4 MAIN WHEEL BRAKE HEAT PACK ASSY’S PER AMM 32-40-114. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 HEAT PACK AHO89881 011007H AHO89881 NSN #4 HEAT PACK AHO89881 011007I AHO89881 NSN REMOVED #3 AND #4 HEAT PACKS HAD 864 LANDINGS AT REPLACEMENT. INSTALLED ASSY’S PURCHASED FROM ALL WEST AVIATION, OVERHAULED BY RAPCO, INC., 445 CARDINAL LANE, HARTLAND, WI 53029, CRS NE5RO64N, UNDER WO 011007H AND 011007I, BOTH DATED 1/12/2007. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/05/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 176. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 08/05/2008 AC 810 9.5 810 9.5 6269.3 4295 Total 2492.6 6720 INDEX NUMBER 52 EN1 798 8.2 798 8.2 N1 6031.8 4166 EN2 582 0 801 2.2 N2 6214.3 4269 #3 AND #4 MAIN WHEEL AND TIRE ASSYS REPLACED FOR WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 MAIN WHEEL ASSY AHA 1814 XB003 AHA1814 LC290 #4 MAIN WHEEL ASSY AHA 1814 XB007 AHA1814 WW032 BOTH WHEELS SB 32-1374 & SB 32-3746 CW. REMOVED TIRES HAD 170 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 33625, DATED 07/11/2008 UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/05/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 177. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 08/11/2008 AC 810 9.5 810 9.5 6269.3 4295 Total 2492.6 6720 INDEX NUMBER 53 EN1 798 8.2 798 8.2 N1 6031.8 4166 EN2 582 0 801 2.2 N2 6214.3 4269 BRAKES DRAG ON #3 AND #4 BRAKES. REMOVED AND REPLACED #3 AND #4 MAIN WHEEL BRAKE UNITS PER AMM 32-40- 114. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 BRAKE UNIT AHA1897 ZV109 AHA 1288 KV116 #4 BRAKE UNIT AHA1897 ZX182 AHA 1288 LC370 INSTALLED BRAKE ASSY’S PURCHASED OVERHAULED FROM COSGROVE AIRCRAFT SERVICE, INC, 6 LOOP ROAD, BUILDING #2, WESTCHESTER COUNTY AIRPORT, WHITE PLAINS NY, 10604 UNDER WO# 41702 (SN ZV109) DATED 04/23/2008 AND WO# 41638Z (SN ZX182) DATED 03/03/2008. #3 AND #4 MAIN WHEEL AND TIRE ASSYS REMOVED AND RE-INSTALLED PER AMM 32-40-12. MAIN WHEELS INSPECTED AND TIRES REPLACED BY COSGROVE AIRCRAFT SERVICES UNDER WO# 42966 AND WO# 42967 BOTH DATED 08/07/08. BOTH WHEELS DUNLOP SB 32-1360 CW. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/11/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 178. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 08/13/2008 AC 810 9.5 810 9.5 6269.3 4295 Total 2492.6 6720 INDEX NUMBER 54 EN1 798 8.2 798 8.2 N1 6031.8 4166 EN2 582 0 801 2.2 N2 6214.3 4269 APU ANNUAL/500 HR/1000 CYCLE INSPECTION CW AFMS TASK 492003 APU ANNUAL/1000 HR/2000 CYCLE INSPECTION CW AFMS TASK 492004 APU BIENNIAL /1500 HR/3000 CYCLE INSPECTION CW AFMS TASK 492005. OIL FILTER CHANGE RQD BY BIENNIAL INSPECTION PCW ON 3/27/08 WITH PN 169009-1 INSTALLED BY HAWKER BEECHCRAFT. OIL FILTER NEXT DUE AT 2915 HOURS OR NEXT BIENNIAL INSPECTION. RAN APU FOR FUNCTION AND LEAK CK, OPS OK. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/13/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 179. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 08/18/2008 AC 810 9.5 810 9.5 6269.3 4295 Total 2492.6 6720 INDEX NUMBER 55 EN1 798 8.2 798 8.2 N1 6031.8 4166 EN2 582 0 801 2.2 N2 6214.3 4269 CW MANDATORY SB 35-3886, ISSUED JULY 2008. AIRCRAFT IS IN COMPLIANCE WITH SB PARAGRAPH 1 A 1, NA BY EFFECTIVITY CLAUSE, PART INSTALLED WAS PURCHASED BEFORE JUNE 1, 2006. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 08/18/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 180. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 09/05/2008 AC 810 9.5 810 9.5 6286.1 4312 Total 2504.0 6740 INDEX NUMBER 56 EN1 798 8.2 798 8.2 N1 6048.6 4183 EN2 582 0 801 2.2 N2 6231.1 4286 COMPLETED AFMS TASK 240001 ON LT AND RT STARTER GENERATORS IN CONJUNCTION WITH 300 TO 400 HOUR ENGINE ROUTINE PERIODIC INSPECTION. NEXT DUE IN 300 HOURS AT 6586 AFTT. COMPLETED AFMS TASK 720005, 150 TO 200 HOUR ENGINE ROUTINE PERIODIC INSPECTION, LT AND RT ENGINES. NEXT DUE IN 150 HOURS AT 6436 AFTT. COMPLETED AFMS TASK 720011, 300 TO 400 HOUR ENGINE ROUTINE PERIODIC INSPECTION LT AND RT ENGINES. NEXT DUE IN 300 HOURS AT 6586 AFTT. COMPLETED AFMS TASK 783003, 150 TO 200 HOUR THRUST REVERSER INSPECTION, LT ENGINE. NEXT DUE IN 150 HOURS AT 6436 AFTT. COMPLETED AFMS TASK 783004, 150 TO 200 HOUR THRUST REVERSER INSPECTION, RT ENGINE. NEXT DUE IN 150 HOURS AT 6436 AFTT. COMPLETED AFMS TASK 783007, 300 TO 400 HOUR THRUST REVERSER INSPECTION, LT ENGINE. NEXT DUE IN 300 HOURS AT 6586 AFTT COMPLETED AFMS TASK 783008, 300 TO 400 HOUR THRUST REVERSER INSPECTION, RT ENGINE. NEXT DUE IN 300 HOURS AT 6586 AFTT. COMPLETED AFMS TASK 21015, DUCT TEMP OVERHEAT SWITCHES, PN 156D05, SN 803L AND 803R, BENCH CHECK, PER KIDDE-GRAVINER CMM 26-12-70, DATED SEPT 1997. OK FOR SERVICE. NEXT DUE IN 60 MONTHS, 09/05/2013. SOAP SAMPLES TAKEN FOR #1 AND #2 ENGINES, NEW OIL FILTERS, PN 3070945-1, O- RING PN S9413-06 INSTALLED, RAN BOTH ENGINES TO LEAK CHECK NEW FILTERS, CKS OK. SERVICED OIL LEVEL TO FULL. NORMAL RESAMPLE NEXT DUE IN 150 HOURS AT 6436 AFTT. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 09/05/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 181. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 09/09/2008 AC 810 9.5 810 9.5 6289.9 4318 Total 2509.2 6749 INDEX NUMBER 57 EN1 798 8.2 798 8.2 N1 6052.4 4188 EN2 582 0 801 2.2 N2 6234.9 4291 LT AND RT NLG TIRES WORN. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LT NLG WHEEL AND TIRE ASSY AH52339 LS064 AH52339 DW061 RT NLG WHEEL AND TIRE ASSY AH52339 LS069 AH52339 149-1045 TIRES HAD 161 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3584, DATED 06/03/2008 UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 09/09/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 182. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 09/25/2008 AC 810 9.5 810 9.5 6292.9 4322 Total 2512.0 6755 INDEX NUMBER 58 EN1 798 8.2 798 8.2 N1 6055.4 4192 EN2 582 0 801 2.2 N2 6237.9 4295 AFMS TASK 334009, TAIL STROBE INTENSITY CHECK CW BY REMOVAL AND REPLACEMENT WITH NEW TAIL STROBE/POSITION LIGHT ASSY. OP CKS OK NEXT DUE INTENSITY CK IN 1500 HOURS, AT 7792 AFTT NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF REAR POSITION LIGHT ASSY 30-0516-1 7045 30-0516-1 8654 INSTALLED REAR POSITION LIGHT PURCHASED FROM ALL WEST, OVERHAULED BY KELLY AEROSPACE TURBINE ROTABLES, 3414 WEST 29TH ST. SOUTH WICHITA KS 67217, CRS NV2R045L UNDER WO APS-30286, DATED 03/12/2008. BULB PN W678 COMPLETED AFMS TASK 783011, 600 TO 800 HOUR THRUST REVERSER INSPECTION, LT ENGINE. NEXT DUE IN 600 HOURS AT 6892 AFTT. COMPLETED AFMS TASK 783012, 600 TO 800 HOUR THRUST REVERSER INSPECTION, RT ENGINE. NEXT DUE IN 600 HOURS AT 6892 AFTT. COMPLETED AFMS TASK 320036.1, CK OF #1 BRAKE FOR WEAR, NEXT DUE AT 4397 LANDINGS. COMPLETED AFMS TASK 320036.2, CK OF #2 BRAKE FOR WEAR, NEXT DUE AT 4397 LANDINGS. UPDATED AVTRAK SYSTEM RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 09/25/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 183. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 10/06/2008 AC 810 9.5 810 9.5 6301.3 4331 Total 2519 6766 INDEX NUMBER 59 EN1 798 8.2 798 8.2 N1 6063.8 4201 EN2 582 0 801 2.2 N2 6246.3 4304 INSTALLED TWO CONCORDE RG-390E MAIN SHIP BATTERIES PURCHASED NEW FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE., AZUSA, CA 91702 NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 BATTERY RG-390E 40251513 RG-390E 40195945 #2 BATTERY RG-390E 40251482 RG-390E 40190737 BATTERY #1 & #2 SWAP IN 3 MOS RECOMMENDED DUE 1/6/2009. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/06/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 184. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M LDGS APU HRS CYCLES EVENT DATE 10/16/2008 AC 810 9.5 810 9.5 6307.8 4337 Total 2519 6766 INDEX NUMBER 60 EN1 798 8.2 798 8.2 N1 6070.3 4207 EN2 582 0 801 2.2 N2 6252.8 4310 RESEARCHED AD 2008-21-01 AND FOUND THIS AIRCRAFT COMPLIANT PER HB SB 32-3920 EFFECTIVITY STATEMENT. UPDATED AVTRAK RECORDS, TASK CODE 990471, NO FURTHER ACTION REQUIRED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/10/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 185. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 10/16/2008 AC 810 9.5 810 9.5 6307.8 4337 Total 2519 6766 INDEX NUMBER 61 EN1 798 8.2 798 8.2 N1 6070.3 4207 EN2 582 0 801 2.2 N2 6252.8 4310 RESEARCHED AD 2008-19-12, EFFECTIVE 10/27/2008. BOTH ENGINES ON THIS AIRCRAFT ARE AFFECTED BY THIS AD DUE TO PN 3074766-1 ITT DUCTS INSTALLED. PER PARA (e) OF AD WILL SCHEDULE ITT DUCT CHANGE AT NEXT CZI, ACCESS OR 2600 ( 8915 AFTT )HOURS FROM EFFECTIVE DATE OF AD 2008-19-12 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 10/10/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ 10/21/2008 AFTT CYCLES Transcribed #1 Engine, SN P-91363 logbook 871 380 SB TFE731-72-A3748 DETERMINED NA DATE 10/21/2008 SIGN CERT NO: A&P 121480127 GREGORY A. STULTZ
- 186. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 11/26/2008 AC 810 9.5 810 9.5 6343.9 4372 Total 2543.3 6812 INDEX NUMBER 62 EN1 798 8.2 798 8.2 N1 6106.4 4345 EN2 582 0 801 2.2 N2 6288.9 4345 COMPLETED AFMS TASK 320036.1, CK OF #1 BRAKE FOR WEAR, NEXT DUE AT 4447 LANDINGS. COMPLETED AFMS TASK 320036.2, CK OF #2 BRAKE FOR WEAR, NEXT DUE AT 4447 LANDINGS. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 11/26/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 187. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 11/26/2008 AC 810 9.5 810 9.5 6346.9 4374 Total 2543.3 6812 INDEX NUMBER 63 EN1 798 8.2 798 8.2 N1 6109.4 4244 EN2 582 0 801 2.2 N2 6291.9 4347 MX LOG ENTRY BY STANDARD AERO: Aircraft Logbook Entry Easton Flying Partners Hawker 800A DATE: 11/26/200 NXXGS ACTT: 6346.9 S/N: 2581XX LDGS: 4374 W/O#: 251523 1. Performed the following miscellaneous maintenance: Installed new customer furnished right fire bell cancel switch p/n 99-222. This aircraft or component has been inspected and work described above found airworthy for return to service. WO# 251523 Date 11/26/2008 Signed Brian J. Zicari for CRS# GW4R221M, Augusta, Ga. 30906 THIS AIRCRAFT OR COMPONENT HAS BEEN INSPECTED AND WORK DESCRIBED ABOVE FOUND AIRWORTHY FOR RETURN TO SERVICE. Wo 251533 SIGNED BRIAN ZICARI FOR STANDARD AERO CRS# GW4R221M.
- 188. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 12/12/2008 AC 810 9.5 810 9.5 6369.1 4395 Total 2558.2 6843 INDEX NUMBER 64 EN1 798 8.2 798 8.2 N1 6131.6 4365 EN2 582 0 801 2.2 N2 6314.1 4368 CW AFMS TASK 245006, REMOVE AND REPLACE #2 WILD FREQUENCY AC ALTERNATOR FOR TIME, IAW AMM 24-22-21-401. RAN #2 ENGINE TO TEST ALTERNATOR UNDER LOAD. OP CKS OK. INSTALLED AC GENERATOR OVERHAULED BY DUNCAN AVIATION, LINCOLN AIRPORT, LINCOLN, NE, 68524. CRS# JGVR194F UNDER WO# T376A, DATED 07/14/2008 NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 AC ALTERNATOR BA02801-1 1860 BA02801-1 1323 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/12/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 189. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 12/16/2008 AC 810 9.5 810 9.5 6369.1 4395 Total 2558.2 6843 INDEX NUMBER 65 EN1 798 8.2 798 8.2 N1 6131.6 4365 EN2 582 0 801 2.2 N2 6314.1 4368 REMOVED #4 AUX BATTERY AND INSTALLED NEW. INSTALLED BATTERY PURCHASED NEW FROM FALCON CREST AVIATION, 8318 BRANIFF, HOUSTON, TX 77061 NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF CONCORDE SEALED LEAD ACID BATTERY #4 AUX RG-126 40280430 RG-126 CBC-404429 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/16/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 190. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 12/19/2008 AC 810 9.5 810 9.5 6373.8 4398 Total 2559.2 6846 INDEX NUMBER 66 EN1 798 8.2 798 8.2 N1 6136.3 4368 EN2 582 0 801 2.2 N2 6318.8 4371 REMOVED AND REPLACED CAPTS EMERGENCY OXYGEN MASK. OP CK OF MASK, OXYGEN FLOW AND COMMUNICATIONS OK FOR SERVICE. INSTALLED MASK BOUGHT FROM BUSINESS AEROTECH, OVERHAULED BY AMERON GLOBAL PRODUCT SUPPORT, 1350-2 LINCOLN AVE, HOLBROOK, NY 11741, CRS OVVR461N UNDER WO# 19654 DATED 12/18/2008. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF EMERGENCY OXYGEN MASK CAPT MC10-14-124 63721 MC10-14-51 19244 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/19/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 191. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 12/22/2008 AC 810 9.5 810 9.5 6380.1 1 4403 Total 2561.2 6848 INDEX NUMBER 67 EN1 798 8.2 798 8.2 N1 6142.6 4273 EN2 582 0 801 2.2 N2 6325.1 4376 CREW REPORTS INSTANCE OF TOTAL FAILURE OF #1 AHARS SYSTEM, REVERSION MODE OPS NORMAL. TROUBLESHOOTING INDICATES FAILURE OF AHARS UNIT AH-600. REMOVED AND REPLACED #1 ATTITUDE HEADING AND REFERENCE UNIT PER HONEYWELL SYSTEM MAINT MANUAL 22-16-00 PG 702, OP CKS OK. UNIT PURCHASED THROUGH DUNCAN AVIATION, LINCOLN NE. UNIT PREVIOUSLY REPAIRED BY HONEYWELL, 7227 W. HARRY, WICHITA, KS 67209, CRS LV2R992K UNDER WO# 5002185707 DATED 12/08/2008. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF AH-600 AHARS #1` 7003360-943 86090540 7003360-943 88121186 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/22/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 192. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin LDGS APU HRS CYCLES EVENT DATE 12/30/2008 AC 810 9.5 810 9.5 6380.1 1 4403 Total 2561.9 6852 INDEX NUMBER 68 EN1 798 8.2 798 8.2 N1 6142.6 4273 EN2 582 0 801 2.2 N2 6325.1 4376 COMPLETED 200 HOUR AIRFRAME LUBRICATION, AVTRAK TASK 050050, PER AMM 007-001-001. NEXT DUE AT 6580 AFTT. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/30/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 193. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 12/31/2008 AC 810 9.5 810 9.5 6380.1 1 4403 Total 2561.9 6852 INDEX NUMBER 69 EN1 798 8.2 798 8.2 N1 6142.6 4273 EN2 582 0 801 2.2 N2 6325.1 4376 REMOVED AND RE-INSTALLED SERVICEABLE AUX BATTERIES #3 AND #4 AND IRS BATTERY AFTER CAPACITANCE CK. AVTRAK TASKS 241017, 241019 AND 241030 RESPECTIVELY. NOMENCLATURE POSITION P/N S/N ON AUX BATTERY #3 UJ RG-126 40126243 AUX BATTERY #4 UL RG-126 40184860 IRS BATTERY IRS CA-54-1 10300827 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 12/31/2008 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 194. Standard Aero MaintenanceLog Entry Dated 1/29/2009 NXXGS 6390.1 4276 1/29/2009 -Removed the existing IRS standby power supply (battery) while retaining the mounting try and wiring. Installed into the IRS system standby power supply mounting tray a Concorde model RG-131 power supply in accordance with Standard Aero drawing. Maintenance Manual Supplement, Instructions for Continued Airworthiness, as issued to BAE 125 Series 800A s/n 2581XX (NA04XX), Standard Aero document 1016360 Rev. (A) was provided. Reference FAA Form 337 dated 1-29-09 for details. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF SEALED LEAD ACID BATTERY IRS RG-131 40273576 CA-54-1 10300827 -Complied with the following “Structural” Inspection codes: 260001 (Functional test fire extinguishers) 320032 (Comply with main landing gear fairing strut) 510002 (Front pressure bulkhead) 510003 (Inspect windshields) 510009 (Entry door surround) 520008 (Inspect main entry door) 530001 (Skin exterior under the dorsal intake, forward of frame 19) 530002 (Fuselage skin under wing-to-fuselage panels) 530003 (Wing to fuselage attachment links, brackets and bolts) 530011 (Front face of rear pressure bulkhead) 550001 (Inspect horizontal stabilizer rear attachment fitting) 550006 (Inspect elevators) 550007 (Detail inspect Elevators) 550009 (Detail inspect rudder) 550010 (Comply with inspection of rudder trim rods) 550011 (Inspect rudder) 550015 (Inspect elevators) 570007 (Inspect wing bottom skins and stringers between the front and rear spars) 570008 (Main landing gear and Sidestay attachment fittings) 570012 (Inspect wing rear spar, rear face) 570013 (Detail inspect airbrakes) 570014 (Detail inspect ailerons-hinge brackets) 570015 (Detail inspect ailerons) 570016 (Lubricate/replace the front and rear rod end bearings) 570017 (Inspect flaps and flap vanes) 570030 (Inspect aileron outboard hinge castings) -Complied with the following “Out of Phase” inspection code: 210006 (Inspect water separator) ATA 8 -Weighed aircraft using Revere Electronic weight scale p/n C55805-3-25, s/n 4712 calibration due date 9/22/09. Revised weight/balance book. STANDARD CONFIGURATION LH WING: 6000 LBS, RH WING: 6024 LBS, TAIL: 4120 LBS = 16145 CUSTOM CONFIG LH WING: 6060 LBS, RH WING 6096 LBS, TAIL: 4107 LBS = 16263 ATA 21 -Removed and replaced cabin NRV p/n AWE124-51A s/n 8802019 with s/n RR239 after overhaul by APPH Houston, Inc. ATA 24 -INVESTIGATE EXTERNAL POWER INTERMITTENTLY SLOW TO ENGAGE
- 195. STARTED TS BYREMOVING RELAY CP FROM ZK PNL, BENCH CKD OK. MEASURED CONTINUITY FROM THE EXTERNAL POWER RECEPTACLE SMALL PIN TO PIN B1 ON RELAY CP BASE. FLEXED THE AREA AROUND FUSE GA-F1 AND DIODE GG-DA AND WIRING ON THE TERMINAL C5 OF THE INTERNAL START CONTACTOR ZL-U, CKS OK. CONTINUITY CK FROM EXT PWR SMALL PIN TO X1 ON CP BASE, MANIPULATED EXTERNAL PWR SW CG-EL 3 TIMES, WHILE IT WAS ON, TAPPED ON THE INTERNAL START CONTACTOR AND FLEXED TERMINAL C4. THIS CIRCUIT CHKD OK. FROM X2 OF THE CP BASE CKD CONTINUITY TO GND CYCLED THE EXTERNAL PWR SW 3 TIMES, CONTINUITY CKD OK. CHKD CONTINUITY FROM B2 OF CP BASE TO THE TERMINAL T OF THE OVERVOLT SENSOR GA-V, READ THE CONTINUITY FO THE GND PWR RELAY COIL GA-E FLEXED THE WIRES AT TERMINAL ONE AND TWO OF GA-E, CKD CONTINUITY FROM TERMINAL P OF THE OVERVOLT SENSOR TO GND. CYCLED THE EXTERNAL PWR SW 3 TIMES, GOOD GRND. CKD CONTINUITY FROM THE EXTERNAL POWER RECEPTACLE POWER PIN TO TERMINAL S OF THE OVERVOLT SENSOR. HAD ABOUT 10K OHMS, SHOULD HAVE BEEN ABOUT 15 OHMS. FLEXED THE WIRING FROM THE TERMINAL A2/B2/C2 OF THE INTERNAL START CONTACTOR TO TERMINAL S . REMOVED THE COVER FROM DIODE GA-W . WHEN THE ANODE OF DIODE W WAS PRESSED THE CONTINUITY DROPPED TO 15 OHMS. THERE DID NOT APPEAR TO BE A CRACKED SOLDER JOINT AS THE ANODE POST OF THE DIODE WAS JUST LOOPED AROUND TERMINAL POST 1. REMOVED THE TERMINAL POST 1 NUT, INSP THE TERMINAL 1 NUT WAS SLIGHTLY LOOSE, INSTALLED THE DIODE COVER AND RELAY ZK-CP, CONNECTED TO EXTERNAL PWR, OPS CKS OK. -Removed and replaced aft bay door micro switch p/n V3L-3013-D8 with new switch p/n V7- 6C17D8-048-1. -Removed and reinstalled No. 1 FMS NZ-2000 p/n 7018879-03022, s/n 98082029 and No. 2 FMS NZ-2000 p/n 7018879-03022, s/n 96091165 after replacing batteries with new batteries p/n 09-3642-002. NEXT DUE REPLACEMENT IN 1/31/2011. (previously used pn replaced 7020116-1, two of each) ATA 26 -Complied with test of all 6 ea. equipment bay overhead BAY OVERHEAT detector switches. ATA 27 -Removed and replaced flap sync cables with the following new cables and part numbers: L/H aft inboard p/n 25CF3455-17A, L/H forward inboard p/n 25CF3455-19A, L/H forward outboard p/n 25CF3455-7A, L/H aft outboard p/n 25CF3455-3A, R/H forward inboard p/n 25CF3455-11A, R/H aft inboard p/n 25CF3455-9A, R/H forward outboard p/n 25CF3455-13A, R/H aft outboard p/n 25CF3455-11A. -Removed and replaced L/H and R/H aileron trim actuator bolts, bushings and nuts with new bolts p/n DHS1432-8EE, new bushings p/n 25WG177 and new nuts p/n A110ES. -Removed and replaced R/H flap outboard hinge fairing brackets with 2 ea. new hinge brackets p/n 25-8WS2093-1A. -Removed and reinstalled L/H flap screw jack p/n 25-8CW159A/B s/n MEC/DHB/199 after overhaul by Midcoast Aviation, Inc. -Removed and replaced L/H elevator trim aft rod end bearings with 2 ea. new bearings p/n CN6-33MESO56G. -Removed and replaced R/H aileron servo tab aft rod end bearings with 2 ea. new bearings p/n CN6-35MESP56G. -Removed and replaced R/H elevator tab aft rod bearings with 2 ea. new bearings p/n CN6- 35MESP56G. -Removed and replaced L/H and R/H aileron center hinge bolts and nuts with 2 ea. new bolts p/n 25-8WG45-3 and 2 ea. new nuts p/n A103GS. ATA 28 -Removed and replaced 6 ea. manhole cover seals with 6 new seals p/n 25WS619. ATA 29 -Removed and reinstalled upper full flow relief valve p/n 45394 s/n LK8708982 after overhaul by Midcoast Aviation, Inc. -Removed and reinstalled lower full flow relief valve p/n 45394 s/n LK8709033 after overhaul by Midcoast Aviation, Inc. -Removed and replaced RETURN quick disconnect fitting with new fitting p/n T015519S4- 12D. ATA 32 -LH AND RH MLG SIDE STAY SHORT LINKS AND BUSHINGS ARE WORN AND ROLLER CLEARANCES ARE
- 196. OUT OF TOLERANCE.REMOVED LH MLG SIDESTAY LOCKING LEVER ASSY. REMOVED OLD BUSHING AND SHORT LINK. INSTALLED NEW SHORT LINK ASSY PN 25-8UM79-1A, ONE EA AND NEW LEVER BUSHING PN 25UM379, 1 EA. REINSTALLED LOCKING LEVER ASSY AND ADJUSTED ROLLER CLEARANCES AS REQUIRED. REMOVED RH MLG SIDESTAY LOCKING LEVER ASSY. REMOVED OLD BUSHING AND SHORT LINK. INSTALLED NEW SHORT LINK ASSY PN 25-8UM79-1A, ONE EA AND NEW LEVER BUSHING PN 25UM379, 1 EA. REINSTALLED LOCKING LEVER ASSY AND ADJUSTED ROLLER CLEARANCES AS REQUIRED. -Removed and replaced emergency reducing valve knife edges with 1 ea. new p/n ACO34629 and 1 ea. new p/n ACO34630 -FOUND LH AND RH MLG SIDESTAY LOWER PIVOT NUTS LOOSE, COULD NOT ACHIEVE PROPER TORQUE ON NUTS WITH EXISTING NUTS AND SPLIT HOLES. REDRILLED LH AND RH SIDESTAY LOWER FITTINGS AT 90 DEGREES TO ACHIEVE PROPER TORQUE ON NUTS. REINSTALLED LH AND RH SIDESTAYS. Removed and replaced L/H and R/H lower sidestay shims using new shims p/n 25UM1153. Assembled R/H sidestay with new bottle bolt p/n 25- 8UM37. -Removed and reinstalled landing gear selector dump valve p/n AIR45406-1 s/n LK0307 after overhaul by Midcoast Aviation, Inc. ATA 33 -Removed and replaced overhead panel overlay bulbs with 38 ea. new bulbs p/n 6838. -Removed and replaced fire control panel overlay bulbs with 12 ea. new bulbs p/n 6838. -Removed and replaced APU control panel overlay bulbs with 3 ea. new bulbs p/n 6838. -Removed and replaced No. 2 inverter fail enunciator light bulbs with 2 ea. new bulbs p/n 327. -Removed and replaced overhead emergency light off indication bulb with new bulb p/n 6838. -Removed and replaced No. 1 ignition light cover with new cover p/n BEPB-A07-ABP. ATA 34 -Complied with ELT test. -Removed the existing IRS standby power supply (battery) p/n CA-54-1 s/n 10300827 and installed serviceable Concorde model RG-131 s/n 40273576. ATA 35 -Removed and reinstalled hydrostatic portable oxygen bottle p/n 176965-SMB3 s/n 620814 after inspection by Ameron Global Product Support. Note: Next hydrotest due January 2014. ATA 52 -Removed and replaced cabin window desiccant with new desiccant p/n S162-500. -Repaired main entrance door by fabricating all parts in accordance with Structural Repair Manual 52-10-11. -Removed and replaced door bumper with new bumper (CAP) p/n 25FC2943. ATA 53 -Repaired R/H main wheel well tub in accordance with Structural Repair Manual 53-20-12. ATA 57 -Removed and replaced L/H and R/H flap hinge bolts and nuts with new hinge bolts 2 ea. p/n A112-12J, new 2 ea. nuts p/n A110JS and inboard 2 ea. new bolts p/n DHS1432-15GG and 2 ea. new nuts p/n A110GS. ATA-78 REPLACED #1 TR FAN FLAP SW. TR WOULD DEPLOY, BUT THE DEPLOY LIGHT WOULD NOT COME ON AND THE PIGGY BACK REMAINED LOCKED OUT. GAINED ACCESS TO CONNECTORS P813 AND P815 ON THE #1 TR DISCONNECTED THEM. FROM P815 CHKD CONTINUITY OF THE DEPLOYED MICROSWITCH S7, AND THE UPPER FAN MICRO SW S9, CKS OK. FROM CONNECTOR P813 CKD CONTINUITY OF THE LOWER FAN FLAP, S8, FOUND DEFECTIVE AND CHANGED, PN DS159-2 AND RIGGED. I certify all maintenance performed on this aircraft was performed in accordance with current regulations of the
- 197. Federal Aviation Administrationand is approved for return to service with respect to the work performed. For details see work order 252528 and 253517 on file with this agency. StandardAero CRS UO2R221L Springfield, IL. _____________________________ I certify this aircraft has been inspected in accordance with “E” E1-12 (TASK 050520), “F” F1-12(TASK 050650) and “G” (TASK 050780)” inspections under FAR. 91.409(f)(3)and is approved for return to service. For details see work order 252528 on file with this agency, StandardAero CRS UO2R221L Springfield, IL. _____________________________ …..End….. Standard Aero Maintenance Log Entry Dated 1/29/2009 NXXGS 6390.6 4278 1/31/2009 ATA 32 -Removed and replaced #4 maxaret p/n AC65216 s/n 30DM with s/n JY230 after overhaul by Aero Trades Inc. -Removed and replaced R/H modulator p/n ACM22742 s/n KW580 with s/n 129AT after overhaul by Aero Trades Inc. -Removed and replaced #4 brake assembly p/n AHA1897 RFS s/n ZX182 with s/n PA031 after overhaul by Aircraft Specialties Inc. I certify all maintenance performed on this aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. For details see work order 253783 on file with this agency. StandardAero CRS UO2R221L Springfield, IL. _____________________________ …..End….. 1/29/2009
- 198. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" LDGS APU HRS CYCLES EVENT DATE 02/02/2009 AC 810 9.5 810 9.5 6393.0 1 4410 Total 2569.6 6861 INDEX NUMBER 70 EN1 798 8.2 798 8.2 N1 6155.5 4280 EN2 582 0 801 2.2 N2 6338.0 4383 APU SEMI ANNUAL/125 HR/250 CYCLE INSPECTION C/W AFMS TASK 492001. NEXT DUE AUGUST 2009. APU SEMI ANNUAL/250 HR/500 CYCLE INSPECTION C/W AFMS TASK 492001. NEXT DUE AUGUST 2009. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 02/02/2009 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 199. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 02/12/2009 AC 810 9.5 810 9.5 6399.7 1 4419 Total 2574.4 6877 INDEX NUMBER 71 EN1 798 8.2 798 8.2 N1 6162.2 4289 EN2 582 0 801 2.2 N2 6344.7 4392 #1 AND #2 MAIN WHEEL AND TIRE ASSYS REPLACED FOR WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA 1814 WWO32 AHA1814 SL105 #2 MAIN WHEEL ASSY AHA 1814 LC290 AHA1814 LR165 BOTH WHEELS SB 32-1374 & SB 32-3746 CW. REMOVED TIRES HAD 158 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3719, DATED 11//04/2008 COMPLETED AFMS TASK 050790, 400 HOUR LUBRICATION. NEXT DUE AT 6800 AFTT. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 02/12/2009 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 200. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 02/17/2009 AC 810 9.5 810 9.5 6406.0 4424 Total 2575.9 6880 INDEX NUMBER 72 EN1 798 8.2 798 8.2 N1 6168.5 4294 EN2 582 0 801 2.2 N2 6351 4397 COMPLETED AFMS TASK 320036.1, CK OF #1 BRAKE FOR WEAR, NEXT DUE AT 4499 LANDINGS. COMPLETED AFMS TASK 320036.2, CK OF #2 BRAKE FOR WEAR, NEXT DUE AT 4499 LANDINGS. REMOVED AND INSPECTED #1 ENGINE OIL FILTER AND CHIP DETECTOR BECAUSE FOUND OIL FILTER BYPASS PIN PROTRUDED ON POST FLIGHT WALK AROUND. NO CONTAMINATION OF ANY KIND IN FILTER OR CHIP DETECTOR. INSTALLED NEW OIL FILTER, PN 3070945-1, RAN #1 ENG TO CHECK FOR LEAKS, OK FOR SERVICE. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 02/17/2009 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 201. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 03/09/2009 AC 810 9.5 810 9.5 6419.7 4436 Total 2590.4 6895 INDEX NUMBER 73 EN1 798 8.2 798 8.2 N1 6183.9 4306 EN2 582 0 801 2.2 N2 6366.4 4409 CREW REPORTS INTERMITTENT #1 ENGINE FIRE BELL CANCEL LIGHT WILL NOT ILLUMINATE WHEN ACTIVATED, BELL CANCEL FUNCTION NORMAL. REPLACED #1 ENGINE FIRE BELL CANCEL LIGHT SWITCH ASSY, MFG PN 99-222, NSN. OP CKS NORMAL. CW AFMS TASK 237012, CHECK OF UNDERWATER LOCATOR BEACON WITH DUKANE TESTER, OP CKS OK. CW TASK 334001-API CK OF WINGLET NAV LIGHT LENSE CONDITION, CKS OK. CW TASK 334003-API CK OF WINGLET STROBE LENSE CONDITION, CKS OK. CW AFMS TASK 210001 DRAIN AND RE-SERVICE COOLING TURBINE LUBE OIL WITH EXXON 2380 TO FULL, LEAK CKS OK. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 03/09/2009 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 202. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 03/18/2009 AC 810 9.5 810 9.5 6419.7 4436 Total 2590.4 6895 INDEX NUMBER 74 EN1 798 8.2 798 8.2 N1 6183.9 4306 EN2 582 0 801 2.2 N2 6366.4 4409 CREW REPORTS INTERMITTENT STALL IDENT AND FLAP DISCREET FAULT LIGHT. TROUBLESHOOTING REVEALED RH FLAP 0 DEGREE POSITION SW OUT OF ADJUSTMENT, THE SW WAS STAYING ON TOO LONG. ADJUSTED SW PER AMM. REMOVED RELAYS HC AND KC DURING TS AND REPAIR, REINSTALLED SAME. REINSTALLED DA-B ACCESS PANEL THAT COVERS RELAYS. RAN FLAPS THROUGH FULL OPERATION AND OPS CKS GOOD. NOTED EVIDENCE OF PREVIOUS WEAR ON INBOARD FLAP DRIVE TORQUE TUBE IN LH GEAR WHEEL WELL AREA CHAFING INBD FLAP FORWARD FLAP LEADING EDGE. DETERMINED THAT THERE IS NO PRESENT INTERFERENCE BETWEEN FORWARD FLAP AND TORQUE TUBE. CHAFE DEPTH ON SURFACES INSIGNIFICANT, CLEANED, PRIMED AND PAINTED WORN TORQUE TUBE AND FORWARD FLAP AREAS. RE-INSPECTION BY CREW OR MAINTENANCE AFTER NEXT FLIGHT RECOMMENDED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 03/18/2009 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 203. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 1.003 TOTAL Selection.Ho meKey unit:=wdSto ry Selection.M oveDown unit:=wdLin e, Count:=4 Selection.Ho meKey unit:=wdLin e Selection.M oveDown unit:=wdLin e, Count:=2 Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell Selection = "" Selection.M oveRight unit:=wdCell , Count:=2 Selection = "" Selection.M oveDown unit:=wdLin e LDGS APU HRS CYCLES EVENT DATE 03/27/2009 AC 810 9.5 810 9.5 6433.3 4447 Total 2593.6 6912 INDEX NUMBER 75 EN1 798 8.2 798 8.2 N1 6195.8 4317 EN2 582 0 801 2.2 N2 6378.3 4420 RE-INSPECTION OR PREVIOUSLY PAINTED LEFT FLAP TORQUE TUBE WEAR RECOMMENDED IN ITEM 74 SHOWS NO NEW WEAR OR EVIDENCE OF INTERFERENCE. OK FOR SERVICE. REPLACED FAULTY COMPONENT GG-AS, TDA310, TWO SECOND TIME DELAY UNIT IN #1 LOW OIL PRESSURE MASTER WARNING AND DISCREET LIGHT INDICATION CIRCUIT FOR INTERMITTENT FAILURE TO INDICATE LOW OIL PRESSURE AFTER ENGINE SHUTDOWN. INSTALLED NEW PART PER HB SB 31-3756 OBTAINED THROUGH GLOBAL PARTS INC. PART NEW FROM HAWKER BEECHCRAFT (RAPID), DALLAS DISTRIBUTION CENTER, 801 INDUSTRIAL BLVD, SUITE 100, GRAPEVINE, TX 76051 UNDER WO# 0001547387-000010, DATED 3/26/2009. ACCOMPLISHED FUNCTIONAL TEST PER AMM 31-50-00-501, OPS CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF TIME DELAY UNIT 140-360044-0002 NSN TDA310 0234T UPDATED AVTRAK RECORDS TO REFLECT INCORPORATION OF SB31-3756, TASK CODE 98313756, AND REPLACEMENT OF TDA310 SN 0234T, TASK CODE 7710502. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. DATE 03/27/2009 SIGN CERT NO: A&P 3357851 GREGORY A. STULTZ
- 204. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.0 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/23/2009 A/C 6448.9 4460 Total 2606.6 6929 INDEX NUMBER 76 EN 1 6211.4 4330 APU tach 4495 6921 EN 2 6393.9 4433 RESEARCHED THE FOLLOWING AD’S AND FOUND TO BE NOT APPLICABLE: AD 2009-05-08 (EFFECTIVE DATE: APRIL 20, 2009) TRIMBLE OR FREEFLIGHT SYSTEMS 2101 I/O APPROACH PLUS GPS NAVIGATION SYSTEMS, NOT INSTALLED. AD 2009-05-05 (EFFECTIVE DATE: APRIL 3, 2009) AVIDYNE CORPORATION PRIMARY FLIGHT DISPLAYS (PFDS) (SUPERSEDES AD 2008-06-28 R1), NOT INSTALLED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 205. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.0 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/11/2009 A/C 6461 4469 Total 2615.1 6942 INDEX NUMBER 77 EN 1 6223.5 4339 APU tach 4503.5 6934 EN 2 6406 4442 #3 AND #4 MAIN WHEEL AND TIRE ASSYS REPLACED FOR WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 MAIN WHEEL ASSY AHA 1814 SL105 AHA1814 XB003 #4 MAIN WHEEL ASSY AHA 1814 LR165 AHA1814 XB007 BOTH WHEELS SB 32-1374 & SB 32-3746 CW. COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1& #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4544 LANDINGS. COMPLETED AFMS TASK 720005, 150 TO 250 HOUR ENGINE ROUTINE PERIODIC INSPECTION, LT AND RT ENGINES. NEXT DUE IN 250 HOURS AT 6711 AFTT . SOAP SAMPLES TAKEN FOR #1 AND #2 ENGINES, NEW OIL FILTERS, PN 3070945-1, O- RING PN S9413- 06 INSTALLED, RAN BOTH ENGINES TO LEAK CHECK NEW FILTERS, CKS OK. SERVICED OIL LEVEL TO FULL. NORMAL RESAMPLE NEXT DUE IN 150 HOURS AT 6611 AFTT. COMPLETED AFMS TASKS 783003 & 783004, 191 TO 240 HOUR THRUST REVERSER INSPECTION, LT AND RT ENGINES. NEXT DUE IN 240 HOURS AT 6701 AFTT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 206. Engine Log Entry Reg.# NXXGS Date: June 4, 2009 Work Order: FZN9A Make: Hawker Model: 800A S/N: 2581XX A/C TT: 6479.8 Landings: 4477 Engine Position: #2 Engine s/n: P-91371 TSN: 6424.8 CSN: 4450 1) Removed Fuel Control Assembly (FCU) p/n 3070800-15, s/n A9475. 2) Installed an Overhauled FCU p/n 3070800-24, s/n 12547. 3) Accomplished Manual Mode Transfer and Over Speed shutdown checks. 4) Leak and ops check okay on ground run. 5) Done I/A/W Honeywell TFE731-5 LMM 73-20-01. The above described repair or maintenance is certified airworthy and approved for return to service. A detailed record is on file under Work Order # FZN9A. Signed:_Lloyd Kasten____________________________________________________ For Duncan Aviation CRS# JGVR194F Phone: 800-228-4277
- 207. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.1 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/13/2009 A/C 6481.1 4479 Total 2625.6 6965 INDEX NUMBER 78 EN 1 6243.6 4349 APU tach 4514 6957 1888.4 APU tach adj (-) EN 2 6426.1 4452 8 APU Cyc adj (+) REPLACED #1 HYDRAULIC PUMP FOR HYDRAULIC OVERHEAT INDICATION PROBLEM. VERIFIED SYS OVERHEAT FAULT WITH OMEGA ENGINEERING OMEGALABEL TEMP MONITOR PLACARDS, PN TL-10-105-10 AND TL-10-190-10. PERFORMED PRESSURE DISSIPATION TEST PER AMM TO RULE OUT OVERHEATING DOWNSTREAM SYSTEM COMPONENTS. NOTED LH AND RH FULL FLOW RELIEF VALVES REMAIN COOL TO TOUCH DURING INDIVIDUAL ENG RUNS, NO OVERHEAT DEVELOPED DURING ENG RUNS BUT #1 PUMP WAS 10-12 CENTIGRADE WARMER THAN #2 (69C TO 47C) EVEN WITH #1 TESTED FIRST. INSTALLED AND TESTED PUMP PER AMM 29-10-54-401, RAN ENG #1, AFTER 10 MIN PUMP TEMP 46C, NO LEAKS NOTED. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 ABEX HYDRAULIC PUMP APO5V-086-03 4202203 42022-03 AH-17680 4202202 42022-02 AH-18090 REMOVED PUMP HAD 7002 HOURS AND 4699 CYC AT REPLACEMENT. INSTALLED PUMP OVERHAULED BY PARKER HANNIFIN CORP, 2220 PALMER AVE, KALAMAZOO MI, 49001-4165, CRS# UCER345K UNDER WO#737085 DATED 10/22/2007. PART INCORPORATES HB MOD 253226, PUMP WITH A BLEED VALVE LOCATED IN THE SUCTION LINE ON THE PUMP PORT CAP. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 208. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.1 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/30/2009 A/C 6490.1 4487 Total 2634.3 6973 INDEX NUMBER 79 EN 1 6252.6 4357 APU tach 4522.7 6965 1888.4 APU tach adj (-) EN 2 6435.1 4460 8 APU Cyc adj (+) LT AND RT NLG TIRES WORN. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LT NLG WHEEL AND TIRE ASSY AH52339 DW061 AH52339 LS064 RT NLG WHEEL AND TIRE ASSY AH52339 149,1045 AH52339 LS069 TIRES HAD 169 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3720, DATED 11/03/2008 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 209. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.1 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/24/2009 A/C 6506 4496 Total 2642.7 6984 INDEX NUMBER 80 EN 1 6268.5 4366 APU tach 4531.1 6976 1888.4 APU tach adj (-) EN 2 6451 4469 8 APU Cyc adj (+) CW BATTERY CHECK-EMERGENCY EXIT LIGHT UNITS, AVTRAK TASK 335010 BY REPLACEMENT OF ALL FOUR BATTERIES IN POWER PACK, OP CKS OK. INSTALLED PMA PARTS OBTAINED FROM EAGLE INDUSTRIES MFG BY AERO DESIGN, INC., 385 INDUSTRIAL DRIVE, MT. JULIET, TN, 37122, (PH 800-551-1158) PAH # PQ1465CE UNDER WO SO-16241 DATED 06/30/2009. CREW OBSERVES INTERMITTENT PROBLEM WITH LH REFUEL VALVE CLOSING DURING FUELING WITH VALVE RE-OPENING IF LH PUSH TO TEST SW MANIPULATED. CHECKED RESISTANCE AT LH TANK FLOAT SW, CIRCUIT VOLTAGE AT TERMINAL JU, ALL OK. COULD NOT DUPLICATE PROBLEM. REPLACED LH REFUEL VALVE ON/OFF SWITCH (DB-DG) AND LH REFUEL VALVE PUSH TO TEST SWITCH (DB-CG) AS PRECAUTIONARY ACTION. OP CKS OK. CREW REPORTS INTERMITTENT PROBLEM WITH CABIN TEMPERATURE CONTROL FUNCTION INOP AT VIP SEAT WITH TEMP SELECT SWITCH AT VIP SEAT SHOWING “NO TEMP”. COCKPIT PEDESTAL CONTROL POSITION SW “CABIN” ANNUNCIATION ILLUMINATES NORMALLY. TEMP CONTROL IN “COCKPIT” POSITION OPS NORMALLY. REPLACED RELAY K18 IN LAVATORY COMPONENT PANEL. OP CKS OK FROM CABIN AND COCKPIT. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LH REFUEL SW 2TP1-3 NSN 2TP1-3 NSN LH REFUEL VALVE PUSH TO TEST SW/INDICATOR 99-212 NSN 99-212 NSN RELAY K18 MHLO-12D- 26.5VDC NSN MHLO-12D- 26.5VDC NSN (4EA )EMERGENCY LIGHTING POWER SUPPLY BATTERIES AD4002P NSN A25503-025 (MARTHON PN) NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 210. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.1 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/24/2009 A/C 6506 4496 Total 2642.7 6984 INDEX NUMBER 81 EN 1 6268.5 4366 APU tach 4531.1 6976 1888.4 APU tach adj (-) EN 2 6451 4469 8 APU Cyc adj (+) CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 4920004. UPDATED AVTRAK RECORDS TO REFLECT ACCOMPLISHMENT OF TASKS ABOVE. SWAPPED MAIN BATTERY POSITIONS LT TO RT TO PROLONG BATTERY LIFE. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 211. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.1 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/24/2009 A/C 6519.2 4507 Total 2652.5 7003 INDEX NUMBER 82 EN 1 6281.7 4377 APU tach 4540.9 6995 1888.4 APU tach adj (-) EN 2 6464.2 4480 8 APU Cyc adj (+) CREW REPORTS PITOT AMP INDICATION INOP FOR LT SIDE PROBES, RT SIDE OPS NORMAL. CREW PLACED ITEM ON MMEL, INSTALLED PLACARD AND CW OPS PROCEDURE. CLEARED MMEL 30-3 BY REPAIRING COLD SOLDERED, BROKEN WIRES ON PITOT AMP INDICATION SELECT SWITCH, TERMINALS 1,2,5 AND 7. OPS CK OK BOTH SIDES, REMOVED PLACARD AND SIGNED AIRCRAFT MMEL/SQUAWK BOOK NOTING MX ACTION PERFORMED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 212. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 ADDED TABLE BOX FOR TITLE WITH TRANSPARENT TOP AND SIDE BORDERS. TOTAL LDGS APU HRS CYCLES EVENT DATE 9/22/2009 A/C 6559 4527 Total 2664.2 7028 INDEX NUMBER 83 EN 1 6321.5 4397 APU tach 4552.6 7020 1888.4 APU tach adj (-) EN 2 6504 4500 8 APU Cyc adj (+) REMOVED AND REPLACED #1 & #2 ENGINE FUEL FILTERS, (AVTRAK TASK 730005) PN 897830-1, NSN, IAW AMM 73-21-02. PARTS PURCHASED NEW FROM GENERAL DYNAMICS AVIATION SERVICES, MFG’D BY HONEYWELL 700 HENRIETTA CREEK RD, ROANOKE, TX 76262 UNDER WO# 5923244 004 DATED 9/4/2007. CW 150-200 HOUR (AVTRAK TASK 720005) AND 300-400 HOUR INSPECTION (AVTRAK TASK 720011) ON #1 & #2 ENGINES IAW HONEYWELL MM 72-00-00 SEC 601. REPLACED BOTH OIL FILTERS WITH NEW PN 3070945-2, FROM JET CARE MFG’D BY HONEYWELL 700 HENRIETTA CREEK RD, ROANOKE, TX 76262 UNDER WO# 6449694 007 DATED 9/23/2008. NO SERIAL NUMBERS. FILTERS SENT AS SOAP SAMPLES TO JETCARE. NO FAULTS NOTED ON ENGINE INSPECTIONS, RAN ENGINES, OPS AND LEAK CKS GOOD, SERVICED OIL TO FULL. CW BRAKE WEAR INSPECTION ON #1 AND #2 BRAKES ASSY’S, OK FOR SERVICE (AVTRAK TASK 320032.1 & 320036.2). ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 213. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/5/2009 A/C 6572.2 4537 Total 2671.6 7043 INDEX NUMBER 84 EN 1 6334.7 4407 APU tach 4560 7035 1888.4 APU tach adj (-) EN 2 6517.2 4510 8 APU Cyc adj (+) CW MANDATORY SB 32-3962. LOGBOOK RESEARCH PER SB INSTRUCTIONS RQD REPLACEMENT OF NLG STEERING SLEEVE PIN, PN 25UN605 AND LH AND RH MLG UPPER TORQUE LINK PIVOT PINS PN 25-8UM131-11A. WORK ACCOMPLISHED IAW SB 32-3962, CMM 32-20-30 AND 32-10-01. CREW REPORTS INSTANCE OF TOTAL FAILURE OF #1 AHARS SYSTEM, REVERSION MODE OPS NORMAL. TROUBLESHOOTING INDICATES FAILURE OF AHARS UNIT AH-600. REMOVED AND REPLACED #1 ATTITUDE HEADING AND REFERENCE UNIT PER HONEYWELL SYSTEM MAINT MANUAL 22-16-00 PG 702, OP CKS OK. UNIT OBTAINED THROUGH DUNCAN AVIATION (AS A WARRANTY EXCHANGE), LINCOLN NE. UNIT PREVIOUSLY REPAIRED BY HONEYWELL, 7227 W. HARRY, WICHITA, KS 67209, CRS LV2R992K UNDER WO# 5002836784 DATED 9/23/2009. NEW UNIT MOD STATUS: C, D, F - M, P – AA. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF AH-600 AHARS #1 7003360-943 97083876 7003360-943 86090540 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 214. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/7/2009 A/C 6572.2 4537 Total 2671.6 7043 INDEX NUMBER 85 EN 1 6334.7 4407 APU tach 4560 7035 1888.4 APU tach adj (-) EN 2 6517.2 4510 8 APU Cyc adj (+) COMPLETED 200 HR LUBE AFMS/AVTRAK TASK 050050. NEXT DUE AT 6772 AFTT. COMPLETED 12 MONTH INSPECTION AND CAPACITY TEST / RECHARGE ON MAIN BATTERY SN 40251482, REINSTALLED IN #1 POSITION, AVTRAK TASK 241015, IAW CONCORDE RG390E ICA DWG NO. 5-0142 REV J ISSUED 2/20/2007. CKS OK, NEXT DUE CAP CHECK 1/07/2010. COMPLETED 12 MONTH INSPECTION AND CAPACITY TEST / RECHARGE ON MAIN BATTERY SN 40251513, REINSTALLED IN #2 POSITION, AVTRAK TASK 241016, IAW CONCORDE RG390E ICA DWG NO. 5-0142 REV J ISSUED 2/20/2007. CKS OK, NEXT DUE CAP CHECK 1/07/2010. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 215. Jet East CorporateAviation, LLC Airframe Log Book Entry 8375 enterprise Ave Philadelphia PA 19153 Aircraft Reg.: NXXGS Airframe Time: 6577 W.O. # 910522 Aircraft S/N: 2581XX Airframe Cycles: 4541 1. Removed and replaced left mixing valve with an overhauled valve. The unit was overhauled by Duncan Aviation CRS# JGVR194F all work done IAW Hawker 800 MM CH. 21-10-35. Operational checks are good. P/N ON: 3213788-1-1 S/N ON: 1195 P/N OFF: 3213788-1-1 S/N OFF: P-116 2. Removed and replaced right mixing valve with an overhauled valve. The unit was overhauled by Duncan Aviation CRS# JGVR194F all work done IAW Hawker 800 MM CH. 21-10-35. Operational checks are good. P/N ON: 3213788-1-1 S/N ON: 1196 P/N OFF: 3213788-1-1 S/N OFF: 1058 3. Replaced cooling turbine to heat exchanger disc seal P/N 2872-32A and spring P/N 172328 with new. Operational and leaks checks satisfactory. All work in accordance Hawker 800 MM CH 21-10-85 and 21-10-15. 4. Performed operational checks of L/H and R/H mixing valves(L/P H/P) IAW Hawker 800 MM CH 21-10-35. 5. Performed operational check of pressurization control system IAW Hawker 800MM CH 21-30-00. The aircraft and/or components identified above were repaired and inspected IAW FAA regulations and were found airworthy to return to service. Pertinent details of this repair are on file at this agency. Signature : _______________________ Certification: ___AP 3380865_________ Date: 10/15/09 Print Name: _Dennis R Ross______________________
- 216. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/15/2009 A/C 6577.4 4541 Total 2677.3 7051 INDEX NUMBER 86 EN 1 6339.9 4411 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6522.4 4514 8 APU Cyc adj (+) COMPLETED AFMS TASK 210001, DRAINED AND REPLENISHED COOLING TURBINE (PN 203880-2-2, SN 38-868) WITH EXXON 2380 OIL. COMPLETED AFMS TASK 210003, HP/LP BLEED AIR FUNCTION TEST PER AMM 21-10-35, CKS OK. COMPLETED AFMS TASK 210004 CK OF MANUAL CABIN ALTITUDE CONTROL VALVE. COMPLETED AFMS TASK 210005 CK OF COOLING TURBINE EXHAUST DRAIN. REPLACED DRAIN LINE, OP CKS OK. COMPLETED AFMS TASK 210006 INSPECTION/CLEAN OF WATER SEPARATOR AND DRAIN OUTLET. INSPECTED AND CLEANED ARKANSAS AEROSPACE, AAI ADDITIONAL WATER SEPARATOR IN COCKPIT AIR CONDITIONING LINE PER AAI BAe 128-800 MAINTENANCE MANUAL ADDENDUM 21-20 PAGE 3, CLEANED SOCK, PN 800-8234-64. COMPLETED AFMS TASK 210011 INSPECTION OF AIR CONDITIONING DUCTS. SCHEDULED AFMS TASK 210021, RE-INSPECTION OF DISTURBED AIR CONDITIONING DUCTS IN 300 FLYING HOURS AT 6877 AFTT. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 217. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/2/2009 A/C 6563.9 4548 Total 2687.8 7069 INDEX NUMBER 87 EN 1 6326.4 4418 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6508.9 4521 8 APU Cyc adj (+) #1 AND #2 MAIN WHEEL AND TIRE ASSYS REPLACED FOR WEAR PER AMM 32-40-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA 1814 XB003 AHA1814 WWO32 #1 TIRE GOODYEAR FLT EAGLE 237K23-2 70710842 NA NA #2 MAIN WHEEL ASSY AHA 1814 XB007 AHA1814 LC290 #2 TIRE GOODYEAR FLT EAGLE 237K23-2 70690853 NA NA BOTH WHEELS SB 32-1374 & SB 32-3746 CW. REMOVED TIRES HAD 129 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 3842, DATED 07/20/2009 COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1& #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4623 LANDINGS. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ XX XXX LLC MAINTENANCE LOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2
- 218. TOTAL LDGS APUHRS CYCLES EVENT DATE 11/4/2009 A/C 6563.9 4548 Total 2687.8 7069 INDEX NUMBER 88 EN 1 6326.4 4418 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6508.9 4521 8 APU Cyc adj (+) CREW REPORTS INTERMITTENT FAILURE OF IRS TO ALIGN. CONFIRMED FAULT IN IRU BY FAULT BALL INDICATION ON UNIT. REPLACED IRU WITH REPAIRED UNIT OBTAINED THROUGH STANDARD AERO. BITE TEST AND GROUND INDICATIONS NORMAL, OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF HONEYWELL LASERREF III IRU HG1075AE03 720 HG1075AE03 737 MODS INCORPORATED PER DATA PLATE: SER 2, 1,2,3,5,6,8,9,10,12,13 INSTALLED IRU REPAIRED BY HONEYWELL, 8840 EVERGREEN BLVD, MINNEAPOLIS, MN 55433-6040 CRS KE2R949K UNDER WO 356682, DATED 09/24/2009 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 219. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/5/2009 A/C 6563.9 4548 Total 2687.8 7069 INDEX NUMBER 89 EN 1 6326.4 4418 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6508.9 4521 8 APU Cyc adj (+) RESEARCHED AD 2009-21-03, EFFECTIVE 11/20/2009 FOUND NA BY MFG PART NUMBER. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 220. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.2 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/19/2009 A/C 6573.4 4558 Total 2692.6 7079 INDEX NUMBER 90 EN 1 6335.9 4426 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6518.4 4529 8 APU Cyc adj (+) FLIGHT CREW REPORTS THAT THE LEFT AUTOPILOT DISENGAGES AND THE FLIGHT DIRECTOR FLAGS FAIL INTERMITTENTLY. OPS OK ON LAST 2 LEGS. SWAPPED #1 AND #2 FGCs FZ-800 P/N 7003974-732, S/N 87080925 NOW #1, S/N 89041674 NOW #2. OP CK ON GND OK FOR SERVICE. SERVICED AUX HYDRAULIC TANK TO FULL. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 221. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.3 Wider parts table. TOTAL LDGS APU HRS CYCLES EVENT DATE 11/29/2009 A/C 6579.4 4563 Total 2698.8 7089 INDEX NUMBER 91 EN 1 6341.9 4431 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6524.4 4534 8 APU Cyc adj (+) CREW REPORTS UNUSUAL VIBRATION FROM NLG AFTER RETRACTION, NO NLG SHIMMY ASSOCIATED WITH THIS SQUAWK. NO FAULTS FOUND IN WHEEL WELL AREA. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LT NLG WHEEL AND TIRE ASSY AH52339 QA033 AH52339 DW061 RT NLG WHEEL AND TIRE ASSY AH52339 QG038 AH52339 149,1045 TIRES HAD 94 LANDINGS AT REPLACEMENT. INSTALLED WHEELS PURCHASED FROM PROSERVE AVIATION WITH FRESH OVERHAUL BY PRECISION AIRCRAFT SUPPORT, INC, 8700 AKINS RD, STE#5, NORTH ROYALTON, OH 44133, CRS QQ7R193Y, UNDER WO 2929, DATED 7/30/2009. SERVICED NORMAL HYDRAULIC TANK TO FULL. DETERMINED HAWKER BEECHCRAFT MANDATORY SB 32-3962, REV. 2 (LANDING GEAR COMPONENT REPLACEMENT FOR HYDROGEN EMBRITTLEMENT) NO FURTHER ACTION RQD PREVIOUSLY CW. DETERMINED HAWKER BEECHCRAFT SB 35-3989 (INSPECTION FOR CLEARANCE BETWEEN UPPER RT OXYGEN CYLINDER AND PRIMARY RUDDER CABLE) NO FURTHER ACTION RQD BECAUSE AUX OXY CYLINDER NOT INSTALLED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 222. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.4 CLOSE UP GAP BELOW TIMES TABLE AND MX DESCRIPTION BLOCK TOTAL LDGS APU HRS CYCLES EVENT DATE 11/29/2009 A/C 6579.4 4563 Total 2698.8 7089 INDEX NUMBER 92 EN 1 6341.9 4431 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6524.4 4534 8 APU Cyc adj (+) DETERMINED AD 2009-21-10, EFFECTIVE 12/17/2009 IS NA TO THIS AIRCRAFT. AVOX SYSTEMS AND B/E AEROSPACE OXYGEN CYLINDER ASSY’S NOT INSTALLED ON THIS AIRCRAFT AT THIS TIME. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 223. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.4 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/7/2009 A/C 6588.7 4572 Total 2701 7093 INDEX NUMBER 93 EN 1 6351.2 4440 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6533.7 4543 8 APU Cyc adj (+) CREW REPORTS INTERMITTENT FAILURE OF #2 STALL IDENT SYSTEM TEST. FOUND RH AIRFLOW ANGLE SENSOR LOW OHM READING AT #2 SSU TERMINAL PINS 6 AND 7 (2 OHMS). REPLACED RH AIRFLOW ANGLE SENSOR UNIT (CU) PER AMM 27-33-17-401, OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RH AIRFLOW ANGLE SENSOR VANE 1703-12 1419 1703-12 731 STALL VANE PURCHASED FROM DUNCAN AVIATION, UNIT OVERHAULED BY SAFE FLIGHT INSTRUMENT CORPORATION 20 NEW KING ST., WHITE PLAINS, NY 10604, TEL 914-946-9500, CRS# QA1R419K UNDER WO# 760978 DATED 10/16/2009. MODS A AND B INCORPORATED AT OVERHAUL. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 224. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.4 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/8/2009 A/C 6588.7 4572 Total 2701 7093 INDEX NUMBER 94 EN 1 6351.2 4440 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6533.7 4543 8 APU Cyc adj (+) CREW REPORTS INTERMITTENT INFLT CABIN PRESSURE LOSS RATE OF UP TO 2000 FPM (INITIAL) WHEN BOTH THROTTLES RETARDED TO IDLE AT ALTITUDES ABOVE 10,000 FEET. PROBLEM CAN BE MASKED IF #1 THROTTLE KEPT ABOVE FLIGHT IDLE. PERFORMED HP/LP VALVE TEST PER AMM AND FOUND #2 MIX VALVE WEAK. REPLACED RH MIX VALVE PER AMM 21-10-35-401. SWAPPED HP AIR VALVES, PN B01A2-14128A, SN 986 NOW ON LH SIDE, SN 1007 NOW ON RH SIDE. RAN ENGINES, PRESSURIZED DISTURBED DUCTING, LEAK AND OP CKS OK PER AMM ADJUSTMENT/TEST 21-10-35-501. NOTED THAT RH SIDE HAS LESS PRESSURE OUTPUT MEASURED AT TEST PORT DURING TEST STEP 14 (ENG 50% N1) 20 PSI ON LH SIDE, 17 PSI ON RH SIDE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RH MIXING VALVE 3213788-1-1 1058 3213788-1-1 1196 MIX VALVE PURCHASED FROM DUNCAN AVIATION, UNIT OVERHAULED BY DUNCAN AVIATION LINCOLN AIRPORT/LINCOLN, NE, 68524, CRS# JGVR194F UNDER WO# UG5FA DATED 11/09/2009. UPDATED AVTRAK RECORDS TO REFLECT PART CHANGES. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 225. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.4 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/10/2009 A/C 6588.7 4572 Total 2701 7093 INDEX NUMBER 95 EN 1 6351.2 4440 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6533.7 4543 8 APU Cyc adj (+) #1 COM INOP. SWAPPED COM UNITS FOR TROUBLESHOOTING, PROBLEM FOLLOWS SWAP. REMOVED FAULTY RCZ-851 COMMUNICATION UNIT AND INSTALLED REPAIRED UNIT IN #2 POSITION, RCZ-851 SN 95061573 IN #1 POSITION. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 RCZ-851 COMM UNIT 7510700-802 88100192 7510700-802 88070149 INSTALLED UNIT MOD STATUS A, B, E, G, K, L, N, R, S, U, Y – AB, AE, AG, AK, AN, AU. UNIT PURCHASED FROM STANDARD AERO, REPAIRED BY HONEYWELL, 8370 DOW CIRCLE, STRONGSVILLE, OH 44136, CRS# FGNR677K, UNDER WO# 5003063260 DATED 12/09/2009. UPDATED AVTRAK RECORDS TO REFLECT PART CHANGES. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 226. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.4 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/18/2009 A/C 6590.3 4575 Total 2701 7093 INDEX NUMBER 96 EN 1 6352.8 4443 APU tach 4565.7 7043 1888.4 APU tach adj (-) EN 2 6535.3 4546 8 APU Cyc adj (+) CREW REPORTS THAT CABIN ALTITUDE CLIMBS 1,500 FPM WHEN PRESSURIZED ABOVE 15,000 FEET AND THROTTLES BROUGHT TO IDLE POWER SETTING, TAKES ABOUT 15 SECONDS TO RECOVER. AIRPLANE FAILED CABIN LEAK RATE TEST PER AMM 21-30-00-501(33 SECONDS, MIN STANDARD IS 45 SECONDS). FOUND ELEVATOR AND RUDDER FLIGHT CONTROL CABLE SEALS AT LOWER AFT PRESSURE VESSEL AND FLOOR LEVEL MAIN ENTRY DOOR DRAIN FIXTURE LEAKING AIR. REPLACED FLIGHT CONTROL CABLE SEALS, PN 25CF2479 (2 EACH) AND PN 25CF2487 (2 EACH) AND MANIPULATED, CLEANED AND LUBRICATED DOOR MOUNTED DRAINAGE FIXTURE FLOOR LEVEL OF MAIN ENTRY DOOR THAT WAS FOUND STUCK IN OPEN POSITION, NOW SEALS OK. AIRPLANE NOW PASSES CABIN LEAK DOWN RATE TEST, TAKES 53 SECONDS TO LEAK DOWN FROM 4 TO 3 PSI DIFFERENTIAL PRESSURE. FLIGHT TEST VERIFIED CABIN PRESSURIZATION OPS OK. REMOVED, CAP CHECKED AND RECHARGED #1 AND #2 MAIN AND #3, #4, #5 AUX AND IRS BATTERIES, BATTERIES CK OK FOR CONTINUED SERVICE AND WERE RE-INSTALLED IN ORIGINAL POSITIONS. #1 AND #2 MAIN BATTS DUE RECHECK 3/18/2010. RECHECK DUE ON #3, #4 AND #5 AUX AND IRS BATTERIES 12/18/2010. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 227. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 Fix drift of times table to right TOTAL LDGS APU HRS CYCLES EVENT DATE 1/8/2010 A/C 6598 4582 Total 2719.7 7130 INDEX NUMBER 97 EN 1 6360.5 4450 APU hrs/cyc 4608.1 7122 1888.4 APU tach adj (-) EN 2 6543 4553 8 APU Cyc adj (+) ACCOMPLISHED AFMS TASK 050520, “INSPECTION E” IAW AMM. ACCOMPLISHED AFMS TASK 240001, LH STARTER GENERATOR 200-400 HOUR INSPECTION IAW AMM. ACCOMPLISHED AVTRAK TASKS 262135 & 262136, COCKPIT AND CABIN FIRE EXTINGUISHER INSPECTION IAW AMM AS PART OF E INSPECTION. ACCOMPLISHED AFMS TASK 320036, LH INBD AND LH OUTBD BRAKE PAD WEAR CK IAW AMM. NEXT DUE AT 4657 CYCLES. ACCOMPLISHED ANNUAL TEST OF CDS-R SYSTEM PER ICA DOCUMENT #050908018, SYSTEM OK. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 228. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/11/2010 A/C 6598 4582 Total 2719.7 7130 INDEX NUMBER 98 EN 1 6360.5 4450 APU hrs/cyc 4608.1 7122 1888.4 APU tach adj (-) EN 2 6543 4553 8 APU Cyc adj (+) ACCOMPLISHED AFMS TASK 050040, APU INSPECTION, SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AND APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE. REPLACED INOP APU FUEL PUMP, OP CKS OK. PUMP PURCHASED FROM ALL WEST AVIATION SERVICES, PART OH’D BY FLEET SUPPORT SERVICES(RAPCO), MONROE AIRPORT, W4711 HWY 59, MONROE, WI 53566, CRS# NE5D064N UNDER WO# 52998 DATED 02/13/2009. FAILED PUMP HAD 423 HOURS AND 896 CYCLES SINCE OH AT REPLACEMENT. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF APU FUEL PUMP 1500-00-65 150 1500-00-65 222 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 229. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/12/2010 A/C 6598 4582 Total 2719.7 7130 INDEX NUMBER 99 EN 1 6360.5 4450 APU hrs/cyc 4608.1 7122 1888.4 APU tach adj (-) EN 2 6543 4553 8 APU Cyc adj (+) INSTALLED NEW APU OIL DRAIN/MAGNETIC CHIP DETECTOR PLUG ASSY. PN 4950875. INSTALLED NEW CHIP DETECTOR O RING PN M83248-1-008 AND NEW PLUG O RING PN M82348-1-906, LEAK CKS OK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 230. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/13/2010 A/C 6602.6 4584 Total 2721 7133 INDEX NUMBER 100 EN 1 6365.1 4452 APU hrs/cyc 4609.4 7125 1888.4 APU tach adj (-) EN 2 6547.6 4555 8 APU Cyc adj (+) INSTALLED FWD AND AFT FIRE BOTTLE GONE INDICATION FUSE CARTRIDGES. PN A1003(1), NSN. PART OBTAINED FROM DUNCAN AVIATION. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 231. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/16/2010 A/C 6602.6 4584 Total 2721 7133 INDEX NUMBER 101 EN 1 6365.1 4452 APU hrs/cyc 4609.4 7125 1888.4 APU tach adj (-) EN 2 6547.6 4555 8 APU Cyc adj (+) CW ANNUAL ELT INSPECTION, AVTRAK TASK 256000, PER CFR 91.202 AND 43 APPENDIX D USING ARTEX INSTALLATION AND OP MANUAL PAGE 4-3 PERIODIC MAINTENANCE CHECKLIST STEPS 1- 4 AND 6-9. CKS OK. UPDATED AVTRAK RECORDS. ELT BATTERY DUE FOR REPLACEMENT AUGUST 2010. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 232. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/19/2010 A/C 6603.9 4586 Total 2723 7137 INDEX NUMBER 102 EN 1 6366.4 4454 APU hrs/cyc 4611.4 7129 1888.4 APU tach adj (-) EN 2 6548.9 4557 8 APU Cyc adj (+) CREW REPORTS INTERMITTENT PROBLEM WITH CABIN TEMPERATURE CONTROL FUNCTION, TEMP CONTROL INDICATES NORMALLY AT VIP SEAT BUT AIR CONDITIONING GOES TO FULL HOT POSITION. TEMP CONTROL IN “COCKPIT” POSITION OPS NORMALLY. BENCH CK OF K18 RELAY SHOWS INTERMITTENT FAULT IN ONE OF THE CONTACTS. REPLACED RELAY K18 IN LAVATORY COMPONENT PANEL. PART OBTAINED FROM ELECTRO ENTERPRISES INC, 3601 N I-35, PO BOX 11456, OKLAHOMA CITY, OK, 73136, PHONE 405- 427-6591 OP CKS OK FROM CABIN AND COCKPIT. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RELAY K18 MHLO-12D- 26.5VDC NSN TRACE #204404 MHLO-12D- 26.5VDC NSN UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 233. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/1/2010 A/C 6613.9 4591 Total 2723 7137 INDEX NUMBER 103 EN 1 6376.4 4459 APU hrs/cyc 4611.4 7129 1888.4 APU tach adj (-) EN 2 6558.9 4562 8 APU Cyc adj (+) CW RVSM STATIC PLATE AND CRITICAL AREA INSP IAW AMM 34-11-29. PERFORMED AIRFRAME PORTION OF RVSM COMPLIANCE CK ACCOMPLISHED BY RED EAGLE AVIONICS. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 234. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/25/2010 A/C 6626.4 4598 Total 2736.3 7160 INDEX NUMBER 104 EN 1 6388.9 4466 APU hrs/cyc 4624.7 7152 1888.4 APU tach adj (-) EN 2 6571.4 4569 8 APU Cyc adj (+) STANDBY COMPASS LEAKING OIL. REPLACED MAGNETIC (STANDBY) COMPASS. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF STBY COMPASS S.I.R.S. NAVIGATION, LTD NV2C-28V 709634-10 KCA0104W SAV21621 ACCOMPLISHED AFMS TASK 340013 COMPASS SWING AND COMPENSATION PER AMM 34-09-111- 501. INSTALLED NEW DEVIATION CARD AND INSTALLED IN POCKET AFT OF CAPTS “C” WINDOW. OK FOR SERVICE. NEXT SWING DUE BY 2/25/2013. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 235. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/26/2010 A/C 6626.4 4598 Total 2736.3 7160 INDEX NUMBER 105 EN 1 6388.9 4466 APU hrs/cyc 4624.7 7152 1888.4 APU tach adj (-) EN 2 6571.4 4569 8 APU Cyc adj (+) ACCOMPLISHED MANDATORY HAWKER BEECHCRAFT SB 32-3979, FOUND NA BY SERIAL NUMBER. MAIN LANDING GEAR SERIAL NUMBER LH MLG SN: DHL/DH/1503 SIDE STAY SERIAL NUMBER LH MLG SIDE STAY SN:DHL/DH/1481 RH MLG SN: DHL/DH/1490 RH MLG SN: DHL/DH/1488 NOSE LANDING GEAR SERIAL NUMBER NLG SN: DHL/DH/742 DRAG STAY SERIAL NUMBER NLG DRAG STAY SN: DHL/DH/732 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 236. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/9/2010 A/C 6633.3 4603 Total 2739.4 7168 INDEX NUMBER 106 EN 1 6395.8 4471 APU hrs/cyc 4627.8 7160 1888.4 APU tach adj (-) EN 2 6578.3 4574 8 APU Cyc adj (+) ACCOMPLISHED CAPACITY CK OF BOTH MAIN RG-390E BATTERIES, RECHARGED AND REINSTALLED, SN 40251513 IN #1 POSITION, SN 40251482 IN #2 POSITION. OK FOR SERVICE. ACCOMPLISHED 400 HOUR DETAILED WALK AROUND INSPECTION PER AMM. OK FOR SERVICE. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 237. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/10/2010 A/C 6637.9 4606 Total 2741.4 7174 INDEX NUMBER 107 EN 1 6400.4 4474 APU hrs/cyc 4629.8 7166 1888.4 APU tach adj (-) EN 2 6582.9 4577 8 APU Cyc adj (+) CREW REPORTS INTERMITTENT #2 FLIGHT DIRECTOR FAIL FLAG, IDENTICAL TO REPORTS ON #1 SIDE (SEE INDEX NUMBER 90, 11/19/2009) PRIOR TO SWAP OF #1 AND #2 FLIGHT GUIDANCE COMPUTERS. REPLACED #2 FLIGHT GUIDANCE COMPUTER, OP CKS OK. PART PURCHASED FROM STANDARD AERO. INSTALLED PART OVERHAULED BY HONEYWELL, 7825 RIDGEPOINT DR, IRVING, TX 75063, CRS# TT1R518K, UNDER WO#5002133170, DATED 11/14/2008. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF FZ-800 FLIGHT GUIDANCE COMPUTER 7003974-732 00105672 7003974-732 89041674 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 238. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/29/2010 A/C 6642.8 4609 Total 2743 7177 INDEX NUMBER 108 EN 1 6405.3 4477 APU hrs/cyc 4631.4 7169 1888.4 APU tach adj (-) EN 2 6587.8 4580 8 APU Cyc adj (+) COMPLETED AFMS TASK 240001, RH STARTER GENERATOR INSPECTION, NO FAULTS NOTED, OK FOR SERVICE. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 239. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/16/2010 A/C 6649.4 4615 Total 2746.8 7186 INDEX NUMBER 109 EN 1 6411.9 4483 APU hrs/cyc 4635.2 7178 1888.4 APU tach adj (-) EN 2 6594.4 4586 8 APU Cyc adj (+) REMOVED BOTH IC-1080 AVIONICS COMPUTERS AND SENT TO HONEYWELL ICH FOR SOFTWARE UPGRADE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 IC-1080 IAC COMPUTER 7017000-20704 06097714 7017000-20704 06097714 #2 IC-1080 IAC COMPUTER 7017000-20704 06117846 7017000-20704 06117846 UNITS UPGRADED TO SOFTWARE MODIFICATION “ A “ STATUS. INSTALLED UNITS AND OPS CKS OK. ACCOMPLISHED CAPACITY CK OF BOTH MAIN RG-390E BATTERIES, RECHARGED AND REINSTALLED, SN 40251513 IN #1 POSITION, SN 40251482 IN #2 POSITION. OK FOR SERVICE. NEXT DUE CAP CK 8/16/2010. UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 240. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/16/2010 A/C 6649.4 4615 Total 2746.8 7186 INDEX NUMBER 110 EN 1 6411.9 4483 APU hrs/cyc 4635.2 7178 1888.4 APU tach adj (-) EN 2 6594.4 4586 8 APU Cyc adj (+) REMOVED BOTH FMS NZ-2000 NAVIGATION AVIONICS COMPUTERS AND SENT TO HONEYWELL ICH FOR SOFTWARE UPGRADE IN ORDER TO COMPLY WITH TERMINATING ACTION AD 2009-08-01, EFF 5/14/2009. THIS AD SUPERSEDES PREVIOUSLY CW AD 2007-07- 12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 NZ-2000 NAV COMPUTER 7018879-03030 98082029 7018879-03022 98082029 #2 NZ-2000 NAV COMPUTER 7018879-03030 96091165 7018879-03022 96091165 BOTH NAV COMPUTERS INCORPORATED HONEYWELL SB A24-6111-035, CONVERT UNITS PN 7018879-03022 TO 7018879-03030 AND SB A24-6111-046, INSTALL SOFTWARE MODIFICATION MOD “A“ STATUS. CHANGED INTERNAL BATTERIES ON BOTH NAV COMPUTERS, PN 7020116-1, NEXT DUE REPLACEMENT 4/12/2013 PER ICA DOCUMENT# 44501800 APPENDIX A NZ-2000 BATTERY REPLACEMENT CAN BE DONE BY OPERATOR. BATTERY PACK PN 7020116- 1 (OR PN 09-3642-002?) INSTALLED UNITS, OPS CKS OK. UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 241. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/16/2010 A/C 6649.4 4615 Total 2746.8 7186 INDEX NUMBER 111 EN 1 6411.9 4483 APU hrs/cyc 4635.2 7178 1888.4 APU tach adj (-) EN 2 6594.4 4586 8 APU Cyc adj (+) REMOVED COCKPIT FIRE EXTINGUISHER AND SENT TO HRD AERO SERVICES, CRS# YN2R325L, VALENCIA, CA FOR OVERHAUL AND REFILL OF HALON 1211 UNDER WO# 125719-1. THIS ACTION IS A TERMINATING ACTION OF AD 2009-0262, AD 2009-0251-E AND AD 2010-01-03 BY COMPLYING WITH PARA (G)(3), HAVING “BEEN CONCLUSIVELY DETERMINED THAT THE LAST TIME IT WAS FILLED, IT WAS FILLED WITH HALON 1211 SUPPLIED BY A COMPANY OTHER THAN LYONTECH ENGINEERING LIMITED”. RESEARCHED AND DETERMINED AD 2010-04-16 NA, PN NOT INSTALLED NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF FFE 1211 PORTABLE FIRE EXTINGUISHER BA5105-3 064502 BA5105-3 033897 UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 242. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/16/2010 A/C 6649.4 4615 Total 2746.8 7186 INDEX NUMBER 112 EN 1 6411.9 4483 APU hrs/cyc 4635.2 7178 1888.4 APU tach adj (-) EN 2 6594.4 4586 8 APU Cyc adj (+) REMOVED, SENT FOR OVERHAUL BY HRD AERO SERVICES, CRS# YN2R325L, VALENCIA, CA UNDER WO# 125694-1 (SN 1465C1) AND WO# 125695-1 (SN 14266C1), DATED 4/12/2010 AND REINSTALLED BOTH MAIN ENGINE FIRE BOTTLE ASSYS PER AMM 26-20-12-201. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF MAIN ENGINE FIRE BOTTLE 33200009 14265C1 33200009 14265C1 MAIN ENGINE FIRE BOTTLE 33200009 14266C1 33200009 14266C1 UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 243. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/16/2010 A/C 6649.4 4615 Total 2746.8 7186 INDEX NUMBER 113 EN 1 6411.9 4483 APU hrs/cyc 4635.2 7178 1888.4 APU tach adj (-) EN 2 6594.4 4586 8 APU Cyc adj (+) CW 150-200 HOUR LT AND RT THRUST REVERSER INSPECTION IAW NORDAM MM 78-30-00 CW 300-400 HOUR LT AND RT THRUST REVERSER INSPECTION IAW NORDAM MM 78-30-00 TOILET TANK HAS SLOW LEAK PAST DRAIN VALVE. REMOVED, SENT FOR OVERHAUL BY ILIFF AIRCRAFT REPAIR AND SERVICE CO, CRS# DE2R765L, TULSA, OK , UNDER WO# 04/12/2010 DATED 4/13/2010 AND REINSTALLED LAVATORY TOILET DUMP VALVE ASSY AND REPLACED TOILET TANK DUMP VALVE AND FLUSH MOTOR SEAL. LEAK CKS GOOD. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF TOILET DUMP VALVE 4650-16 080 4650-16 080 REPAINTED LAVATORY TOILET SEAT, DECK AND UNDERSIDE OF SEAT COVER AND REINSTALLED. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 244. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/22/2010 A/C 6660.4 4623 Total 2750.3 7193 INDEX NUMBER 114 EN 1 6422.9 4491 APU hrs/cyc 4638.7 7185 1888.4 APU tach adj (-) EN 2 6605.4 4594 8 APU Cyc adj (+) ACCOMPLISHED AFMS TASK 320036, LH INBD AND LH OUTBD BRAKE PAD WEAR CK IAW AMM. NEXT DUE AT 4735 CYCLES REPLACED RH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS FOR NORMAL TIRE WEAR. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 MAIN WHEEL ASSY AHA1814 WW032 AHA1814 SL105 #4 MAIN WHEEL ASSY AHA1814 LC290 AHA1814 LR165 #3 TIRE ASSY GOODYEAR FLIGHT EAGLE 237K23-2 70681023 237K23-2 83530697 #4 TIRE ASSY GOODYEAR FLIGHT EAGLE 237K23-2 70691020 237K23-2 83530721 REMOVED TIRES HAD 154 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4016, DATED 2/17/10 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 245. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/26/2010 A/C 6664.8 4629 Total 2756.6 7206 INDEX NUMBER 115 EN 1 6427.3 4497 APU hrs/cyc 4645 7198 1888.4 APU tach adj (-) EN 2 6609.8 4600 8 APU Cyc adj (+) RESEARCHED AD 2010-06-11, EFFECTIVE 4/21/2010. ENGINE #1, SN P-91363, NA BY PN AND SN. ENGINE #2 SN P-91371 HAS A LOW PRESSURE COMPRESSOR ROTOR DISK (LPCR) ON THE LP 3rd STAGE THAT THIS AD APPLIES TO PER PARAGRAPH (g). DISC PN IS 3072397, SN IS 6-12112-1245. THIS DISC WILL BE SCHEDULED FOR REPLACEMENT BEFORE 8600 HOURS PART TOTAL TIME OR THE NEXT TIME THE INTERMEDIATE CASE IS REMOVED FROM THE LOW PRESSURE CASE PER PROVISIONS OF PARA (g) (1) AND (2). SB TFE731-72-A3748, TFE731-72-A3749 AND AD NOTE 2010-06-11 COMPLIANCE STATEMENT ENTRIES MADE IN RESPECTIVE ENGINE LOGBOOKS. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 246. APU INSPECTION /MAINTENANCE RECORD FAA CRS PB8R624N / West Palm Beach, FL MODEL: Hawker 800A ACTT: 6680.7 SERIAL NO.: 258-128 ACTL: 4645 REGISTRATION NO.: NXXGS DATE STARTED: 05/21/10 WORK ORDER NO.: SC6421 DATE COMPLETED: 05/19/10 ENGINE MODEL: T62-40C8D1 ENGINE TOTAL TIME: 2763.8 7232 CYCLES TIME SINCE OVERHAUL: N/A Component(s) Replaced: 8.1 Removed APU Fuel Nozzle Holder Assembly P/N 160238-400, S/N N/A and installed a new Holder Assembly P/N 4503159. Removed Flow Restrictor P/N 179290-1 S/N N/A and installed a new Restrictor Assembly P/N 179290-1, S/N 11992864. All work performed IAW Hamilton-Sundstrand Solar APU T62-40C8D1 MM 49-20-00. The maintenance listed above was performed in accordance with current Federal Aviation Regulations and is approved for return to service with regards to the maintenance accomplished. Further details are on file at this repair station under the above work order. Authorized RTS Signature Sean Barry, Airworthiness Inspector CAH For; General Dynamics Aviation Services West Palm Beach, FL 33406 FAA CRS PB8R624N
- 247. INSPECTION / MAINTENANCERECORD FAA CRS PB8R624N / West Palm Beach, FL. MODEL: Hawker 800A ACTT: 6680.7 SERIAL NO.: 258-128 ACTL: 4645 REGISTRATION NO.: NXXGS DATE: 05/19/10 WORK ORDER NO.: SC6421 PAGE: 1 of 1 Component(s) Replaced: 6.1 Removed No. 1 Main Battery P/N RG-39E, S/N 40251482 and performed top charge and installed in the No. 2 position IAW Hawker 800A MM 24-30-00. Removed No. 2 Main Battery P/N RG-39E, S/N 40251513 and performed top charge and installed in the No. 1 position IAW Hawker 800A MM 24-30-00. 8.1 Removed APU Fuel Nozzle Holder Assembly P/N 160238-400, S/N N/A and installed a new Holder Assembly P/N 4503159. Removed Flow Restrictor P/N 179290-1 S/N N/A and installed a new Restrictor Assembly P/N 179290-1, S/N 11992864. All work was performed IAW Hamilton-Sunstrand Solar APU T62-40C8D1 MM 49-20-00. The maintenance listed above was performed in accordance with current Federal Aviation Regulations and is approved for return to service with regards to the maintenance accomplished. Further details are on file at this repair station under the above work order. Authorized RTS Signature Sean A. Barry, Airworthiness Inspector For; General Dynamics Aviation Services West Palm Beach, FL 33406 FAA CRS PB8R624N
- 248. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/22/2010 A/C 6684.1 4648 Total 2767.3 7236 INDEX NUMBER 117 EN 1 6446.6 4516 APU hrs/cyc 4655.7 7228 1888.4 APU tach adj (-) EN 2 6629.1 4619 8 APU Cyc adj (+) CREW REPORTS VIBRATION FROM NLG AFTER RETRACTION, NO NLG SHIMMY ASSOCIATED WITH THIS SQUAWK. NO FAULTS FOUND IN WHEEL WELL AREA. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LT NLG WHEEL AND TIRE ASSY AH52339 DW061 AH52339 QA033 RT NLG WHEEL AND TIRE ASSY AH52339 149,1045 AH52339 QG038 TIRES HAD 85 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270, UNDER WO 4041, DATED 4/13/2010. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 249. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/26/2010 A/C 6684.1 4648 Total 2767.3 7236 INDEX NUMBER 118 EN 1 6446.6 4516 APU hrs/cyc 4655.7 7228 1888.4 APU tach adj (-) EN 2 6629.1 4619 8 APU Cyc adj (+) CW ATA TASK 570010, 900 HOUR SPECIAL INSPECTION OF LH AND RH WING BOTTOM SKIN ADJACENT TO FLAP OUTBOARD HINGE AT RIB 8 PER APH-0608 ICA TO API WINGLETS STC: ST01411SE. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 250. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/1/2010 A/C 6688.8 4654 Total 2777.8 7254 INDEX NUMBER 119 EN 1 6451.3 4522 APU hrs/cyc 4666.2 7246 1888.4 APU tach adj (-) EN 2 6633.8 4625 8 APU Cyc adj (+) REMOVED AND REPLACED FO EMERGENCY OXYGEN MASK. OP CK OF MASK, OXYGEN FLOW AND COMMUNICATIONS OK FOR SERVICE. INSTALLED MASK BOUGHT FROM AND OVERHAULED BY MASTER AIR PARTS, INC, 3070 SKYWAY DRIVE SUITE 303, SANTA MARIA, CA 93455, TEL (805) 928-2929, CRS 1MPR946Y UNDER WO# M1720 DATED 05/26/2010. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF EMERGENCY OXYGEN MASK CAPT MC10-14-124 58516 MC10-14-51 13604 RESEARCHED AD 2010-11-05, EFF 7/6/2010 “AVOX SYSTEMS AND B/E AEROSPACE OXYGEN CYLINDERS AS INSTALLED ON VARIOUS 14 CFR PART 23 AND CAR 3 AIRPLANES” AND FOUND NA BY MAKE. THIS AIRCRAFT HAS TWO WALTER KIDDE OXYGEN BOTTLES CURRENTLY INSTALLED: BOTH PN WKA37447, #1 POS SN 14510X, #2 POS SN 560655. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 251. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/28/2010 A/C 6707.7 4666 Total 2783.8 7273 INDEX NUMBER 120 EN 1 6470.2 4534 APU hrs/cyc 4672.2 7265 1888.4 APU tach adj (-) EN 2 6652.7 4637 8 APU Cyc adj (+) COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1& #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4741 LANDINGS. CW REINSPECTION OF LAVATORY RECEPTACLES AND PLACARDS PER AD 74-08-09 R2. NEXT DUE IN 1000 HOURS. COMPLETED AFMS TASK 720005, 150 TO 250 HOUR ENGINE ROUTINE PERIODIC INSPECTION, LT AND RT ENGINES. NEXT DUE IN 250 HOURS AT 6958 AFTT . SOAP SAMPLES TAKEN FOR #1 AND #2 ENGINES, NEW OIL FILTERS, PN 3070945-1, O- RING PN S9413-06 INSTALLED, CKD LH AND RH ENG CHIP DETECTORS, RAN BOTH ENGINES TO LEAK CHECK NEW FILTERS, CKS OK. SERVICED OIL LEVEL TO FULL. NORMAL RESAMPLE NEXT DUE IN 150 HOURS AT 6858 AFTT. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 252. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/20/2010 A/C 6711 4672 Total 2786.9 7278 INDEX NUMBER 121 EN 1 6473.5 4540 APU hrs/cyc 4675.3 7270 1888.4 APU tach adj (-) EN 2 6656 4643 8 APU Cyc adj (+) COMPLETED AFMS TASKS 335010, REPLACED AND CHECKED FWD AND AFT EMERGENCY EXIT POWER SUPPLY “D” CELL NI-CAD BATTERIES WITH NEW, 2 EACH PER BATTERY PACK, PN AD- 4002P, NSN, BATCH NUMBER BA5526. BATTERIES OBTAINED FROM MFG’R, AREO DESIGN, INC, 385 INDUSTRIAL DR, MT. JULIET, TN, 37122, PH 800-551-1158, PRODUCTION APPROVAL HOLDER ( PAH ) # PQ1465CE, WORK ORDER # 10- 18693, DATED 7/19/2010. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 253. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/20/2010 A/C 6711 4672 Total 2786.9 7278 INDEX NUMBER 122 EN 1 6473.5 4540 APU hrs/cyc 4675.3 7270 1888.4 APU tach adj (-) EN 2 6656 4643 8 APU Cyc adj (+) F.A.A. CRS YRR8491L 900 Nolen Dr, Suite 100 Dallas, Texas 76501 CUSTOMER: XX XXX LLC REG:NXXGS A/C S/N: 2581XX TSN: 6711.0 CSN: 4672 CUSTOMER ENG: TFE731-5R-1H S/N: P-91363 TSN: 6473.5 CSN: 4540 POS: #1 Disassembled engine S/N P-91363 to investigate for Metal in oil system. Sent removed components to repair facility for inspection and/or repair. Ref. work order FS20187 line 3 for items replaced during inspection. Reassembled engine with repaired components and replaced the following items at reassembly. Installed 1ea repaired condition Lube Pump P/N 3071949-12 S/N 98-14057-0416. Installed 1ea new condition Breather Valve P/N 3075323-3 NSN. Installed New condition Accy Gearbox Garloc Seals P/N 3072784-2. Installed Fan assembly with final stretch Dim. Of .0055 per Honeywell TFE731-5 LLM. Complied with ground run, leak check, setup And operational checks on engine S/N P-91363. NO DEFECTS NOTED. All maintenance has been accomplished with reference to the TFE731-5 Light Maintenance Manual and Hawker 800 maintenance manual. This certified that only the work requested by the customer, listed above and described on our sales order, was accomplished. The work performed was inspected with reference to the manufacturer’s specifications and current Federal Aviation Administration regulations and is approved for return to service. The pertinent details of the repair are on file at this agency under: Work order FS20187. # NOMENCLATURE PN OFF SN OFF PN ON SN ON CONDITION 1 #1 CARBON SEAL 3060457-1 08-05158-13844 3075675-2 10-169020-00176 FN 5 BALL BEARINGS 3072885-1 87-06049-9644 3072885-1 09-06331-08803 FN 87-06049-9642 09-06331-08809 FN 87-06049-9643 09-06331-13721 FN 87-06049-9646 09-06331-13755 FN 87-06049-9641 09-06331-08800 FN 3 BALL BEARINGS 3072884-1 87-06049-10653 3072884-1 09-182386-07057 FN 87-06049-10656 09-182386-07060 FN 87-06049-10633 09-182386-07075 FN 2 BALL BEARINGS 3072883-1 8706049-10915 3072883-1 09-06331-15756 FN 8706049-10935 09-06331-15803 FN 1 SEAL 3072784-2 NSN FN 1 ADAPTER OIL 3071355-1 NSN FN Signed log entry in engine #1 logbook UPDATED AVTRAK RECORDS WITH PART CHANGES
- 254. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/27/2010 A/C 6724.1 4680 Total 2793 7291 INDEX NUMBER 123 EN 1 6486.6 4548 APU hrs/cyc 4681.4 7283 1888.4 APU tach adj (-) EN 2 6669.1 4651 8 APU Cyc adj (+) REPLACED RH NAV LIGHT ASSY DUE TO DIM LED BARS. NEW UNIT OBTAINED AS A WARRANTY REPLACEMENT FROM API. NEW UNIT OP CKS GOOD. CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 4920004. CW APU BIENNIAL/1500 HR/3000 CYCLE MAINTENANCE AVTRAK TASK 492005. DRAINED AND SERVICED APU OIL WITH MOBIL 254. REPLACED APU OIL FILTER ELEMENT. CLEANED APU FUEL INLET FILTER PN 211-326 AND REPLACED FILTER SEAL PN 3500AS12. RAN APU, LEAK AND OP CKS OK. NOMENCLATURE PN OFF SN OFF PN ON SN ON NAV LIGHT ASSY H800-0353-2 041 H800-0353-2 301 OIL FILTER 169009-1 NSN 179411 NSN UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 255. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/9/2010 A/C 6735.3 4690 Total 2799.2 7303 INDEX NUMBER 124 EN 1 6497.8 4558 APU hrs/cyc 4687.6 7295 1888.4 APU tach adj (-) EN 2 6680.3 4661 8 APU Cyc adj (+) COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1& #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4765 LANDINGS. REPLACED LH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS FOR NORMAL TIRE WEAR. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA1814 SL105 AHA1814 XB003 #2 MAIN WHEEL ASSY AHA1814 LR165 AHA1814 XB007 #1 TIRE GOODYEAR FLT EAGLE 237K23-2 00963011 237K23-2 70710842 #2 TIRE GOODYEAR FLT EAGLE 237K23-2 00963019 237K23-2 70690853 REMOVED TIRES HAD 142 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4076, DATED 6/26/10 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 256. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/10/2010 A/C 6735.3 4690 Total 2799.2 7303 INDEX NUMBER 125 EN 1 6497.8 4558 APU hrs/cyc 4687.6 7295 1888.4 APU tach adj (-) EN 2 6680.3 4661 8 APU Cyc adj (+) SOAP SAMPLES TAKEN EARLY (25 HOURS) ON #1 AND #2 ENGINES PER HONEYWELL ENGINEERING. NEW OIL FILTERS, PN 3070945-1, O- RINGS PN S9413-06 INSTALLED, LH AND RH ENG CHIP DETECTORS CHECK OK, RAN BOTH ENGINES FOR LEAK/OP CK, OK FOR SERVICE. SERVICED OIL LEVEL TO FULL. NORMAL RESAMPLE NEXT DUE IN 150 HOURS AT 6885 AFTT. TOTAL TIME SINCE #1 OIL CHANGE @6470.2 ETSN: 24.3 HOURS TOTAL TIME SINCE #2 OIL CHANGE @5835.7 ETSN: 844.6 HOURS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 257. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/17/2010 A/C 6752.2 4698 Total 2805.6 7315 INDEX NUMBER 126 EN 1 6514.7 4566 APU hrs/cyc 4694 7307 1888.4 APU tach adj (-) EN 2 6697.2 4669 8 APU Cyc adj (+) LH STARTER GENERATOR BEGINNING TO CREATE SUBSTANTIALLY MORE RESIDUE FROM COOLING VENT. GENERATOR REPLACED 147 HOURS EARLY AS PRECAUTIONARY MEASURE. WORK ACCOMPLISHED IAW AMM 24-30-21-401, OP CKS OK. COMPLIED WITH AFMS TASK 240001, STARTER GENERATOR INSPECTION BY REPLACEMENT OF #1 ENGINE STARTER GENERATOR INSTALLED STARTER GENERATOR OBTAINED FROM ALL WEST AVIATION, OVERHAULED BY WECO AEROSPACE, INC., 1501 AVIATION BLVD, LINCOLN, CA 95648, PH (913) 645-8961 UNDER WO# C8026 DATED 3/15/2007 REMOVED UNIT HAD 869 HOURS AND 715 CYCLES AT REPLACEMENT. NOMENCLATURE PN OFF SN OFF PN ON SN ON STARTER GENERATOR 23080-005 6949 23080-064 2428 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 258. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/30/2010 A/C 6752.2 4698 Total 2805.6 7315 INDEX NUMBER 127 EN 1 6514.7 4566 APU hrs/cyc 4694 7307 1888.4 APU tach adj (-) EN 2 6697.2 4669 8 APU Cyc adj (+) REPLACED ARTEX ELT BATTERY FOR LIFE LIMIT REQUIREMENTS IAW INSTALLATION INSTRUCTIONS IN ARTEX DOCUMENT 571-0406 REV C, DATED 10/13/2008. AVTRAK TASK CODE 256005. BATTERY NEXT DUE REPLACEMENT OCTOBER 31, 2015. CW ELT INSPECTION REQUIREMENTS OF CFR 91.207 & 91.409 PER ARTEX INSTALLATION AND OP MANUAL PG 4-3, STEPS 1-4, AND 6-9. AVTRAK TASK CODE 256000. NOMENCLATURE PN OFF SN OFF PN ON SN ON ELT BATTERY 452-0133 NSN 452-0133 NSN UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 259. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/24/2010 A/C 6764 4711 Total 2814.8 7332 INDEX NUMBER 128 EN 1 6526.5 4579 APU hrs/cyc 4703.2 7324 1888.4 APU tach adj (-) EN 2 6709 4682 8 APU Cyc adj (+) INSTALLED TWO CONCORDE RG-390E MAIN BATTERIES PURCHASED NEW FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE, AZUSA, CA 91702, TEL (626) 969-7227. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 BATTERY RG-390E 40383367 RG-390E 40251482 #2 BATTERY RG-390E 40383366 RG-390E 40251513 UPDATED AVTRAK MAIN BATT CAP CK AND INSTALL RECORDS, TASKS 241015, 241016, 241021, 241022. CW AFMS TASK 050050 200 HR AND AFMS TASK 050790 400 HR LUBRICATIONS. CW AFMS TASK 050800 400 HOUR DETAILED WALK AROUND INSPECTION. CW AFMS TASK 320036 CK OF BRAKE UNIT WEAR , NEXT DUE 4786 LANDINGS. UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 260. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/1/2010 A/C 6772.9 4717 Total 2820 7340 INDEX NUMBER 129 EN 1 6535.4 4585 APU hrs/cyc 4708.4 7332 1888.4 APU tach adj (-) EN 2 6717.9 4688 8 APU Cyc adj (+) INSTALLED ONE CONCORDE RG-126 AUX BATTERY PURCHASED NEW FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE, AZUSA, CA 91702, TEL (626) 969-7227. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 (UJ) AUX BATTERY RG-126 40400072 RG-126 40126243 AVTRAK TASK 241017 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 261. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/4/2010 A/C 6776 4721 Total 2822 7344 INDEX NUMBER 130 EN 1 6538.5 4589 APU hrs/cyc 4710.4 7336 1888.4 APU tach adj (-) EN 2 6721 4692 8 APU Cyc adj (+) CREW REPORTS INTERMITTENT #2 FLIGHT DIRECTOR FAIL INDICATION. REPLACED #2 FLIGHT GUIDANCE COMPUTER, OP CKS OK. PART PURCHASED REPAIRED FROM HONEYWELL, 7825 RIDGEPOINT DR, IRVING, TX 75063, CRS# TT1R518K, UNDER WO#5003693637, DATED 9/3/2010. FAILED UNIT HAD 138.1 HOURS AND 115 CYCLES SINCE INSTALL. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 FZ-800 FLIGHT GUIDANCE COMPUTER 7003974-732 99025228 7003974-732 00105672 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 262. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/7/2010 A/C 6831.1 4762 Total 2854.3 7399 INDEX NUMBER 131 EN 1 6593.6 4630 APU hrs/cyc 4742.7 7391 1888.4 APU tach adj (-) EN 2 6776.1 4733 8 APU Cyc adj (+) COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1 & #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4837 LANDINGS. REPLACED RH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS FOR NORMAL TIRE WEAR. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 MAIN WHEEL ASSY AHA1814 XB003 AHA1814 WW032 #4 MAIN WHEEL ASSY AHA1814 XB007 AHA1814 LC290 #3 TIRE GOODYEAR FLT EAGLE 237K23-2 01992049 237K23-2 70681023 #4 TIRE GOODYEAR FLT EAGLE 237K23-2 01422523 237K23-2 70691020 REMOVED TIRES HAD 139 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4230, DATED 11/19/2010. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 263. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/11/2010 A/C 6833.3 4762 Total 2856.3 7401 INDEX NUMBER 132 EN 1 6595.8 4630 APU hrs/cyc 4744.7 7393 1888.4 APU tach adj (-) EN 2 6778.3 4733 8 APU Cyc adj (+) FOUND #1 ENG THRUST REVERSER OUTBOARD PRIMARY ACTUATOR LEAKING DURING TR INSPECTION. REPLACED #1 ENG OB PRIMARY ACTUATOR IAW NORDAM GROUP TR5000 MM 78-32-40 M-RAH17, REV4, DATED MAY, 2004. LEAK AND FUNCTION TESTS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LH ENG OB THRUST REVERSER PRIMARY ACTUATOR 5453512-19 528 5453512-1 202 OVERHAULED ACTUATOR OBTAINED FROM THE NORDAM GROUP – NACELLE/THRUST REVERSERS SYSTEMS DIVISION, 6911 N. WHIRLPOOL DR, TULSA, OK 74117, CRS#NZ6R569Y UNDER WORK ORDER # R10-2201 DATED 9/16/2010. COMPLETED 150-250 HR AND 300-400 HR TR INSPECTION ON LH AND RH THRUST REVERSERS, AVTRAK TASK 783003, 783004, 783007 & 783008. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 264. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/14/2010 A/C 6833.3 4762 Total 2856.3 7401 INDEX NUMBER 133 EN 1 6595.8 4630 APU hrs/cyc 4744.7 7393 1888.4 APU tach adj (-) EN 2 6778.3 4733 8 APU Cyc adj (+) REPLACED INOP FMS DATA LOADER. NEW UNIT CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF FMS DATA LOADER DL- 900 701660-901 04033361 701660-901 97091047 REPAIRED DATA LOADER OBTAINED FROM HONEYWELL, 7727 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K UNDER WORK ORDER# 5003772434 DATED 10/05/2010. CAP CK’D CONCORDE RG-131 IRS BATTERY, S/N: 40273576, AVTRAK TASK 241030. NEXT DUE CAP CK 12/13/2011, REINSTALLED SAME. CAP CK’D CONCORDE RG-126 BATTERIES IN #3 AUX POS, S/N: 40400072, AVRTAK TASK 241017 AND #5 AUX POS, SN 40184860, NEXT DUE CAP CK 12/13/2011, REINSTALLED SAME WEIGHED AND REINSTALLED CABIN FIRE EXTINGUISHER, AVTRAK TASK 262136. WEIGHED AND REINSTALLED COCKPIT FIRE EXTINGUISHER, AVTRAK TASK 262135. REMOVED AND CAP CK’D #4 PN RG-126 AUX BATTERY, BATTERY FAILED TEST/RETEST. INSTALLED NEW BATTERY FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE, AZUSA, CA 91702, TEL 626-969-7227 IN #4 POSITION. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #4 AUX BATTERY RG-126 40413638 RG-126 40280430 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 265. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/6/2011 A/C 6843.6 4775 Total 2862.1 7415 INDEX NUMBER 134 EN 1 6606.1 4643 APU hrs/cyc 4750.5 7407 1888.4 APU tach adj (-) EN 2 6788.6 4746 8 APU Cyc adj (+) WEIGHED AND REINSTALLED CABIN FIRE EXTINGUISHER, AVTRAK TASK 262136. WEIGHED AND REINSTALLED COCKPIT FIRE EXTINGUISHER, AVTRAK TASK 262135. COMPLETED AFMS TASK 05020 INSPECTION “E”. COMPLETED API WINGLET CONDITION INSPECTION OF WING TIP STROBES AND NAV LIGHT LENSE, OK FOR SERVICE. TESTED CDS-R SYSTEM PER PROCEDURE DOCUMENT 050908018 IAW STC ST01406WI-D ICA SWAPPED MAIN BATTERY POSITIONS FOR BATTERY LONGEVITY. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 BATTERY RG-390E 40383366 RG-390E 40383367 #2 BATTERY RG-390E 40383367 RG-390E 40383366 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 266. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/28/2011 A/C 6853.7 4784 Total 2866 7421 INDEX NUMBER 135 EN 1 6616.2 4652 APU hrs/cyc 4754.4 7413 1888.4 APU tach adj (-) EN 2 6798.7 4755 8 APU Cyc adj (+) CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 267. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.6 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/2/2011 A/C 6853.7 4784 Total 2866 7421 INDEX NUMBER 136 EN 1 6616.2 4652 APU hrs/cyc 4754.4 7413 1888.4 APU tach adj (-) EN 2 6798.7 4755 8 APU Cyc adj (+) RESEARCHED AD 2011-01-09, EFF 2/9/2011 “B/E AEROSPACE PROTECTIVE BREATHING EQUIPMENT (PBE) PART NUMBER 119003-11 INSTALLED ON VARIOUS TRANSPORT AIRPLANES”. FOUND THIS AD NA PART NUMBER, PART NOT INSTALLED AT THIS TIME. THIS AIRCRAFT HAS ONE PBE INSTALLED, AVOX SYSTEMS INC, FORMERLY SCOTT AVIATION, INC PN 802300-14, NSN, REPLACEMENT DATE OF MAY, 2011. UPDATED MOD RECORD BOOK AND AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 268. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.7 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/23/2011 A/C 6863.6 4794 Total 2867 7423 INDEX NUMBER 137 EN 1 6626.1 4662 APU tach 4755.4 7415 1888.4 APU tach adj (-) EN 2 6808.6 4765 8 APU Cyc adj (+) CW ELT INSPECTION REQUIREMENTS OF CFR 91.207 & 91.409 PER ARTEX INSTALLATION AND OP MANUAL PG 4-3, STEPS 1-4, AND 6-9. AVTRAK TASK CODE 256000. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 269. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.7 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/23/2011 A/C 6863.6 4794 Total 2867 7423 INDEX NUMBER 138 EN 1 6626.1 4662 APU tach 4755.4 7415 1888.4 APU tach adj (-) EN 2 6808.6 4765 8 APU Cyc adj (+) RESEARCHED AD 2010-07-02, EFF 5/3/2010 FOUND NA TO THIS AIRCRAFT BY PART NUMBER, AFFECTED PN NOT INSTALLED AT THIS TIME. THIS AD SUPERSEDES AD 2006-22-05 (ALSO DETERMINED TO BE NA BY PN) RE AIRCRAFT EQUIPPED WITH HONEYWELL PRIMUS II RNZ-850()/-851() INTEGRATED NAVIGATION UNITS (INUs). UPDATED MOD RECORD BOOK AND AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 270. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.7 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/2/2011 A/C 6869.1 4797 Total 2867.5 7423 INDEX NUMBER 139 EN 1 6631.6 4665 APU tach 4755.9 7415 1888.4 APU tach adj (-) EN 2 6814.1 4768 8 APU Cyc adj (+) RE-REGISTERED 406 MHz ELT, NATIONAL ENVIRONMENTAL SATELLITE, DATA AND INFORMATION SERVICE (NESDIS) BEACON ID 2DC755E58CFFBFF, NEXT DUE 3/2/2013. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ NXXGS Service Bulletin and Airworthiness Directive Compliance Record Engine PN TFE731-5R-1H PN: 3074600-1 #1 SN: P91363 #2 SN: P91371 Bulletin Number #1 Eng Date #2 Eng Date Description 72-3001 R1 4/11/1988 Service Life limits of critical life limited components 72-3001 R41 8/14/1995 Life Limited parts 72-3001 R51 6/15/2007 Life limits of critical parts 72-3001 R6 Accomplish at next MPI and updated at each subsequent MPI 72-3078 R1 4/11/1988 Installed new bolts with lock wire feature 72-3219 R1 4/11/1988 Identify Lp & HP rotors after replacement 72-3234 R5 10/8/1998 Rework or replace ITL PN 3070039-4 to -6. 3072337-1,2 72-3237 R3 10/8/1998 Install HP compressor impeller 72-3253 R1 4/11/1988 Rework/replace fourth stage LP compressor stator 72-3253 R3 12/6/1989 Inactive by 3/2011 72-3263 R1 4/11/1988 Inspection intervals –establishing periodic inspection intervals 72-3263 R11 10/8/1998 Establish periodic inspection intervals-5 72-3263 R14 6/15/2007 Verified periodic inspections 72-3263 R3 12/16/1989 Establishing periodic inspection intervals, R 14 current as of 3/2011 72-3263 R9 8/14/1995 Periodic Insp 72-3275 R1 4/11/1988 Install improved seal in diffuser 72-3279 R1 4/11/1988 Permanently plug compress interstage diffuser 72-3287 R2 4/11/1988 Rework/replace accessory drive gearbox housing assembly 72-3292 R1 4/11/1988 Wiring harness installation incorporates additional hardware 72-3293 R1 4/11/1988 Accessory drives –replace shim at transfer gearbox 72-3296 R1 4/11/1988 Replacement of number one bearing in specified engines 72-3304 R2 4/11/1988 Replace/rework fan disk nut 72-3310 R1 4/11/1988 Inspect/replace radially mismatched third stage LP to turbine 72-3322 R1 4/11/1988 Permanently plug compressor interstage diffuser boroscope
- 271. 72-3327 R1 4/11/1988Replace bolts in LP compressor bearing housing 72-3329 R1 4/11/1988 Convert engine part numbers 72-3332 R1 4/11/1988 Replace/rework fan support shaft and housing assembly 72-3334 R1 4/11/1988 Replacement of number three compressor bearing retainer nut 72-3336 R1 4/11/1988 Install silver plated string washers in planet gear shaft 72-3342 R5 10/8/1998 Lance Peen fan hub 3072816-1/-2, 4621-1/-3, 5163-1/-3 72-3347 R1 4/11/1988 Install redesigned combustion system 72-3354 R0 12/16/1989 Installation dinner transition liner PN numerals 3072337-4 72-3354 R1 4/11/1988 Turbine section –install in our transition liner 72-3356 R1 4/11/1988 Install pinion sun gear shaft assembly with improved 72-3357 R1 4/11/1988 Compressor section –replace spring tension washer 72-3362 10/8/1998 Perform 1 time inspection four specific lot number on first stage LPT 72-3366 10/8/1998 Replace/rework scavenge inlet baffle 72-3368 R1 10/8/1998 Install pinion gear PN 3075213-4 or 3075231-4 72-3369 R4 10/8/1998 Adjust a-5 A.E. 72-3383 12/16/1989 Installation stainless steel oil tube PN 3075295-1. 72-3387 12/16/1989 NA inspection and re-identification of LPT third stage rotor disk 72-3389 12/16/1989 NA install pin (sun) gear shaft assembly with dampner rings 72-3392 12/16/1989 NA Inactive by 3/2011, R1 72-3494 Accomplish at next MPI and updated at each subsequent MPI 72-3397 R2 6/15/2007 Initiate compliance record 72-3397 R2 8/14/1995 Initiated component maintenance/modification record card 72-3398 12/16/1989 NA replaced number two bearing retainer PN 3074776-2 72-3403 R1 10/8/1998 Installed circuit and third LPT nozzles 72-3405 R1 8/14/1995 Replace shroud retaining sleeve HPT 72-3408 12/29/1993 Replaced spring tension washer 3000005-2/-56 W/-64 72-3409 R1 10/8/1998 LPC first stage believe retainers 72-3410 R1 10/8/1998 LPC second stage blade retainers 72-3411 R1 10/8/1998 LPC third stage labor towers 72-3413 8/14/1995 Install DR valves & tee pl that include lock wire holes 72-3416 R5 10/8/1998 Installed each PC shroud/aluminum coding 72-3421 10/8/1998 Install number three bearing housing-2, 3 opt -5 rec 72-3431 10/8/1998 Replaced number five bearing 72-3436 R2 11/22/1991 Inactive by 3/2011, R3 72-3438 R2 10/8/1998 Replaced number three bearing nut 72-3439 R1 8/14/1995 Replaced HPT nozzle anti-rotation ring 72-3443 10/8/1998 Inspect second LPC shroud 72-3449 10/8/1998 Installed each PC support washers 72-3455 R3 10/8/1998 Transfer tube seals 72-3457 10/8/1998 Replaced rework air seal to 3074754-2 on third stage LPT stator 72-3458 R3 8/14/1995 Eddy current inst for fan or rotor disks 72-3458 R5 10/8/1998 Eddy current instructions for fan disks 72-3465 5/26/1992 Compliance with SB 731-72-3436 completed and no further rework rqd, PN 3075435-2 per para1.A Rework rqd next access to Ring Gear PN 3077067-1/-2 per para 1.A. 72-3465 R1 8/14/1995 Installed new retaining ring for fan shaft 72-3467 R2 8/14/1995 Inspect fan rotor assy containing disc and hub 72-3467 R2 10/8/1998 Inspect fan disk PN 3074621 & 3075163 72-3468 R2 8/14/1995 Replace #1 carbon seal and rotor 72-3469 12/23/1993 Inactive by 3/2011, R3 72-3476 R1 8/14/1995 Install piston ring 3000002-10 72-3477 10/8/1998 Replaced accessory drive gearbox gasket 72-3483 R2 10/8/1998 Install LPC fourth stage compressor 72-3494 R 8 4/30/2007 High pressure turbine/low pressure turbine blade tracking 72-3494 R1 8/14/1995 HP& LP turbine blades hourly tracking 72-3494 R3 10/8/1998 HPT& LPT blade hour tracking
- 272. 72-3495 R1 12/23/1993Inactive by 3/2011, R4 72-3522 R1 4/30/2007 Replacement of and spinner not applicable by part number 72-3532 10/8/1998 Rework compressor interstage diffuser 72-3534 R1 8/14/1995 Install/rework first stage LPT stator 72-3539 8/14/1995 Install fan spinner PN 3074623 72-3541 R3 10/8/1998 #4 & #5 bearing sump scavenge 72-3542 10/8/1998 Install second stage LPC frequency/blades 72-3548 12/23/1993 Replace pinion nut locking nut 72-3576 R3 10/8/1998 Remove and replace first stage LPT rotor and second stage seal rotor 72-3579 R2 10/8/1998 Controlled fit combustor 72-3587 12/14/1997 Rework/install LP third stage turbine rotor assembly 72-3588 10/8/1998 Rework/install transition duct 72-3595 4/30/2007 Replacement of 2nd LPT rotor assembly 72-3597 R4 10/8/1998 Rep. main shaft carbon rings seals/vent oil System 72-3600 10/8/1998 Install LPC stator shim 72-3602 10/8/1998 HPT nozzle tangs inspection category 3 recommended 72-3603 R1 10/8/1998 Compressor inter. diffuser inspection rework 72-3604 R2 10/8/1998 Rework transfer gear box 72-3605 R2 10/8/1998 Accessory gearbox assembly 72-3606 10/8/1998 Identify, inspected and replace combustion plenums 72-3611 10/8/1998 Inspect/and remove specific third stage LPT blades 72-3613 R2 10/8/1998 Replace #1 & # 3 carbon seal and associated components 72-3614 10/8/1998 Rework number 1 seal housing 72-3615 10/8/1998 Rework breather valve 72-3620 Future future 9/20/11 Install LPT 1st ITT duct and 2nd stage turbine nozzle and rotor assy’s for improved LP turbine efficiency. Accomplish at next access in conjunction with 72-3768 72-3622 10/8/1998 Install LP 2nd stage turbine nozzle assembly and associated component parts 72-3635 4/30/2007 Inspection/rework of oil filter cover 72-3640 12/31/1998 Inactive by 3/2011, R4 72-3641 R6 6/15/2007 Eddy current inspection of impeller 72-3645 R1 4/30/2007 Inspection/replacement of specific A4 nozzle segments 72-3653 4/30/2007 Replacement of specific 2nd low pressure turbine rotating seals NA PN 72-3655 4/30/2007 Replacement of 1st stage low pressure turbine nozzle assembly 72-3662 R6 6/15/2007 Replace #4 and #5 carbon seals 72-3664 4/30/2007 Inspection replacement of tie bolt 72-3672 4/30/2007 Identification of 1st low pressure turbine nozzle(less seal and support) 72-3674 R2 4/30/2007 Inspection of specific mainframe assemblies NA to engine SN 72-3686 R2 4/30/2007 Inspection of specific 3rd LPT blades 72-3687 11/27/2002 NA REMOVE SPECIFIC IDENTIFIED LP COMPRESSOR 2nd STAGE (LPC2) 72-3691 R1 4/30/2007 Inspection of specific 3rd LPT blades NA by disk sn and mx history 72-3693 R1 4/30/2007 Inspection replacement of specific HPT retaining nuts 72-3696 6/14/2008 New air-oil separator pn 3075781-1. 72-3699 4/30/2007 Replacement of specific HPT disks NA SN 72-3708 4/30/2007 Replacement of specific 2nd LPT blades NA by disk SN 72-3714 R5 4/30/2007 Inspection of specific mainframe assys, NA by engine SN 72-3720 4/30/2007 Insp/replacement of specific HPT disks NA SN (also 10/26/06) 72-3720 10/26/06 Inspect/Replace HPT Discs, P/N 3075772 AD 2008-02-19, eff 3/6/2008. All suspect HP turbine rotor discs removed must pass a curvic root radius inspection to reinstall in the engine.NA
- 273. 72-3739 6/14/2008 Improved designof the carbon seal #1 pn 3060457-1, sn 08- 05158-13844, #3 pn 3060458-1, sn 08– 05158 – 15895 72-3764 8/17/2011 8/17/2011 NA both engs by sn. 3rd stage compressor, LPC disk, #1 sn 6- 12112-1234, #2 sn 6-12112-1245 72-A3748 10/21/2008 NA replace specified second stage LPC second and third stage LPC 3 rotor desks 72-A3749 4/26/2010 NA SB’s 72-A3748, 8/21/2008, and 72-A3749, 8/21/2008, require removing at the next access, second and third stage LPCR discs per SN. AD 2010-06-11, eff 4/21/2010 require removing discs within 100 cycle. 72-3759 R1 12/2/2011 72-3760 R1 NA NA 12/2/2011, original issue 9/2/2011 NA by PN. 72-3768 Future Future 9/20/11 Install new LPT1 Rotor at nest access or CZI. 72-3769 NA NA 9/2/2011 NA by PN 72-3770 NA NA 9/2/2011 NA by PN 72-3773 9/2/2011 Install Stage 4 case and vane assy, PN 3074555-10 or -11 whenever case vane assy -8 requires replacement. 72-3774 NA NA 9/20/2011 NA by PN 72-3778 NA NA Install LPC2 shroud, na to this eng pn 73-30 41 R1 4/11/1988 Install electronic engine control EEC 73-3075 R1 4/11/1988 Replace fuel call differential pressure ind 73-3075 R5 10/8/1998 Replace fuel pump differential pressure indicator 73-3078 R1 4/11/1988 Engine fuel control installation of fuel pump update record 73-3080 R1 4/11/1988 Replace/and rework fuel manifold and matched set assembly 73-3083 R1 4/30/2007 Replacement of specific fuel pumps NA SN 73-3083 R1 4/11/1988 Replace fuel pump anti-icing valve 73-3089 R1 4/11/1988 Deletion of fuel heater check valve mount 73-3091 R1 4/11/1988 Install reworked fuel control with improved governor 73-3108 8/14/1995 Install fuel control P3 gasket 73-3109 R1 4/30/2007 Maintenance of engine service tubes and clamps 73-3110 2/24/1992 NA replace secondary flexible hose assembly 73-3113 8/14/1995 Replaced fuel heater outlet 73-3115 R1 6/15/2007 Install fuel control 73-3121 3/24/1994 Replaced secondary flexible hose assembly 73-3127 10/8/1998 Rework fuel manifolds, category 3 rework 73-3131 R1 10/8/1998 One time inspection/fuel control sensor bellows 73-3134 R2 4/30/2007 Replacement of specific fuel controls NA PN 73-3137 02/26/2001 N.A. Replace fuel heater check valve PN 3073932-5 with-6 73-3138 4/30/2007 Replacement of fuel nozzle gaskets 73-3142 11/25/2002 N.A. Replace specific identified fuel control assembly 73-3147 4/30/2007 Replacement of specific fuel controls NA PN(also 5/17/2005) 73-3147 5/17/2005 Replace Specific Fuel Controls With A Suspect Overspeed Governor NA 73-3149 4/30/2007 Replacement of fuel filter element 73-3151 4/30/2007 Replacement of specific fuel pumps NA to engine model 73-3152 4/30/2007 Replacement of specific fuel controls NA PN 74-3003 R4 10/8/1998 Installed ignition unit with redundant firing circuits 74-3006 2/21/1995 Installed ignition igniter plug 3074541-1 74-3007 R1 8/14/1995 Inspect iridium igniters 76-3041 10/8/1998 Install EEC 2118002-6 76-3044 R1 4/11/1988 Replaced electronic engine control harness 76-3049 10/8/1998 Replaced specific identified DEEC 2118002-X 76-3054 8/14/1995 Install surge control P3 gasket 77-3015 R1 4/11/1988 N1 motional pickup transducer deletion of backup plate 77-3016 R1 4/11/1988 Replace thermocouple harness 77-3017 R1 4/11/1988 All replace cover plate screws on N1 compensator 77-3018 12/16/1989 Installed thermocouple harness 3073605-1 77-3021 R1 4/30/2007 Replacement of N1 transducer 79-3034 R1 4/11/1988 Replaced and rework of plug chip detector
- 274. 79-3034 R2 10/8/1998Replaced/rework of chip detector housing 79-3035 R2 4/11/1988 Replaced seal and breather pressure valve 79-3036 R1 4/11/1988 Replaced number six bearing scavenge tube assembly 79-3037 R1 4/11/1988 Incorporate improved Oil scavenge tube 79-3038 R1 4/11/1988 Replace seal in breather pressurization valve 79-3039 8/14/1995 Replace/rework #4 & #5 cavity tube 79-3039 R2 4/11/1988 Replaced rework number four and number five cavity vent tube 79-3041 R1 4/11/1988 Replacement/inspection/rework chip detector 79-3043 3/4/1991 Inactive by 3/2011, R1 79-3045 8/14/1995 Install oil in tube assembly 79-3051 10/8/1998 Install metal gasket PN: 307 5481-2 79-3052 4/30/2007 Replacement of #6 bearing oil scavenge elbow 79-3054 8/14/1995 Rework oil pump regulator section 79-3055 R1 8/14/1995 Breather valve seal and oil nozzle 79-3057 R3 4/30/2007 Replacement of oil tank site glass 79-3057 R3 10/8/1998 Oil tank bubble site glass 79-3059 R1 10/8/1998 Oil lube scavenge pump 79-3060 4/30/2007 Installation of flex oil hose 79-3062 10/8/1998 Replace de-oil valve PN 3074372-1 with PN 3074372-2 79-3065 rev 2 6/15/2007 Install metal #6 bearing oil in tube assembly 79-3066 rev 1 6/15/2007 Install lube with regulator and scavenge pump A72-3296 12/6/1989 NA. Remove from service defective #1 bearings installed some engines. A72-3371 12/6/1989 NA. Remove suspect first stage LPT disc A72-3624 3/14/98 One time oil and filter resample A72-3636 10/8/1998 Review engine log book for specific HP impellers A76-3065 4/30/2007 Installation of N1 DEEC A76-3079 4/30/2007 Replacement of specific N1 DEECs NA PN A76-3080 4/30/2007 Replacement of specific N1 DEECs NA PN A77-3020 6/26/1990 NA by mfg date 731-72-3764 AD NO. EFF #1 ENG #2 ENG DATE AND METHOD OF COMPLIANCE 89-22-16 10/25/1989 11/01/1989 NA per SB TFE731-76-3049 90-24-06 10/13/1990 12/11/1990 NA per SB TFE 731-A77-3020 98-17-01 10/29/1999 10/7/1998 No applicable airworthiness directives through issue 98-17-01 2000-15-09 10/10/2000 06/15/2007 CW removal & inspection of HPC impeller SB A72- 3641 2005-05-15 4/18/2005 9/2/2011 9/2/2011 NA PN by SIL pub# D201104000055 2008-02-19 03/06/2008 02/06/2008 NA PN not installed per SB 72-3720 2010-02-19 04/10/2010 04/26/2010 NA PN not installed per SB 72-A3748 & 72-A3749 LIFE LIMITED PART LOG ASSY NAME NOZZLE ASSY LPT 1 PN 307521-4 SN 3075271-4 LIFE LMTD PART NAME SUPPORT SEAL (POST SBP TFE0631) PN 3074052-2 SN 061756501904 DATE ON POS TIME ON PART AT INSTALL TOTAL TIME ON PART REMARKS CYCLES HOURS CYCLES HOURS
- 275. 4/27/2007 1 00 0 0
- 276. A/C MAKE: HawkerDATE:3/18/11 L/H ENG TSN: 6,636.9 A/C MODEL: 800 W/O: MX-652L/H ENG CSN: 4,668 A/C SN:2581XX ACTT: 6,874.4R/H ENG TSN: 6,819.4 A/C REG:NXXGS LNDS: 4,800 R/H ENG CSN: 4,771 1) Complied with 800 Hour B1, B2, B3, B4, B5, B6, B7, B8, B9, B10, B11, B12 and 24 Month F1, F2, F3, F4, F5, F6, F7, F8, F9, F10, F11 and F12 Inspections in accordance with Hawker 800 Aircraft Flexible Maintenance Schedule. 2) Complied with 5 Year Overhaul of APU Fire Bottle. Removed APU Fire Bottle P/N 30402104 S/N 20376B2 and reinstalled same after O/H by CRS NV2R045L (W.O. WO6530). Bottle installed with original squibbs dated 11/05. 3) Complied with No. 1 Oxygen Bottle 5 Year Overhaul. Removed No. 1 Oxygen Bottle Assembly P/N WKA37447 S/N 14510X with Valve P/N WKA31424 S/N 162 and reinstalled same after bottle inspection and valve O/H by CRS NV2R045L (W.O. WO6404 & WO6405). Serviced bottle with oxygen, leak check good. 4) Complied with No. 2 Oxygen Bottle 5 Year Overhaul. Removed No. 2 Oxygen Bottle Assembly P/N WKA37447 S/N 560655 with Valve P/N WKA31424 S/N 1143 and reinstalled same after bottle inspection and valve O/H by CRS NV2R045L (W.O. WO6402 & WO6403). Serviced bottle with oxygen, leak check good. 5) Complied with 2 Year Inspection of the L/H and R/H Wing Leading Edges in accordance with Hawker 800 Flexible Maintenance Schedule Part 3 item 570027. Performed aircraft stall flight with no stall characteristic defects noted. 6) Complied with Hawker Beechcraft Mandatory Service Bulletin 33-3682, Titled Lights - Reactivation Of Precise Flight Pulselight System, Rev 1, dated March 2010, Fix D and Fix E. Installed kits per SB instructions. Pulselight system ops check good. 7) Complied with 4 Year Lubrication of the L/H and R/H Elevator Trim Tab Connecting Rods in accordance with Hawker 800 Flexible Maintenance Schedule Part 3 item 550008. 8) Complied with 5 Year Test of the APU Fuel Pump Enclosure Fire Warning Switch. Removed switch P/N 17343-62 NSN and reinstalled same after inspection by CRS JGVR194F (W.O. 0JP2A). Note: CRS JGVR194F assigned tracking number 5309DA to this unit. 9) Complied with 5 Year Test of the APU Lower Fire Warning Switch. Removed switch P/N 160275-1 S/N 144606 and reinstalled same after inspection by CRS JGVR194F (W.O. 0JP2C). 10) Complied with 5 Year Test of the APU Generator Overheat Switch. Removed switch P/N 67100-1-350F NSN and reinstalled same after inspection by CRS JGVR194F (W.O. 0JP2B). Note: CRS JGVR194F assigned tracking number 5308DA to this unit. 11) Resealed NLG and both MLG struts. Replaced associated seals, o-rings and scraper rings with new. Serviced struts with hydraulic fluid and nitrogen. All three leak check good. 12) Removed Pilots Windshield P/N NF24016-385 NSN (S/N L171139) and installed repaired unit P/N NF24016-415 S/N L171139. Performed ground run, windshield leak check and ops check good. 13) Removed and replaced 4 ea main entrance door tensator motor springs with new units P/N N2441 DOT3. Door rig check and ops check good. 14) Removed and replaced L/H and R/H lower wing boost pump manhole panel and outboard manhole panel seals with new units P/N 25WS619. Leak check good. 15) Complied with 300 Hour Out Of Phase Item 210021, Inspect Air Conditioning Duct After Disturbance. No defects noted. 16) Complied with 2 Year Elevator Mass Balance Weight Inspection in accordance with Hawker 800 Flexible Maintenance Schedule Part 3, Item 550015. No defects noted. 17) Removed L/H MLG Door Aft Hinge P/N 25FC5803 NSN and replaced with new unit P/N 25FC5803 NSN. Performed gear swing, ops check good. 18) Repaired air tube leaks in the L/H #2, R/H #5 and R/H #6 TKS panels in accordance with T.K.S. LTD C.M.M.30-10-03, repair 3, assembly. Three panels worked leak check good. 19) Complied with gearbox pressure check on the No. 1 engine in accordance with Honeywell TFE731-5 L.M.M. 72-00-00. Max Accy = 10.0in/H2O, Max Fan = -2.5 psi, Max Xfer = 1.5 psi. No defects noted. 20) Removed and replaced garloc seal on the No.1 engine starter generator shaft with new unit P/N 3072784-2. Ran engine, leak check good. 21) Adjusted L/H inboard flap vane to obtain largest clearance between the flap vane and the torque shaft. Ran flaps, ops check good. Tech Sign: Cert: CRS-XZAR763L
- 277. I certify thatthis aircraft has been inspected in accordance with a 800 Hour B1, B2, B3, B4, B5, B6, B7, B8, B9, B10, B11, B12 and 24 Month F1, F2, F3, F4, F5, F6, F7, F8, F9, F10, F11 and F12 Inspections as required by FAR 91.409 (f) (3) and has been repaired in accordance with current Federal Aviation Regulations with respect to the maintenance performed and was determined to be in airworthy condition and has been approved for return to service. Insp Sign:Cert: CRS-XZAR763L MX Jet Service, Inc. 2000 Brett Road, New Castle, DE 19720 302-322-7757 -------------------------END------------------------- Go See additional maint notes on mx documented in Work Order MX-652 at MX JET SERVICE with parts change documented by 8130 records: Replaced Main Hydraulic system filter PN MFHA189/1A Replaced TKS Filter, PN 19295
- 278. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.7 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/22/2011 A/C 6875.7 4803 Total 2884.4 7452 INDEX NUMBER 140 EN 1 6638.2 4671 APU tach 4772.8 7444 1888.4 APU tach adj (-) EN 2 6820.7 4774 8 APU Cyc adj (+) COMPLETED 150-200 HOUR ENGINE AND 300-400 HOUR ENGINE INSPECTION PER HONEYWELL MM 72-00-00 INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES, AVTRAK TASK CODES 720005, 720011. RAN ENGINES, LEAK CKS OK. WORK PERFORMED IAW HONEYWELL AMM 79-20-03 AND 79-20-01. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. UPDATED AVTRAK SYSTEM RECORDS NEXT 150-200 HOUR ENGINE INSPECTION DUE AT 7075.7 AFTT. NEXT 300-400 HOUR ENGINE INSPECTION DUE AT 7275.7 AFTT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERT NO: A&P 3357851 GREGORY A. STULTZ
- 279. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG: AIRCRAFT TYPE AIRCRAFT SERIAL LH ENGINE SERIAL RH ENGINE SERIAL NXXGS BAe 125-800A 2581XX P91363 P91371 VER 2.7 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/11/2011 A/C 6884.7 4812 Total 2889.7 7463 INDEX NUMBER EN 1 6647.2 4680 APU tach 4772.8 7444 1888.4 APU tach adj (-) EN 2 6829.7 4783 8 APU Cyc adj (+) A/C MAKE: HawkerDATE: 4/11/11 A/C MODEL: 800 A/C SN: 2581XX ACTT: 6,884.7 A/C REG: NXXGS LNDS: 4,812 Log Book Entry Insert for the Aircraft identified above. 1. Complied with Raytheon Aircraft Repair Instruction Letter No. RIL-25-WF46, Issue 6, dated AUG 29, 1997, Titled: Rectification Of Inner Flap Vane Fouling On Torque Shaft to the L/H inboard flap vane. Replaced outboard attach plate per RIL instructions and adjusted vane to obtain required clearance. Ran flaps, ops check good. I certify that this aircraft has been repaired in accordance with current Federal Aviation Regulations with respect to the maintenance performed and was determined to be in airworthy condition and has been approved for return to service. Sign: Gerard VanDyk Cert:1565083 -------------------------END------------------------- UPDATED AVTRAK RECORDS.
- 280. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/24/2011 A/C 6899.3 4835 TSMOH 2898.3 7483 INDEX NUMBER 143 ENG 1 6661.8 4703 APU TACH 4786.7 7475 APU TACH ADJ (-) 1884.4 ENG 2 6844.3 4806 APU CYC ADJ (+) 8 DISCREPANCY: PBE (PROTECTIVE BREATHING EQUIPMENT) TIME CHANGE REQUIRED. CORRECTIVE ACTION: INSTALLED PBE MFGD SEPTEMBER, 2006, DUE FOR REPLACEMENT IN SEPTEMBER, 2016. PART PURCHASED FROM G.A. TELESIS, 1850 NW 49TH ST, FT. LAUDERDALE, FL 33309, 954-676-3111 NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF PBE PROTECTIVE BREATHING EQUIPMENT 802300-14 E06090375 802300-14 NSN AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 281. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/20/2011 A/C 6903.1 4839 TSMOH 2904.6 7493 INDEX NUMBER 144 ENG 1 6665.6 4707 APU TACH 4793 7485 APU TACH ADJ (-) 1884.4 ENG 2 6848.1 4810 APU CYC ADJ (+) 8 DISCREPANCY: CREW REPORTS #1 FMS CDU HARD TO READ IN DIRECT SUNLIGHT, DIM DISPLAY CANNOT BE BRIGHTENED WITH CONTROL. CORRECTIVE ACTION: INSTALLED OVERHAULED FMS CD-800 OBTAINED FROM HONEYWELL. UNIT OP CKS OK. UNIT OH’D ON 6/15/2011 BY HONEYWELL WICHITA, CRS# LV2R992K UNDER WO# 5004370969. DATA PLATE REFLECTS MODS A, B, C, D, E, F, G, H, J, K, L, M, N, P, R, S INCORPORATED. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 FMS CDU 7004403-902 86090164 7004403-902 92100390 AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 282. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/21/2011 A/C 6903.1 4839 TSMOH 2904.6 7493 INDEX NUMBER 145 ENG 1 6665.6 4707 APU TACH 4793 7485 APU TACH ADJ (-) 1884.4 ENG 2 6848.1 4810 APU CYC ADJ (+) 8 COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1 & #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4914 LANDINGS. REPLACED LH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS FOR NORMAL TIRE WEAR. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA1814 WW032 AHA1814 SL105 #2 MAIN WHEEL ASSY AHA1814 LC290 AHA1814 LR165 #1 TIRE GOODYEAR FLT EAGLE 237K23-2 03562955 237K23-2 00963011 #2 TIRE GOODYEAR FLT EAGLE 237K23-2 03562950 237K23-2 00963019 REMOVED TIRES HAD 149 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4289, DATED 1/28/2011. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 283. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/1/2011 A/C 6909 4846 TSMOH 2904.6 7493 INDEX NUMBER 146 ENG 1 6671.5 4714 APU TACH 4793 7485 APU TACH ADJ (-) 1884.4 ENG 2 6854 4817 APU CYC ADJ (+) 8 COMPLETED AFMS TASKS 320036.1 & 320036.2, CK OF #1 & #2 BRAKES FOR WEAR, NEXT DUE IN 75 CYCLES AT 4921 LANDINGS. REPLACED LH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS. #1 TIRE BLEW FUSE PLUG AFTER LANDING AT KMMU. REPLACED BOTH LH MLG WHEELS AND TIRES PER AMM 32-40-12-401. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA1814 LR165 AHA1814 WW032 #2 MAIN WHEEL ASSY AHA1814 SL105 AHA1814 LC290 #1 TIRE GOODYEAR FLT EAGLE 237K23-2 71412957 237K23-2 03562955 #2 TIRE GOODYEAR FLT EAGLE 237K23-2 11412977 237K23-2 03562950 REMOVED TIRES HAD 7 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4383, DATED 6/28/2011. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 284. 8375 Enterprise Ave.Philadelphia PA 19153 23 Aircraft Reg.: NXXGS Airframe Time: 6909.2 Aircraft S/N: 2581XX Airframe Cycles: 4846 1. REMOVED AND REPLACED THE LEFT MLG BRAKE MODULATOR WITH A SERVICEABLE UNIT FROM DUNCAN AVIATION CRS# JGVR194F IAW HAWKER 800 MM CH 32-40-00 OPERATIONAL AND LEAK CHECKS ARE GOOD. P/N ON: ACM22740 S/N ON: 50DM P/N OFF: ACM22740 S/N OFF: KW140 The aircraft and/or components identified above were repaired and inspected IAW FAA regulations and were found airworthy to return to service. Pertinent details of this repair are on file at this agency. Signature : Date 07/01/11 A & P 3328658 Print Name Jim Pacifico Work Order: 11AN62239 GO SEE NOTES: INSTALLED: 4 EA PLASTIC BACK UP RINGS BOTH MAXERET PN DAS2100-2, 2 EA. MODULATOR PACKING PN ACO321216, 4 EA. SEAL PN DAS2138-2, 3 EA. BRAKE MODULATOR RING PN DAS2119-4, 2 EA SEAL PN DAS2118-2, 2 EA. SEAL PN DAS2119-6
- 285. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/11/2011 A/C 6914.7 4850 TSMOH 2908.6 7501 INDEX NUMBER 147 ENG 1 6677.2 4718 APU TACH 4797 7493 APU TACH ADJ (-) 1884.4 ENG 2 6859.7 4821 APU CYC ADJ (+) 8 COMPLETED AVTRAK TASKS 335010, REPLACED AND CHECKED FWD AND AFT EMERGENCY EXIT POWER SUPPLY “D” CELL NI-CAD BATTERIES WITH NEW, 2 EACH PER BATTERY PACK, PN AD-4002P, NSN, BATCH NUMBER BA6189. BATTERIES OBTAINED FROM MFG’R, AREO DESIGN, INC, 385 INDUSTRIAL DR, MT. JULIET, TN, 37122, PH 800- 551-1158, PRODUCTION APPROVAL HOLDER No. (PAH#) PQ1465CE, WORK ORDER # 11-20960, DATED 6/23/2011. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LT NLG WHEEL AND TIRE ASSY AH52339 QA033 AH52339 DW061 RT NLG WHEEL AND TIRE ASSY AH52339 QG038 AH52339 149, 1045 REMOVED TIRES HAD 202 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4103, DATED 9/21/2010. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 286. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/13/2011 A/C 6915.9 4852 TSMOH 2915.7 7512 INDEX NUMBER 148 ENG 1 6678.4 4720 APU TACH 4804.1 7504 APU TACH ADJ (-) 1884.4 ENG 2 6860.9 4823 APU CYC ADJ (+) 8 REPLACED LH MLG INBD AND OUTBOARD BRAKE ASSEMBLIES PER AMM 32-40-114-401. OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 BRAKE UNIT AHA 1897 5001DW AHA 1288 LC378 #2 BRAKE UNIT AHA 1897 5006DW AHA1288 LS269 INSTALLED BRAKE ASSY’S OVERHAULED BY PRECISION ACCESSORIES & INSTRUMENTS, DIVISION OF PAG HOLDING CORP, 495 LAKE MIRROR RD, BLDG 800G, ATLANTA, GA 30349, CRS# ZV4R714M UNDER WO# 039578J FOR #1, DATED 4/20/2011 AND WO# 039148J FOR #2, DATED 4/1/2011. INSTALLATION OF NEW BRAKE ASSEMBLIES CHANGES THE AIRCRAFT MOD STATUS TO POST MOD 257668A. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 287. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/14/2011 A/C 6915.9 4852 TSMOH 2915.7 7512 INDEX NUMBER 149 ENG 1 6678.4 4720 APU TACH 4804.1 7504 APU TACH ADJ (-) 1884.4 ENG 2 6860.9 4823 APU CYC ADJ (+) 8 REPLACED AIRSHOW 400 DATA INTEGRATION UNIT FOR INTERMITTENT FAILURE. NEW UNIT OPS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF AIRSHOW 400 DIU 920050 1110 920050 1150 INSTALLED UNIT PURCHASED FROM DUNCAN AVIATION, OVERHAULED BY ENSAMBLADORES ELECTRONICOS, DE MEXICO S.DE R.L. DE C.V., AVE SIERRA SAN AGUSTIN #2498 COL PORVENIR, MEXICALI, B.C., MEXICO CP 21185, AIR AGENCY CERTIFICATE EASA. 145.0328 UNDER WO# R007845 DATED 12/4/2010 DATA PLATE REFLECTS INCORPORATION OF MODS F, G, H, J, K, M, N, P, R, T, U, V, Y, AD, AE. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 289. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/26/2011 A/C 6932.9 4864 TSMOH 2925 7525 INDEX NUMBER 150 ENG 1 6695.4 4732 APU TACH 4813.4 7517 APU TACH ADJ (-) 1884.4 ENG 2 6877.9 4835 APU CYC ADJ (+) 8 RESEARCHED AD 2011-14-08, EFFECTIVE 8/19/2011, B/E AEROSPACE CONTINUOUS FLOW PASSENGER OXYGEN MASK ASSY’S. AD NA BY PN, NOT INSTALLED ON THIS AC AT THIS TIME. CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 4920004. DRAINED AND SERVICED APU OIL WITH MOBIL 254. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 290. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/29/2011 A/C 6932.9 4864 TSMOH 2925 7525 INDEX NUMBER 151 ENG 1 6695.4 4732 APU TACH 4813.4 7517 APU TACH ADJ (-) 1884.4 ENG 2 6877.9 4835 APU CYC ADJ (+) 8 REPLACED LASERREF III IRU FOR INTERMITTENT 10+ MILE POSITION ERRORS. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF HONEYWELL LASERREF III IRU HG1075AE03 659 HG1075AE03 720 MODS INCORPORATED PER DATA PLATE: SER 2, 1,2,3,5,6,8,9,10,12,13 INSTALLED IRU REPAIRED BY HONEYWELL, 8840 EVERGREEN BLVD, MINNEAPOLIS, MN 55433-6040 CRS KE2R949K UNDER WO306976620, DATED 3/12/2011. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 291. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/2/2011 A/C 6946.9 4881 TSMOH 2937 7539 INDEX NUMBER 152 ENG 1 6709.4 4749 APU TACH 4825.4 7531 APU TACH ADJ (-) 1884.4 ENG 2 6891.9 4852 APU CYC ADJ (+) 8 RESEARCHED AD 2005-05-15, EFF 4/18/2005 AND FOUND TO BE NA TO #1 ENG SN P91363 AND #2 ENG SN P91371. NO FURTHER ACTION REQUIRED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 292. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/15/2011 A/C 6961.5 4893 TSMOH 2941.9 7555 INDEX NUMBER 153 ENG 1 6724 4761 APU TACH 4830.3 7547 APU TACH ADJ (-) 1884.4 ENG 2 6906.5 4864 APU CYC ADJ (+) 8 CW HAWKER BEECHCRAFT SB 78-4048, MODIFICATION OF TR ACCUMULATOR ASSY. OK FOR SERVICE. CW 200 HR LUBRICATION, AVTRAK TASK 050050. CW 200 HR/4 MO CAPACITY CHECK OF #1 AND #2 MAIN BATTERIES, BOTH CK OK FOR SERVICE. AVTRAK TASKS 241015 AND 241016 CW 24 MO INSPECTION OF PITOT/STATIC DRAIN TAPS, OK FOR SERVICE. AFMS TASK 340002 CW 300 HR INSPECTION OF RT STARTER GENERATOR, SN 3237. OK FOR SERVICE AFMS TASK 240001. CW 400 HR COOLING TURBINE INSPECTION. OK FOR SERVICE, AFMS TASK 210001. CW 400 HR WATER SEPARATOR INSPECTION, OK FOR SERVICE, AFMS TASK 210006. TWO OF FOUR LED LIGHT BARS IN LH NAV LIGHT ASSY INOP. REPLACED LH WINGLET LED NAV LIGHT ASSY, WHELEN MODEL 9028502, PN 01-0790285-02, OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF API LH LED NAV LIGHT ASSY H800-353-1 00146 H800-353-1 NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 293. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/27/2011 A/C 6973.6 4903 TSMOH 2946.1 7567 INDEX NUMBER 154 ENG 1 6736.1 4771 APU TACH 4834.5 7559 APU TACH ADJ (-) 1884.4 ENG 2 6918.6 4874 APU CYC ADJ (+) 8 CREW REPORTS INTERMITTENT FAILURE OF WEATHER RADAR TO SHOW SIGNIFICANT WEATHER. GROUND TEST FAILED WITH FAULT CODE 22 DISPLAYED. REPLACED HONEYWELL PRIMUS 870 RADAR TRANSMITTER ANTENNA ASSY; OP CKS OK PER HONEYWELL SYSTEM AND DESCRIPTION MANUAL 34-42-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RTA 7012640-922 92050963 7012640-922 88120185 PART OFF HAD 5939 HOURS AND 1687 CYCLES BEFORE FAILURE. INSTALLED UNIT MOD STATUS: A-L, N, R-Y REPAIRED UNIT OBTAINED FROM HONEYWELL, 8370 DOW CIRCLE, STRONGSVILLE, OH 44136, CRS# FGNR677K, UNDER WO# 5004524767 DATED 8/03/2011. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 294. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/11/2011 A/C 6982.1 4910 TSMOH 2949.2 7573 INDEX NUMBER 155 ENG 1 6744.6 4778 APU TACH 4837.6 7565 APU TACH ADJ (-) 1884.4 ENG 2 6927.1 4881 APU CYC ADJ (+) 8 REPEAT PROBLEM UPLOADING FMS DATA. REPLACED DL-900 DATA LOADER, OK FOR SERVICE. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF DL900 DATA LOADER 7016600-901 02022965 7016600-901 04033361 PART OFF HAD 149 HOURS AND 148 CYCLES BEFORE FAILURE. INSTALLED UNIT MOD STATUS: A-D. TESTED UNIT OBTAINED FROM HONEYWELL, 7227 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K, UNDER WO# 5004706967, DATED 10/03/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 295. StandardAero6201 West ImperialHighway Los Angeles, Ca. 90045 FAA Approved Repair Station, AN3R377L Airframe Log Entry Oct 18, 2011 Aircraft: H800 Registration no.: NXXGS Serial no.: 2581XX Total Time: 6991.2 Total Landings: 4917 1. Removed # 2 AHARS Computer Model AH-600 P/N: 7003360-943, S/N: 88121189 and installed repaired same part number Computer S/N: 00104520 per AMM 23-23-61. This Airframe was inspected in accordance with current Federal Aviation Regulation and is approved for return to service with respect to work performed on work order no. 283038. Signed: __________________________________________for StandardAero-LAX-CRS # AN3R377L
- 296. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/21/2011 A/C 6999.9 4921 TSMOH 2954.4 7585 INDEX NUMBER 156 ENG 1 6762.4 4789 APU TACH 4842.8 7577 APU TACH ADJ (-) 1884.4 ENG 2 6944.9 4892 APU CYC ADJ (+) 8 #1 COMM AUDIO HAS STATIC, ALSO ON SIDETONE DURING TRANSMIT. INSTALLED LOANER AUDIO CONTROL PANEL IN #1 POSITION AND REMOVED ORIGINAL UNIT FOR REPAIR. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF AV-850 AUDIO CONTROL PANEL 7511000-909 89070295 7511000-910 88020114 PART OFF WAS INSTALLED ON 5/19/1993 AND HAD 5179 HOURS AND 3878 CYCLES AT REPLACEMENT. INSTALLED UNIT MOD STATUS: A-C. REPAIRED LOANER UNIT OBTAINED FROM HONEYWELL, 8370 DOW CIRCLE, STRONGSVILLE, OH 44136, CRS# FGNR677K, UNDER WO# 5004457536, DATED 9/26/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 297. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/10/2011 A/C 7007.8 4931 TSMOH 2958.6 7569 INDEX NUMBER 157 ENG 1 6770.3 4799 APU TACH 4847 7561 APU TACH ADJ (-) 1884.4 ENG 2 6952.8 4902 APU CYC ADJ (+) 8 FMS DATA LOADER INOP. REPLACED DL-900 DATA LOADER, OK FOR SERVICE NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF DL900 DATA LOADER 7016600-901 98011164 7016600-901 02022965 PART OFF WAS INSTALLED ON 10/11/2011 AND FAILED AFTER ONE SUCCESSFUL DATA UPLOAD. INSTALLED UNIT MOD STATUS: A-D. REPAIRED UNIT OBTAINED FROM HONEYWELL, HANGAR 1 ANNEX, GULFSTREAM FACILITY TRAVIS FIELD, SAVANNAH, GA 31402-2206, CRS# LV2D992K, UNDER WO# 5004787653, DATED 10/27/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 298. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/16/2011 A/C 7009 4933 TSMOH 2959 7598 INDEX NUMBER 158 ENG 1 6771.5 4801 APU TACH 4847.4 7590 APU TACH ADJ (-) 1884.4 ENG 2 6954 4904 APU CYC ADJ (+) 8 REMOVED LOANER AUDIO CONTROL PANEL ON CAPTAINS SIDE AND INSTALLED UNIT OBTAINED FROM FIELDTECH AVIONICS AND INSTRUMENTS, INC, 4151 N. MAIN ST, FORT WORTH, TX 76106 PH: 817-625-2719. OK FOR SERVICE REPLACED FWD AND AFT APU FIRE BOTTLE SQUIBS IAW AMM 26-20-54-201 FOR TIME. NEW INSTALLED CARTRIDGES OBTAINED FROM HRD AERO SYSTEMS, 25555 AV STANFORD, VALENCIA, CA 91355, PH: 661- 295-0670. SQUIBS TEST OK. DOM 7/6/2011, REPLACEMENT DUE ON 7/6/2017. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF AV850 AUDIO CONTROL PANEL 7511000-910 88100196 7511000-909 89070295 AFT APU FIRE BOTTLE SQUIB M13083-5 23693 13083-5 ESD05L136-001 FWD APU FIRE BOTTLE SQUIB M13083-5 23706 13083-5 ESD05L136-001 INSTALLED AUDIO CONTROL UNIT REPAIRED BY DUNCAN AVIATION/LINCOLN, LINCOLN, NE, 68524, CRS# JGVR194F, UNDER WO# 10HHA, DATED 10/26/2011. INSTALLED FIRE BOTTLE CARTRIDGES MFG’D BY AMETEK, AMERON LLC DBA MASS SYSTEMS, 4750 LITTLEJOHN ST, BALDWIN PARK, CA 91706, PMA DMIR-NM602533, UNDER WO# 15174.6, DATED 7/6/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 299. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/21/2011 A/C 7009 4933 TSMOH 2959 7598 INDEX NUMBER 159 ENG 1 6771.5 4801 APU TACH 4847.4 7590 APU TACH ADJ (-) 1884.4 ENG 2 6954 4904 APU CYC ADJ (+) 8 NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #3 MAIN WHEEL ASSY AHA1814 WW032 AHA1814 XB003 #4 MAIN WHEEL ASSY AHA1814 LC290 AHA1814 XB007 #3 TIRE GOODYEAR FLT EAGLE 237K23-2 237K23-2 71412957 #4 TIRE GOODYEAR FLT EAGLE 237K23-2 237K23-2 11412977 REMOVED TIRES HAD 171 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4407, DATED 7/28/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 300. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/16/2011 A/C 7009 4933 TSMOH 2959 7598 INDEX NUMBER 160 ENG 1 6771.5 4801 APU TACH 4847.4 7590 APU TACH ADJ (-) 1884.4 ENG 2 6954 4904 APU CYC ADJ (+) 8 REPLACED #2 RCZ851 COMMUNICATIONS UNIT FOR TEST FAILURE AT POWER UP. INSTALLED UNIT OPS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RCZ-851 COMM UNIT 7510700-802 93030990 7510700-802 95061573 INSTALLED COMM UNIT REPAIRED BY HONEYWELL 8670 DOW CIRCLE, STRONGSVILLE OH 44136, CRS# FGNR677K, UNDER WO# 5004704807, DATED 11/17/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 301. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/13/2011 A/C 7018.1 4941 TSMOH 2978 7608 INDEX NUMBER 161 ENG 1 6780.6 4809 APU TACH 4866.4 7600 APU TACH ADJ (-) 1884.4 ENG 2 6963.1 4912 APU CYC ADJ (+) 8 COMPLETED 150-200 HOUR ENGINE INSPECTION, AVTRAK TASK CODE 720005, PER HONEYWELL MM 72-00- 00 INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES IAW HONEYWELL AMM 79-20-03 AND 79-20-01. RAN ENGINES, LEAK CKS OK. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. NEXT 150-200 HOUR ENGINE INSPECTION DUE AT 7218.1 AFTT. COMPLETED 150-200 HR TR INSPECTION, AVTRAK TASK 783003, 783004. COMPLETED LH AND RH WINGTIP NAV LIGHT LENSE INSPECTION, AVTRAK TASK 334001. COMPLETED LH AND RH WINGTIP STROBE LIGHT ASSEMBLIES INSPECTION, AVTRAK TASK 334002. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 AND #2 ENG OIL FILTERS 3070945-1 NSN 3070945-1 NSN UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 302. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/15/2011 A/C 7018 4941 TSMOH 2978 7608 INDEX NUMBER 162 ENG 1 6780.5 4809 APU TACH 4866.4 7600 APU TACH ADJ (-) 1884.4 ENG 2 6963 4912 APU CYC ADJ (+) 8 CAP CK’D CONCORDE RG-131 IRS BATTERY, S/N: 40273576, AVTRAK TASK 241030. NEXT DUE CAP CK 12/15/2012, REINSTALLED SAME. CAP CK’D CONCORDE RG-126 BATTERY IN #5 AUX POS, SN 40184860, AVRTAK TASK 241019. NEXT DUE CAP CK 12/15/2012, REINSTALLED SAME UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 303. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/16/2011 A/C 7022.8 4944 TSMOH 2980.4 7611 INDEX NUMBER 163 ENG 1 6785.3 4812 APU TACH 4868.8 7603 APU TACH ADJ (-) 1884.4 ENG 2 6967.8 4915 APU CYC ADJ (+) 8 CAP CK’D CONCORDE RG-126 BATTERY IN #4 AUX POS, SN 40413638, AVRTAK TASK 241018. NEXT DUE CAP CK 12/16/2012, REINSTALLED SAME #2 AHRS FAILED INTERMITTENTLY INFLIGHT. REPLACED #2 AHARS WITH UNIT FORMERLY IN #1 POSITION. REPLACEMENT UNIT INSTALLED IN #1 POSITION FOR MX CONVENIENCE. NOMENCLATURE POS P/N ON S/N ON P/N OFF S/N OFF AH-600 AHRS ATTITUDE HEADING REFERENCE UNIT #1 7003360-943 98054028 OFF A/C 4/4/12 7003360-943 97083876 AH-600 AHRS ATTITUDE HEADING REFERENCE UNIT #2 7003360-943 97083876 7003360-943 00104520 INSTALLED AHRS UNIT MODIFIED BY HONEYWELL 7227 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K, UNDER WO# 5004694164, DATED 12/8/2011. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 304. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/17/2011 A/C 7024 4946 TSMOH 2981.4 7613 INDEX NUMBER 164 ENG 1 6786.5 4814 APU TACH 4869.8 7605 APU TACH ADJ (-) 1884.4 ENG 2 6969 4917 APU CYC ADJ (+) 8 CAP CK’D CONCORDE RG-126 BATTERY IN #3 AUX POS, SN 40400072, AVRTAK TASK 241017. NEXT DUE CAP CK 12/17/2012, REINSTALLED SAME REPLACED LH AND RH RADIO ALTIMETER ANTENNAS FOR ABRASION WEAR ON EXPOSED LEADING EDGES. NOMENCLATURE POS P/N ON S/N ON P/N OFF S/N OFF AT-300 ANTENNA S67-2002-4 LH 7003586 552-16503 7003586 3817 AT-300 ANTENNA S67-2002-4 RH 7003586 552-16505 7003586 3818 INSTALLED ANTENNA UNITS BOTH NEW, MFG DATE OF 11/24/2008, MFG BY SENSOR SYSTEMS, INC, 8929 FULLBRIGHT AVE, CHATSWORTH, CA 91311 UNDER WO#503065 (BOTH) UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 305. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/19/2011 A/C 7024 4946 TSMOH 2981.4 7613 INDEX NUMBER 165 ENG 1 6786.5 4814 APU TACH 4869.8 7605 APU TACH ADJ (-) 1884.4 ENG 2 6969 4917 APU CYC ADJ (+) 8 REPLACED LH AFCS FGC FOR INTERMITTENT AUTOPILOT DISCONNECT. CREW’S FLIGHT FAULT SUMMARY POSTFLT DATA RECORD INDICATES #1 FLIGHT GUIDANCE COMPUTER INTERNAL FAULT. INSTALLED REPAIRED FZ-800 IN LH POSITION, PERFORMED GROUND TEST OF AFCS, CKS OK. NOMENCLATURE POS P/N ON S/N ON P/N OFF S/N OFF #1 FZ-800 FLT GUIDANCE COMPUTER LH 7003974-732 9003214 700374-732 87080925 INSTALLED UNIT OBTAINED FROM HONEYWELL, 7825 RIDGEPOINT DR, IRVING, TX 75063, CRS# TT1R518K, UNDER WO## 5004906277 DATED 12/16/2011. SERVICED AUX HYDRAULIC RESERVOIR. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 306. BANYAN AIR SERVICELOG ENTRY 12/29/2011 WO# 77907 HOURS 7032.8 LNDGS 4954 Description of Work Accomplished. Removed the Rockwell Collins 334D-6A Pitch Trim Servo ( ELEVATOR TRIM ) (P/N: 622-3260-001; S/N: 706) and replaced with an overhauled exchange unit (S/N: 778). Exchange unit was overhauled by CRS# NZ2R049L. System was ground tested and found to operate in accordance with the Honeywell SPZ-8000 Maintenance Manual, Chap. 22-14-00 Approval for Return to Service The article(s) identified above were repaired and inspected in accordance with current maintenance rules of the FAR’s under which the operator is certified and is approved for return to service as per those requirements. Pertinent details of the repair are on file at this agency under this work order. Authorized Signature: Jimmy Eyl, Chief Certification Engineer Hawker Beechcraft Authorized Service Center FAA Certificated Repair Station SD4R514M 5360 NW 20th Terrace Fort Lauderdale, Florida 33309 Phone 954 491 3170 Fax 954 491 1612 NOTES FROM INVOICE AUTOPILOT FAILED. TRIM HARD TO MOVE AT HIGHER ALTITUDES. REPLACE ELEVATOR TRIM MOTOR. -------------- APPLIED GROUND POWER AND PERFORMED AUTOPILOT TEST. SYSTEM SELF TEST PASSED. TESTED ELECTRIC PITCH TRIM. SYSTEM TESTED GOOD. PER CUSTOMER'S REQUEST, REMOVED AND REPLACED THE PITCH TRIM SERVO. REMOVED 334D-6A, P/N: 622-3260-001, S/N: 706 AND INSTALLED CUSTOMER SUPPLIED UNIT S/N: 778 OVERHAULED UNDER CRS# NZ2R049L. INSTALLED AND OPERATIONAL CHECKED IN ACCORDANCE WITH BAE-125-800 MAINTENANCE MANUAL 34-22-144. OPERATIONAL CHECKED GOOD. CONDUCTED TESTS FOR GROUND CHECK IN ACCORDANCE WITH THE HONEYWELL SPZ-8000 MAINTENANCE MANUAL 22-14-00. ALL CHECKED GOOD.
- 307. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/5/2012 A/C 7036.8 4957 TSMOH 2991.2 7625 INDEX NUMBER 166 ENG 1 6799.3 4825 APU TACH 4879.6 7617 APU TACH ADJ (-) 1884.4 ENG 2 6981.8 4928 APU CYC ADJ (+) 8 CW 300 HR INSPECTION OF RT STARTER GENERATOR, PN 23080-064 SN 2428. OK FOR SERVICE AFMS TASK 240001. CW 200 HR/4 MO CAPACITY CHECK OF #1 AND #2 MAIN BATTERIES, BOTH CK OK FOR SERVICE. AVTRAK TASKS 241015 AND 241016 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 308. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/1/2012 A/C 7045 4964 TSMOH 2994.4 7633 INDEX NUMBER 167 ENG 1 6807.5 4832 APU TACH 4882.8 7625 APU TACH ADJ (-) 1884.4 ENG 2 6990 4935 APU CYC ADJ (+) 8 REPLACED COCKPIT VOICE RECORDER UNDERWATER LOCATOR BEACON WITH FOR TIME. BATTERY EXPIRES JANUARY 2018. AVTRAK TASK 237015, BEACON BATTERY REPLACEMENT, TASK 237013, BEACON OVERHAUL, AND TASK 237013, BEACON BENCH CK ACCOMPLISHED. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF CVR UNDERWATER LOCATOR BEACON DK100 SC51056 DK100 DP6948 INSTALLED OVERHAULED UNIT OBTAINED FROM DUKANE SEACOM, 2900 DUKANE DR, ST. CHARLES, IL 60174, CRS# D3KR791J UNDER WO#01042012 DATED 1/4/2012 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 309. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/1/2012 A/C 7045 4964 TSMOH 2994.4 7633 INDEX NUMBER 168 ENG 1 6807.5 4832 APU TACH 4882.8 7625 APU TACH ADJ (-) 1884.4 ENG 2 6990 4935 APU CYC ADJ (+) 8 REPLACED LH "B" SCREEN WINDOW FOR DELAMINATING PROBLEM PER AMM 56-10-22-401 WITH NEW PART. POST INSTALL CKS OK. AVTRAK TASK 5610504 NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF WINDSCREEN, LH NH24016-91 ISSUE 2 L383230 NH24016-91 L338136 INSTALLED UNIT OBTAINED FROM ELLIOTT AVIATION, PART MFG'D BY AEROSPACE COMPOSITE TECHNOLOGIES LIMITED, LONDON LUTON AIRPORT, LUTON, BEDFORDSHIRE, LU2 9PQ ENGLAND DOM 7/20/2011. 8130 FROM HAWKER BEECHCRAFT WO# 0000025588-000180, DATED 9/15/2011. REMOVED WINDOW INSTALLED 9/30/2003. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 310. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/1/2012 A/C 7045 4964 TSMOH 2994.4 7633 INDEX NUMBER 169 ENG 1 6807.5 4832 APU TACH 4882.8 7625 APU TACH ADJ (-) 1884.4 ENG 2 6990 4935 APU CYC ADJ (+) 8 CW 600 HR INSPECTION OF APU STARTER GENERATOR, PN 23076-005, SN 5768, OK FOR SERVICE, AVTRAK TASK 240025. CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION, AVTRAK TASK 492001. CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE, AVTRAK TASK 492002. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 311. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/3/2012 A/C 7046.3 4966 TSMOH 2994.4 7633 INDEX NUMBER 170 ENG 1 6808.8 4834 APU TACH 4882.8 7625 APU TACH ADJ (-) 1884.4 ENG 2 6991.3 4937 APU CYC ADJ (+) 8 RELAMPED LOWER BEACON, PN ON 34-0226010-91. OP CKS OK. REPLACED RH ENG STARTER GENERATOR PER AMM 24-30-21-401 FOR TIME. OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #2 STARTER GENERATOR 23080-064 6949 23080-005 3237 UNIT ON OVERHAULED BY DUNCAN AVIATION, LINCOLN AIRPORT, LINCOLN NE 68524 CRS# JGVR194F UNDER WO# 04R1A DATED 9/25/2010. UPDATED AVTRAK TASKS 240001.2, 243006 AND 243011. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 312. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/6/2012 A/C 7046.3 4966 TSMOH 2994.4 7633 INDEX NUMBER 171 ENG 1 6808.8 4834 APU TACH 4882.8 7625 APU TACH ADJ (-) 1884.4 ENG 2 6991.3 4937 APU CYC ADJ (+) 8 CW "E" INSPECTION, AVTRAK TASK 050520 CW ELT INSPECTION PER FAR 91-207, AVTRAK TASK 256000 CW AIRFRAME PORTION OF RVSM COMPLIANCE INSPECTION, AVTRAK TASKS 340005, 340005.1, 340009 AND 3400019. RED EAGLE AVIONICS PERFORMED PITOT-STATIC SYSTEM AND TRANSPONDER PORTION OF 24 MO RVSM CERTIFICATION. UPDATED AVTRAK RECORDS. Red Eagle Avionics Date: 2/6/12 W/O: 8353 Registration: NXXGS TT: 7046.3 LDG: 4966 Performed pitot/static system and transponder portion of 24-month RVSM certification on the following equipment: #1 AZ-810 ADC (P/N: 7000700-668, S/N: 880912843) #2 AZ-810 ADC (P/N: 7000700-668, S/N: 88123056) Standby Altimeter (P/N: WL1605AM2, S/N: AF125) #1 Transponder (P/N: 7510700-802, S/N: 88100192) #2 Transponder (P/N: 7510700-802, S/N: 95061573) Testing was performed in accordance with the following Federal Aviation Regulations and Manufacturer’s Specifications: FAR 43, Appendix E, Paragraph (b) as required by FAR 91.411; FAR 43, Appendix F as required by FAR 91.413; and Hawker AMM V1-V2, Rev. 53, dated March 2009, 34-10-17-501, pages 4-7, Step 3: Functionally Test The Air Data System, A. Procedure, Action (1)-(13). Systems ground checked good. Aircraft is approved for return to service with regard to the work performed. ______________________________________ Dave Gregg Red Eagle Avionics, LLC - CRS #: EHER536D ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 313. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/13/2012 A/C 7048.9 4970 TSMOH 2997.9 7641 INDEX NUMBER 172 ENG 1 6811.4 4838 APU TACH 4886.3 7633 APU TACH ADJ (-) 1884.4 ENG 2 6993.9 4941 APU CYC ADJ (+) 8 DETERMINED AD AIRWORTHINESS DIRECTIVE (AD) 2011-21-08, EFFECTIVE NOVEMBER 23, 2011, IS NA TO THIS AIRCRAFT. THIS AD APPLIES TO SICMA AERO SEAT 88XX, 89XX, 90XX, 91XX, 92XX, 93XX, 95XX, AND 96XX SERIES PASSENGER SEAT ASSEMBLIES THAT ARE NOT CURRENTLY INSTALLED ON THIS AIRCRAFT. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 314. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/21/2012 A/C 7057.3 4977 TSMOH 3001.4 7649 INDEX NUMBER 173 ENG 1 6819.8 4845 APU TACH 4889.8 7641 APU TACH ADJ (-) 1884.4 ENG 2 7002.3 4948 APU CYC ADJ (+) 8 REPLACED APU STARTER GENERATOR PER AMM 24-30-21-401 FOR TIME. OP CKS OK. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF APU STARTER GENERATOR 23080-005 3237 23080-005 5768 PART ON MOD STATUS: C, D, E, K UNIT ON OVERHAULED BY DUNCAN AVIATION, LINCOLN AIRPORT, LINCOLN NE 68524 CRS# JGVR194F UNDER WO# 18QNA DATED 2/13/2012. PART OFF HAD 957.7 HOURS AND 1643 CYCLES AT REPLACEMENT UPDATED AVTRAK TASKS 2400025, 243007 AND 243009. SERVICED MAIN HYDRAULIC RESERVOIR AND ECU COOLING TURBINE OIL TO FULL. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 315. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/24/2012 A/C 7057.3 4977 TSMOH 3001.4 7649 INDEX NUMBER 174 ENG 1 6819.8 4845 APU TACH 4889.8 7641 APU TACH ADJ (-) 1884.4 ENG 2 7002.3 4948 APU CYC ADJ (+) 8 REPLACED CRACKED RH WING LANDING LIGHT LENS WITH NEW. RELAMPED LANDING AND TAXI LIGHTS, OP CKS OK. REPLACED TRANSPARENT PANEL RETAINING STRIP BOLTS WITH NEW. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF LAMP BAY WINDOW 251W00129-2 PPA22324 251W00129-2 PPA3172 LANDING LIGHT GE 4581 TAXI LIGHT GE 4594 LANDING LITE FRAME SCREWS (NICKEL CHROME FINISH) DHS1421-1-1/2D RH LANDING LIGHT LENS OBTAINED FROM ONTIC BBA AVIATION (ARNONI), 4150 N. SAM HOUSTON E. PKWY, HOUSTON, TX 77032 PH 281-590-1431. PART MFG'D BY HAWKER BEECHCRAFT, UNDER WO#0001826570- 000010 DATED 1/18/2011. OLD WINDOW HAD 1307 HRS AND 1102 CYCLES AT FAILURE. UPDATED AVTRAK TASK 5700002. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 316. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/26/2012 A/C 7062 4980 TSMOH 3001.4 7651 INDEX NUMBER 175 ENG 1 6824.5 4848 APU TACH 4889.8 7643 APU TACH ADJ (-) 1884.4 ENG 2 7007 4951 APU CYC ADJ (+) 8 CW AIRWORTHINESS DIRECTIVE ( AD ) 74-08-09 R3, REINSPECTION OF LAVATORY RECEPTACLES AND PLACARDS. NEXT DUE IN 1000 HOURS. CW HAWKER BEECHCRAFT MANDATORY SB 32-3962, R3. NO FURTHER ACTION REQUIRED. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 317. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/4/2012 A/C 7087.6 4995 TSMOH 3011.9 7971 INDEX NUMBER 176 ENG 1 6850.1 4863 APU TACH 4900.3 7963 APU TACH ADJ (-) 1884.4 ENG 2 7032.6 4966 APU CYC ADJ (+) 8 FIRST OFFICER, RH “A” SCREEN WINDSHIELD OVERHEATS. REMOVED OLD "A" WINDSHIELD AND INSTALLED NEW RH WINDSCREEN PER AMM 56-10-11, OP CHECKS OK. LH PFD AND MFD DATA INFORMATION LOST AS A RESULT OF AHARS #1 FAILURE INFLIGHT. SYSTEM PLACED IN REVERSION MODE FOR ONE MINUTE AND RETURNED TO NORMAL. REMOVED AND REPLACED LH AHARS UNIT, OP CKS OK NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF PANEL ASSY "A" WINDSCREEN RH SIDE Window NF24016-416 L396830 NF24016-416 L323412 #1 AH-600 ATTITUDE HEADING REFERENCE UNIT AHRS 7003360-943 99064271 7003360-943 98054028 NEW RH WINDSCREEN PANEL ASSY OBTAINED FROM GLOBAL PARTS INC., 901 INDUSTRIAL RD, AUGUSTA, KS 67010, PH: 316.733.9240 PART MFG'D BY HAWKER BEECHCRAFT, UNDER WO# 0000110465-000010 DATED 4/2/2012. OLD WINDOW HAD 1124 HRS AND 964 CYCLES AT FAILURE. REPAIRED AHARS UNIT OBTAINED FROM HONEYWELL , 7227 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K UNDER WO# 5005005247 DATED 4/2/2012. OLD AHARS HAD 64.8 HRS AND 60 CYCLES AT FAILURE. UPDATED AVTRAK TASK 561053 FOR RH "A" SCREEN AND TASK 3460521 FOR #1 AHARS REPLACEMENT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 318. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/12/2012 A/C 7093.6 4999 TSMOH 3016.3 7678 INDEX NUMBER 177 ENG 1 6856.1 4867 APU TACH 4904.7 7670 APU TACH ADJ (-) 1884.4 ENG 2 7038.6 4970 APU CYC ADJ (+) 8 REPLACED LH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS PER AMM 32-40-12-401. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 MAIN WHEEL ASSY AHA1814 XB003 AHA1814 LR165 #2 MAIN WHEEL ASSY AHA1814 XB007 AHA1814 SL105 #1 TIRE GOODYEAR FLT EAGLE 237K23-2 10182962 237K23-2 71412957 #2 TIRE GOODYEAR FLT EAGLE 237K23-2 11332977 237K23-2 11412977 INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT #2, NORTH ROYALTON, OH 44133, CRS L5NR1270 UNDER WO 4548, DATED 2/13/12. OLD TIRES HAD 153 LANDINGS AT TIRE CHANGE. UPDATED AVTRAK TASK 3200005 & 3200006 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 319. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/17/2012 A/C 7093.6 4999 TSMOH 3016.3 7678 INDEX NUMBER 177 ENG 1 6856.1 4867 APU TACH 4904.7 7670 APU TACH ADJ (-) 1884.4 ENG 2 7038.6 4970 APU CYC ADJ (+) 8 COMPLETED AFMS TASK 783003, 150 TO 200 HOUR THRUST REVERSER INSPECTION, LT ENGINE. NEXT DUE IN 200 HOURS AT 7293 AFTT. COMPLETED AFMS TASK 783004, 150 TO 200 HOUR THRUST REVERSER INSPECTION, RT ENGINE. NEXT DUE IN 200 HOURS AT 7293 AFTT. COMPLETED AFMS TASK 783007, 300 TO 400 HOUR THRUST REVERSER INSPECTION, LT ENGINE. NEXT DUE IN 400 HOURS AT 7493 AFTT COMPLETED AFMS TASK 783008, 300 TO 400 HOUR THRUST REVERSER INSPECTION, RT ENGINE. NEXT DUE IN 400 HOURS AT 7493 AFTT. COMPLETED AFMS TASK 783011, 600 TO 800 HOUR THRUST REVERSER INSPECTION, LT ENGINE. NEXT DUE IN 800 HOURS AT 7893 AFTT. COMPLETED AFMS TASK 783012, 600 TO 800 HOUR THRUST REVERSER INSPECTION, RT ENGINE. NEXT DUE IN 800 HOURS AT 7893 AFTT. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 320. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/20/2012 A/C 7093.6 4999 TSMOH 3016.3 7678 INDEX NUMBER 178 ENG 1 6856.1 4867 APU TACH 4904.7 7670 APU TACH ADJ (-) 1884.4 ENG 2 7038.6 4970 APU CYC ADJ (+) 8 COMPLETED 1000 HR/ 6 MONTH INSPECTION AND CAPACITY TEST / RECHARGE ON MAIN BATTERY SN 40383367, REINSTALLED IN #2 POSITION, AVTRAK TASK 241015, IAW CONCORDE CMM 24-30-71, REV L, DATED 3/11/2011. CKS OK, NEXT DUE CAP CHECK 10/20/2012. COMPLETED 1000 HR/ 6 MONTH INSPECTION AND CAPACITY TEST / RECHARGE ON MAIN BATTERY SN 40383366, REINSTALLED IN #1 POSITION, AVTRAK TASK 241016, IAW CONCORDE CMM 24-30-71, REV L, DATED 3/11/2011. CKS OK, NEXT DUE CAP CHECK 10/20/2012. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 BATTERY RG-390E 40383366 RG-390E 40383367 #2 BATTERY RG-390E 40383367 RG-390E 40383366 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ ● Jet East Corporate Aviation, LLC ● CRSJ21R713Y ● TRENTON-MERCER AIRPORT ● TRENTON, NJ 08628 ● Phone (215)-937-9020 ● Fax (609)-600-1718 REG # NXXGS DATE: 4/25/12 MAKE: Honeywell W/O #: 12AN43487 MODEL TFE731-5 TIME: 7045.4 RIGHT ENGINE LOG S/N: P-91371 CYCLES: 4975 Removed and replaced #2 engine computer assembly. Ops check good I/A/W Honeywell TFE731-5 MM CH 76-10-03. Removed P/N 2119010 S/N 126-BY0861 Installed ( DEEC ) P/N 2119010-8000 S/N 87-BY0921 I certify that this engine or component has been repair and inspected and determined to be in airworthy condition and return to service. Pertinent details of the inspection are on file at this agency under the work number shown above. Signed Philip Knorr A&P 3112480 Jet East Corporate Aviation
- 321. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/12/2012 A/C 7100.4 5004 TSMOH 3017.3 7682 INDEX NUMBER 179 ENG 1 6862.9 4872 APU TACH 4905.7 7674 APU TACH ADJ (-) 1884.4 ENG 2 7045.4 4975 APU CYC ADJ (+) 8 CREW REPORTS INTERMITTENT FAILURE OF WEATHER RADAR. REPLACED HONEYWELL PRIMUS 870 RADAR TRANSMITTER ANTENNA ASSY; OP CKS OK PER HONEYWELL SYSTEM AND DESCRIPTION MANUAL 34-42-12. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF RTA 7012640-922 960111560 7012640-922 92050963 PART OFF HAD 126.8 HOURS AND 101 CYCLES BEFORE FAILURE. INSTALLED UNIT MOD STATUS: A-L, N, R-Y REPAIRED UNIT OBTAINED FROM HONEYWELL, 7227 W. HARRY, WICHITA KS 67209, CRS# LV2R99K, UNDER WO# 5004861242 DATED 12/07/2011. AVTRACK TASKS 3460565 AND 3460566 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 322. Date: 6/08/2012; Aircraft:NXXGS ; Type: HAWKER 800A; S/N: NA04XX; Work Done At - Airframe Time: 7114.80,, Engine Time: 6877.30,, Engine Cycles: 4885,, L/G Cycles: 5017, REMOVED LEFT AND RIGHT ELEVATORS AND TRIM TAB ACTUATORS. DISASSEMBLED ACTUATORS, CLEANED OUT OLD GREASE, AND REASSEMBLED WITH AEROSHELL 22. REINSTALLED ELEVATORS. TRAVEL AND CLEARANCE CHECKED GOOD. FREED UP AND REMOVED PIVOT BOLT, CLEANED AND INSPECTED. REMOVED BEARING FROM PIVOT BLOCK, INSTALLED NEW BEARING AND REASSEMBLED. DRILLED OUT AND REMOVED OLD MOUNTING HARDWARE, REINSTALLED NEW HARDWARE ON LEFT ELEVATOR OUTBOARD HINGE PIVOT BLOCK FOR BEARING. REMOVED CORROSION ON LEFT AND RIGHT ELEVATOR TRIM ACTUATOR HOUSINGS AND DRAIN HOLES. TREATED AND PAINTED WITH EPOXY PRIMER. REMOVED, FABRICATED AND INSTALLED NEW BONDING WIRE ON LEFT ELEVATOR OUTBOARD HINGE. REMOVED AND REPLACED SEVERAL TAIL BULLET FAIRING SCREWS. The aircraft, aircraft engine, or appliance identified above was repaired and/or inspected in accordance with current maintenance rules of the Federal Aviation Regulations and is approved for return to service for the work performed. Pertinent details of the repair are on file at this repair station under WORK ORDER #12-0215. Signed CRS#XR5R175Y
- 323. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/15/2012 A/C 7118.5 5022 TSMOH 3034.2 7711 INDEX NUMBER 180 ENG 1 6881 4890 APU TACH 4922.6 7703 APU TACH ADJ (-) 1884.4 ENG 2 7063.5 4993 APU CYC ADJ (+) 8 RESEARCHED APPLICABILITY OF MANDATORY HAWKER BEECH SB 35-4081. AFFECTED QUICK DON OXYGEN MASK ASSYS REFERENCED IN SB (BY SN) NOT INSTALLED AT THIS TIME ON THIS AIRCRAFT. NOMENCLATURE POSITION P/N ON S/N ON DATE ON EMERGENCY OXYGEN MASK CAPT MC10-14-124 58516 6/1/2010 EMERGENCY OXYGEN MASK FO MC10-14-124 63721 12/19/2008 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 324. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/3/2012 A/C 7135.6 5033 TSMOH 3042.8 7723 INDEX NUMBER 181 ENG 1 6898.1 4901 APU TACH 4931.2 7715 APU TACH ADJ (-) 1884.4 ENG 2 7080.6 5004 APU CYC ADJ (+) 8 RESEARCHED APPLICABILITY OF AIRWORTHINESS DIRECTIVE AD 2012-11-09, EFFECTIVE 8/10/2012; FOUND NOT APPLICABLE, LAVATORY OXYGEN GENERATORS REFERENCED IN AD NOT INSTALLED AT THIS TIME ON THE AIRCRAFT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 325. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/13/2012 A/C 7139.9 5039 TSMOH 3044.9 7729 INDEX NUMBER 182 ENG 1 6902.4 4907 APU TACH 4933.3 7721 APU TACH ADJ (-) 1884.4 ENG 2 7084.9 5010 APU CYC ADJ (+) 8 COMPLETED AVTRAK TASKS 335010 AND 335310.1, REPLACED AND CHECKED FWD AND AFT EMERGENCY EXIT POWER SUPPLY “D” CELL NI-CAD BATTERIES WITH NEW, 2 EACH PER BATTERY PACK, PN AD-4002P, NSN, BATCH NUMBER AAIC134. BATTERIES OBTAINED FROM MFG’R, AREO DESIGN, INC, 385 INDUSTRIAL DR, MT. JULIET, TN, 37122, PH 800- 551-1158, PRODUCTION APPROVAL HOLDER No. (PAH#) PQ1465CE, FORM TRACKING# STN00023701, DATED 7/10/2012. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 326. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/25/2012 A/C 7159.6 5050 TSMOH 3052.5 7743 INDEX NUMBER 183 ENG 1 6922.1 4918 APU TACH 4940.9 7735 APU TACH ADJ (-) 1884.4 ENG 2 7104.6 5021 APU CYC ADJ (+) 8 CREW REPORTS INTERMITTENT 20 AMP SPLIT BETWEEN LH GENERATOR (LOW) AND RH GENERATOR (HIGH). RAN BOTH ENGINES ON GROUND, COULD NOT DUPLICATE FAULT; VERIFIED COCKPIT INDICATION ACCURATE. INVESTIGATION SHOWS NO EVIDENCE OF LOOSE CONNECTIONS OR DAMAGED COMPONENTS. SWAPPED LH AND RH STARTER GENERATORS FOR TROUBLESHOOTING AND CW STARTER GENERATOR INSPECTION/CHECK PER AMM 24-30-21-401 AND 24-30-21-601, START/RAN BOTH ENGINES, OPS CK FOR SERVICE. AVTRACK TASKS 243005,243006,240001.1 & 240001.2 UPDATED. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF STARTER GENERATOR LH 23080-064 6949 23080-064 2428 STARTER GENERATOR RH 23080-064 2428 23080-064 6949 RESEARCHED AD 2012-14-15, EFFECTIVE 7/19/2012; NA BY PN, KGS200 MERCURY WAAS NOT INSTALLED ON THIS AIRCRAFT AT THIS TIME. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 327. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/28/2012 A/C 7159.6 5050 TSMOH 3052.5 7743 INDEX NUMBER 184 ENG 1 6922.1 4918 APU TACH 4940.9 7735 APU TACH ADJ (-) 1884.4 ENG 2 7104.6 5021 APU CYC ADJ (+) 8 CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 492004. CW APU BIENNIAL/1500 HR/3000 CYCLE MAINTENANCE AVTRAK TASK 492005. DRAINED AND SERVICED APU OIL WITH MOBIL 254. REPLACED APU OIL FILTER ELEMENT. CLEANED APU FUEL INLET FILTER PN 211-326. RAN APU, LEAK AND OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF APU OIL FILTER APU WF331667 NSN 179411 NSN CW AFMS TASK 050050 200 HR AND AFMS TASK 050790 400 HR LUBRICATIONS. CW AFMS TASK 050800 400 HOUR DETAILED WALK AROUND INSPECTION. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 328. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/31/2012 A/C 7161.9 5052 TSMOH 3054 7747 INDEX NUMBER 185 ENG 1 6924.4 4920 APU TACH 4942.4 7739 APU TACH ADJ (-) 1884.4 ENG 2 7106.9 5023 APU CYC ADJ (+) 8 CREW REPORTS RADAR FAILED. CONFIRMED HARD FAILURE, RTA UNIT DOES NOT OPERATE OR POWER UP, COOLING FAN DOES NOT RUN. REPLACED RECEIVER TRANSMITTER ANTENNA ASSY., OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF RADAR RTA 7012640-922 93021120 7012640-922 96111560 PART OFF HAD 61.5 HOURS AND 48 CYCLES BEFORE FAILURE. INSTALLED UNIT MOD STATUS: A-L, N, R-Y REPAIRED UNIT OBTAINED FROM HONEYWELL, 7227 W. HARRY, WICHITA KS 67209, CRS# LV2R99K, UNDER WO# 5004861241 DATED 07/13/2012. AVTRACK TASKS 3460565 AND 3460579 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 329. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/7/2012 A/C 7164.9 5056 TSMOH 3060 7756 INDEX NUMBER 186 ENG 1 6927.4 4924 APU TACH 4948.4 7748 APU TACH ADJ (-) 1884.4 ENG 2 7109.9 5027 APU CYC ADJ (+) 8 CREW REPORTS RADAR FAILED. REPLACED RECEIVER TRANSMITTER ANTENNA ASSY., OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF WU-870 RADAR RTA - 7012640-922 89020226 7012640-922 93021120 PART OFF HAD 4 HOURS AND 4 CYCLES BEFORE FAILURE. INSTALLED UNIT MOD STATUS: A-L, N, R-Y REPAIRED UNIT OBTAINED FROM HONEYWELL, 8370 DOW CIRCLE, STRONGSVILLE, OH 44136, CRS# FGNR677K, UNDER WO# 500473061 DATED 8/4/2012. AVTRACK TASK 3460565 UPDATED. COMPLETED 1000 HR/ 6 MONTH INSPECTION AND CAPACITY TEST / RECHARGE ON MAIN BATTERY SN 40383367, REINSTALLED IN #1 POSITION, AVTRAK TASK 241015, IAW CONCORDE CMM 24-30-71, REV L, DATED 3/11/2011. CKS OK, NEXT DUE CAP CHECK 2/7/2013. COMPLETED 1000 HR/ 6 MONTH INSPECTION AND CAPACITY TEST / RECHARGE ON MAIN BATTERY SN 40383366, REINSTALLED IN #2 POSITION, AVTRAK TASK 241016, IAW CONCORDE CMM 24-30-71, REV L, DATED 3/11/2011. CKS OK, NEXT DUE CAP CHECK 2/7/2013. NOMENCLATURE P/N ON S/N ON P/N OFF S/N OFF #1 BATTERY RG-390E 40383367 RG-390E 40383366 #2 BATTERY RG-390E 40383366 RG-390E 40383367 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 330. Aircraft Logbook Entry XXXPartners Inc. Work Order: 291419 Date: October 22 , 2012 Serial Number: 2581XX Tail Number: NXXGS Model: Hawker 800 ACTT: 7176.6 LNDS: 5068 Engine Position: 1 Engine S/N: P-91363 Engine TSN: 6939.1 Engine Cycles: 4936 Engine Position: 2 Engine S/N: P-91371 Engine TSN: 7121.6 Engine Cycles: 5039 APU APU S/N: 877641 APU TSN: 3066.0 APU CSN: 7769 2. C/W the following Maintenance Schedule Inspection items: 800 Hour “B1-B12” Manufacturer’s routine inspection. 1600 Hour “C1-C12” Manufacturer’s routine inspection. 12 Month “E1-E12” Manufacturer’s routine inspection. 24 Month “F1-F12” Manufacturer’s routine inspection. 48 Month “G” Manufacturer’s routine inspection. 783003, 783004, 783011, 783012, 783015, 783016 -200/400/800/1600 hour Thrust Reverser inspection Nordam TR5000 MM 78-30-00. 3. C/W the following MS Structural inspection requirements: 320032 8 Year/4 Year main landing gear fairing strut NDT. ( NTM 32-10-103) 510002 1000 flights-Front pressure bulkhead. Detail inspect. 510003 12 Year/4 Year flight compartment skin & window structure above windshields NDT. (NTM 53-10-105A) 510005 15-18Year/8 Year center fuselage structure below the floor NLG bay to frame 13 & 16 to 19 NDT. (NTM 53-10-108, 107, 108B & 109) 510006 15-18Year/8 Year structure below escape hatch frames 13 to 14. 510007 15-18Year/8 Year center fuselage structure below the floor frames 8 to 17 NDT. (NTM 53-10-106A) 510008 15-18Year/8 Year center fuselage structure below the floor frames 13 to 16 NDT. (NTM 53-10-108A) 510009 8 Year / 4 Year entry door surround. 510010 15-18Year/8 Year center fuselage structure above the floor inspection and NDT. (NTM 53-10-101, 102, 103A, 104 & 106) 520009 8 Year Escape Hatch-Detailed Inspection -internally and externally. 530001 8 Year / 4 Year skin exterior under the dorsal intake, forward of frame 19. 530002 8 Year/4 Year fuselage skin under wing to fuselage fairings. 530009 15-18Year/8 Year fuselage skin under ventral tank. 530010 15-18Year/8 Year Ventral fuel tank and tank access panels removed IAW AMM 28-10-15 530011 8 Year Left front face of rear pressure bulkhead [frame 19] 530012 8 Year right front face of rear pressure bulkhead [frame 19] 530018 2400 Hours Fuselage skin adjacent to cabin window cutouts. 550002 8 Year horizontal stabilizer front, rear spar, attachment fittings and elevator hinge brackets inspection. Applied CPC IAW AMM 55-13-00. 550003 15-18Year/8 Year vertical stabilizer detailed inspection. (NTM 55-30-101, 102 & 103) 550004 16-8 Year horizontal to vertical stabilizer attachments. 550005 24 Year / 8 Year horizontal stabilizer bond test. (NTM 55-10-104A) 550006 8 Year/4 Year elevators NDT. (NTM 55-20-101 & 102) 550007 4 Year elevator detailed inspection. 550008 4 Year elevator trim tabs connecting rods. 550009 4 Year rudder detailed inspection. 550010 4 Year rudder trim tab, servo tab connecting rods. 550011 8/4 Year rudder NDT. (NTM 55-40-101) 550012 15-18Year/8 Year horizontal stabilizer NDT. (NTM 55-10-101, 102, 103 & 105) 550014 8 Year rudder hinge brackets and attachments. 550015 2 Year elevator mass balance weights & spigots. 570007 8 Year/4 Year wing bottom skins and stringers inspection and NDT. (NTM 57-30-101) 570008 8 Year/4 Year main landing gear and sidestay attachment fittings. 570011 3900 Hour/8 Year wing front spar, forward face. Ref. Aviation Partners, Inc. ICA 570012 2300 Hour/4 Year wing rear spar rear face. Ref. Aviation Partners, Inc. ICA 570013 2400 Hour/4 Year airbrakes hinges detailed inspection. 570014 2400 Hour/4 Year aileron inspection and NDT. (NTM 57-50-107) 570015 2400 Hour/4 Year aileron detailed inspection. 570016 2400 Hour/4 Year aileron connecting rods, trim and servo tabs. 570017 2400 Hour/4 Year flaps and flap vanes inspection and NDT. (NTM 57-50-105,106) 570028 4 Year Wing Leading Edges 570029 3600 Hour/8 Year wing internal structure / fuel system non return valves in inner and outer wings. Ref. Aviation Partners, Inc. ICA 570030 4800 Hour/8 Year then every 4 Years aileron outboard hinge casting inspect and NDT. (NTM -Ref. API # SRH-09-003) 4. C/W the following MS Out of Phase inspection requirements: 300007 1 Month purge of the airplane ice protection system. 340013 36 Month Compass swing IAW 800 AMM 34-23-14. [Installed new Compass Card as required] 5. Addressed the following Airworthiness Directives and MFG Service Bulletins: AD 2012-11-09 Amendment 39-17072 “Chemical Oxygen Generators” is not applicable due to units not installed. AD 2012-17-01 Amendment 39-17164 “Goodyear Tires” is not applicable due to p/n not installed. Complied with AD 2012-02-08 Amendment 39-16931. Removed and reinstalled modified RT-910 TCAS II computer unit p/n 4066010-913 s/n 92081106, modified by ACSS Repair and Overhaul CRS# L3ZR029X / EASA 145.5441. MOD STATUS: ACH SB34-66
- 331. Complied withSB 32-4068 dated July, 2011 “Nose Landing Gear Dragstay Assembly Design Improvement” [dragstay p/n 258UN3-143A s/n DHL/DH/732] Reassembled with new roller p/n 140-818020-0001. Entry Continued on Next Page 1 of 4 Hawker 800A, S/N: 2581XX NXXGS Aircraft Log Book Entry Continued ACTT: 7176.6 Date: 10/22/2012 6. C/W the following MS Life Limited/Component Overhaul requirements and Tasks: 080005-Weighed Aircraft and Updated Flight Manual W&B Info 212015-60M, HP Duct-Overheat switches-Test in accordance with Kiddie Graviner 26-12-70 and Hawker 800 AMM 26-10-12. [2ea] 156D/05 (1) 323009-5000 Landings, Installed an overhauled L/H Main undercarriage Jack p/n AIR48502/7 s/n LK9008460, overhauled by APPH Wichita CRS# OU2R070L / EASA 145.5895 under W/O# 637984. Removed s/n LK8800820. 323010-5000 Landings, Installed an overhauled R/H Main undercarriage Jack p/n AIR48503/7 s/n LK0655, overhauled by APPH Wichita CRS# OU2R070L / EASA 145.5895 under W/O# 637984.Removed s/n LK8803594. 323011-5000 Landings, Installed an overhauled Nose undercarriage Jack assembly p/n AIR45404/1 s/n LK9302336, overhauled by APPH Wichita CRS# OU2R070L / EASA 145.5895 under W/O# 637984.Removed s/n unk. 323015-5000 Landings, Installed an overhauled L/H Main Gear Door Jack p/n AIR48485/3 s/n APB94940, overhauled by APPH Wichita CRS# OU2R070L / EASA 145.5895 under W/O# 636011. Removed s/n LK8800504. 323016-5000 Landings, Installed an overhauled R/H Main Gear Door Jack p/n AIR48484/3 s/n LK0562, overhauled by APPH Wichita CRS# OU2R070L / EASA 145.5895 under W/O# 636010. Removed s/n LK8802336. 334005.1-1500 Hr, Installed new L/H winglet tip strobe light assembly p/n 02-0250276-00. 334005.2-1500 Hr, Installed new R/H winglet tip strobe light assembly p/n 02-0250276-00. 340016-24M, Check static plates and Airframe surrounding structure IAW Hawker 800 AMM 34-11-29.[part of F3] 342561-24M, Inspect Under Upper and Lower TCAS Antenna {ICA Document #44504900}. 351008-6 Year, Overhaul-B/E Aerospace/Puritan Bennett Passenger. Installed 13ea. new passenger Observer/Cabin/Lav oxygen masks p/n C351-2000-205 [DOM: 01/2012]. IAW Hawker 800 AMM 35-20-31. 340001.1, 340002.1-24M Replace NZ-2000’s Battery-IAW Honeywell IM #A09-3642-002.Installed 2ea. new #1 and #2 FMS NZ-2000 batteries p/n 7020116-1. Next Due: 10/2014. 7. Installations with 337’s Installed new LoPresti Speed Merchants “Boom Beam” wing mounted Taxi / Landing light System with new LoPresti Speed Merchants “Boom Beam” Nose mounted HID light System in accordance with LoPresti Speed Merchants “STC STO2893AT” dated June 28, 2004, LoPresti Speed Merchants Installation Instructions LSM-500-042 Rev T dated 10-26-10, LSM-500-047 Rev K dated 12-9-10 and LoPresti Master Drawing List (MDL) No. 47 Rev. Q dated 05-21-12 or later FAA approved revision. Ref. FAA form 337 and Additional Equipment list/Weight and balance form dated 10/22/2012 for details. Landing/Taxi light kit P/N: LSM-500-042-2860 Nose Taxi light kit P/N: LSM-500-047-2860 Installed 2 ea. ECS USB charging outlets located in the cockpit on the respective pilot and copilot side facia panels and related electrical system in accordance with ECS assembly drawing number ECS-210210 and StandardAero electrical systems drawing number 1023231 rev A. Ref. FAA form 337 and Additional Equipment list/Weight and balance form dated 10/22/2012 for pertinent details. 8. Performed the following miscellaneous maintenance: 3300002-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45580. Removed s/n 39442. 3300550-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45097. Removed s/n 42063. 3300552-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45112. Removed s/n 42065. 3300560-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45659. Removed s/n 36930. 3300561-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45649. Removed s/n 36929 3300557-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45570. Removed s/n 42067. 3305011-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45107. Removed s/n 5323. 3305011.1-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45113. Removed s/n 35532. 3305013-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45111. Removed s/n 36928. 3350011-Installed new Cabin lighting power supply unit p/n AL-5112 s/n 45634. Removed s/n 14909. Installed new L/H flap outboard hinge bearing retaining ring p/n A50Y. Installed new NLG axle plate felts p/n 25UN107. Installed new L/H flap outboard hinge bolt p/n A112-12J. Installed new L/H and R/H flap inboard hinge bolts p/n A112-15G. Installed new R/H flap outboard hinge bolt p/n A112-12J. Installed 2ea. new L/H flap outboard driveshaft Gaitors p/n A9030. Installed 2ea. new R/H flap outboard driveshaft Gaitors p/n A9030. Installed new Dorsal fairing bolt p/n DHS1473-10 with nut p/n H51132-3K7. Installed new manhole panels [W311] seal p/n 25WS619. Installed 2ea. new L/H aileron cable pulleys p/n AS103.[L/H outboard flap well] Installed 3ea. new Rudder servo tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y. Installed 3ea. new Rudder Trim tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y. Installed new Rudder lower hinge mount bolt p/n 25TE241. Installed new Rudder servo tab center mount bolt p/n DHS1432-10E. Installed new Escape Hatch rain seal p/n 25FC7767-3. Installed new L/H Airbrake outboard upper hinge bolt p/n 25WS4253AB. Installed new L/H Airbrake outboard Lower hinge bolt p/n 25WS4253AB. Installed new L/H Airbrake inboard lower hinge bolt p/n A111-12G. Installed new R/H Airbrake outboard lower hinge bolt p/n 25WS4253AB.
- 332. Installed newR/H Airbrake inboard lower hinge bolt p/n A111-12G. Installed new R/H flap outboard hinge fairing bracket p/n 25-8WS2093-1A. Installed new R/H Airbrake outboard upper hinge bolt p/n 25WS4253AB. Installed 2ea. new L/H and R/H swing down panels camlocks p/n 1126000-4 Installed 2ea. new L/H and R/H swing down panel camlocs p/n 2600-5. Installed 2ea. new L/H and R/H swing down panel camlocs p/n 2600-7. Installed 4ea. new L/H and R/H swing down panel camlocs p/n 2600-6. Entry Continued on Next Page 2 of 4 Hawker 800A, S/N: 2581XX NXXGS Aircraft Log Book Entry Continued ACTT: 7176.6 Date: 10/22/2012 Performed the following miscellaneous maintenance Continued: Installed 10ea. new L/H and R/H swing down panel camlocs lock washers p/n 2600LW. Installed new NLG, Nose strut barrel p/n 25UN649 s/n WAL42983. Removed s/n UNK. Installed new NLG, axle retaining nut p/n 25UN119. Installed 3ea. new R/H elevator Trim tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y. Installed new R/H elevator center mount bearing hinge mount bolt p/n 25TE241. Installed new L/H Taxi light circuit breaker p/n MS26574-10. Installed new R/H aileron, trim tab inboard bearing p/n ZWDSP4SP1-G81. Installed new R/H aileron, center bearing attach bolt p/n 25-8WG43-1. Installed new R/H aileron, inboard mount bolt p/n 25-8WG25-1. Installed new L/H aileron, inboard mount bolt p/n 25-8WG25-1. Installed new L/H aileron, center bearing attach bolt p/n 25-8WG43-1. Installed 3ea. new L/H elevator, trim tab bearings p/n ZWDSP4SP1-G81 with new retainer P/N A29Y. Installed new L/H elevator, middle bearing attach bolt p/n 25TE241. Installed new L/H elevator center mount hinge bolt p/n DHS1473-11-1-2E. Installed new R/H wheel well hydraulic lines retaining plate p/n 25WS4081. Installed new Fwd closet, curtain hangar p/n T2. Installed 9ea. new aircraft static wicks p/n 10-900-53A-2. Installed new #1 engine LP bleed duct gasket p/n 3071235-1. Installed new #1 transponder coax [@ rack] right angle connector p/n CTR922. Installed new R/H [A] horizontal stab.-to-vertical stab. p/n 25-8GF55-1.IAW Hawker 800 SRM 55-10-41. Installed new L/H [A] horizontal stab.-to-vertical stab. p/n 25-8GF55-1.IAW Hawker 800 SRM 55-10-41. Installed new R/H [B] horizontal stab.-to-vertical stab. p/n 25-8GF63-1.IAW Hawker 800 SRM 55-10-41. Installed new L/H [B] horizontal stab.-to-vertical stab. p/n 25-8GF63-1.IAW Hawker 800 SRM 55-10-41. Installed new R/H [C] horizontal stab.-to-vertical stab. p/n 25-8GF57-1.IAW Hawker 800 SRM 55-10-41. Installed new L/H [C] horizontal stab.-to-vertical stab. p/n 25-8GFR128-1.IAW Hawker 800 SRM 55-10-41. Installed new R/H [D] horizontal stab.-to-vertical stab. p/n 25-8GF59-1.IAW Hawker 800 SRM 55-10-41. Installed new L/H [D] horizontal stab.-to-vertical stab. p/n 25-8GFR129-1.IAW Hawker 800 SRM 55-10-41. Installed new R/H [E] horizontal stab.-to-vertical stab. p/n 25-8GF61-1.IAW Hawker 800 SRM 55-10-41. Installed new L/H [E] horizontal stab.-to-vertical stab. p/n 25-8GF61-1.IAW Hawker 800 SRM 55-10-41. Installed new overfin-to-stinger seals p/n 25-8TF437-265. IAW Hawker 800 SRM 51-43-00. Adjusted rudder control cable tensions in accordance with Hawker 800 AMM 27-20-00. Adjusted rudder auto pilot servo cable tensions in accordance with Hawker 800 AMM 27-20-121. Adjusted airbrake cable tensions in accordance with Hawker 800 AMM 27-61-02. Adjusted aileron autopilot cable tensions in accordance with Hawker 800 AMM 27-10-93. Adjusted aileron trim cable tensions in accordance with Hawker 800 AMM 27-10-00. Adjusted aileron control cable tensions in accordance with Hawker 800 AMM 27-10-00. Adjusted crossfeed cable tensions in accordance with Hawker 800 AMM 28-20-83. Adjusted L/H and R/H HP cable tensions in accordance with Hawker 800 AMM 76-10-00. Adjusted L/H and R/H LP cable tensions in accordance with Hawker 800 AMM 28-20-83. Adjusted elevator servo cable tensions in accordance with Hawker 800 AMM 27-30-00. Resealed R/H wing fuel sump using PRC1422B1/2 in accordance with Hawker 800 AMM 20-00-00. Accomplished crack repair by weld process to the R/H Thrust Reverser stang panel, then prepped, epoxy primered and top coated as required. All work done IAW AC43.13-1B and Hawker 800 structural repair manual 54-10-31 and Hawker 800 AMM. Accomplished Repair to R/H MLG strut barrel per Hawker Siddeley Aviation Repair Drawing #: 25UM/R179 “Plunger Tube Main U/C, Lug Removal” dated 2/7/1976. Adjusted L/H and R/H main landing gear roller clearances in accordance with 800 AMM 32-10-25,401. Removed light surface corrosion from some areas of the L/H and R/H thrust Reverser afterbody, treated primed and painted IAW Hawker 800 AMM 20-10-3527 and 51-20-11. Removed and reinstalled L/H boost pump noise suppressor to remove light corrosion as required, then prepped, epoxy primered, applied top top coat-silver. All work done in accordance with 800 AMM 20-10-228. Removed light surface corrosion from some areas of the L/H and R/H wing leading edge lands, treated primed and painted IAW Hawker 800 SRM 51-43-00 and 51-73-00. Accomplished Securing of main entry door guide pin sleeves IAW Hawker 800 AMM 52-11-00. Accomplished painting of the NLG lower bearing assembly, retaining collar, and torque links, cleaned, treated and epoxy primed then painted [Matterhorn white] IAW Hawker 800 AMM 20-10-228.
- 333. Reglued Escapehatch seal in many area’s as required using 1300L in accordance with 52-20-00. Resealed nose landing gear strut assembly using the following new parts: 1ea. seal P/N: AIR45598, 1ea. seal P/N: 423000A, 1ea. seal P/N: 25UN523, 2ea. seals P/N: AIR45596, 2ea. seals P/N: AIR110410 and 1ea. seal P/N: DHS1650C. Serviced nose strut assembly as required. All work done in accordance with Hawker 800 CMM 32-20-30 and Hawker 800 AMM 12-32-00. Resealed L/H and R/H main landing gear strut assemblies using the following new parts: 4ea. seals P/N: AIR117292, 2ea. seal P/N: AIR46174, 2ea. seal P/N: 25- 6UM31, 2ea. seals P/N: 21UM495-9, 4ea. Delta seals P/N: S30948, 2ea. seal P/N: 100-240-1109, 2ea. seal DHS1650A and 2ea. seal P/N: DHS1650C. Serviced strut assemblies as required. All work done in accordance with Hawker 800 CMM 32-10-01 and Hawker 800 AMM 12-32-00. Removed corrosion from outboard L/H horizontal leading edge landing and repaired strap as needed in accordance with Hawker 800 Structural Repair Manual 51-24-11-001,51-25-00-001,51-31-00-001, 51-41-00-001,51-42-00-001,51-43-00-001,51-44-00-001.55-10-11-001 Fig.1,55-10-11-001. Entry Continued on Next Page 3 of 4 Hawker 800A, S/N: 2581XX NXXGS Aircraft Log Book Entry Continued ACTT: 7176.6 Date: 10/22/2012 Performed the following miscellaneous maintenance Continued: Accomplished crack Repair to the R/H Flap located inboard aft at trailing edge using flush patch/internal doublers, in accordance with Hawker 800 Structural Repair Manual “Flap skin Repairs Aft of Spar [pre-Mod. 253297]” 57-55-12-201 Sec.3.with Fig.203. Accomplished Repair to Cabin center aisle floor stringer @ FR.224 in accordance with Hawker 800 Structural Repair Manual “Fuselage Center Section Center Structure Repair Schemes” 53-20-11-201 Fig. 203. X-rays performed by Certified Inspection Service Inc. CRS #X18R997N on project # 18767. Removed and replaced various hardware, bonding jumpers, lamps, abrasion tape, sealant and paint as needed with new parts in accordance with Hawker 800 AMM. Details on file under StandardAero WO#: 291419. I certify this Aircraft has been inspected in accordance with a “B, C, E, F & G” inspection under FAR 91.409 F (3) and approved for return to service. Details under W/O# 291419 Date 10/22/2012 ACTT: 7176.6 Signed Thomas Styczynski for CRS# GW4R221M, Augusta, GA. 30906 4 of 4 SERVICE RECORD ENTRY XXX Partners Inc. Hawker 800 S/N: 2581XX Work Order Number: 291419 Date: 10/22/2012 ACTT: 7176.6 Ldgs: 5068 Engine Serial Number: P-91363 Position #1 Engine TSN: 6939.1 Engine CSN: 4936 1. 720005-Complied with 150 to 200 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o Analyze oil and filter. o Inspect chip detector for contamination. 2. 720011-Complied with 300 to 400 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o DEEC Bit Check o Electrical Wiring Connectors o Fan Rotor Assembly Blades o Fuel Heater Oil Tube o Fuel Nozzle Shrouds o Plumbing lines and connections 3. 730005-Complied with 600 to 800 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o Fuel Filter Element
- 334. 4. 720021-Complied with1000 to 1500 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o Igniter Plug and leads o Ignition System Installed 2ea. new Igniters p/n 3074541-4. Accomplished “Oil Change”. Drained Oil Tank, Accessory and Transfer Gearboxes and Serviced Oil Tank to Capacity with Mobil 254 Oil. Accomplished required operational and leak checks in accordance with Honeywell TFE731-5R Light Maintenance Manual. I certify this engine has been inspected in accordance with a 150-250/300-400/600-800/1000-1500 Hour inspection under FAR 91.409 (f) (3) and approved for return to service. Details on file under WO#: 291419. Date: 10/22/2012, Signed: Thomas Styczynski for CRS# GW4R221M, Augusta, GA. 30906 SERVICE RECORD ENTRY XXX Partners Inc. Hawker 800 S/N: 2581XX Work Order Number: 291419 Date: 10/22/2012 ACTT: 7176.6 Ldgs: 5068 Engine Serial Number: P-91371 Position #2 Engine TSN: 7121.6 Engine CSN: 5039 5. 720005-Complied with 150 to 200 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o Analyze oil and filter. o Inspect chip detector for contamination. 6. 720011-Complied with 300 to 400 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o DEEC Bit Check o Electrical Wiring Connectors o Fan Rotor Assembly Blades o Fuel Heater Oil Tube o Fuel Nozzle Shrouds o Plumbing lines and connections 7. 730005-Complied with 600 to 800 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o Fuel Filter Element 8. 720021-Complied with 1000 to 1500 Hour Inspection In Accordance with Honeywell TFE731-5R Light Maintenance Manual 72-00-00. o Igniter Plug and leads o Ignition System Installed 2ea. new Igniters p/n 3074541-4. Accomplished “Oil Change”. Drained Oil Tank, Accessory and Transfer Gearboxes and Serviced Oil Tank to Capacity with Mobil 254 Oil. Accomplished required operational and leak checks in accordance with Honeywell TFE731-5R Light Maintenance Manual. I certify this engine has been inspected in accordance with a 150-250/300-400/600-800/1000-1500 Hour inspection under FAR 91.409 (f) (3) and approved for return to service. Details on file under WO#: 291419. Date: 10/22/2012, Signed: Thomas Styczynski for CRS# GW4R221M, Augusta, GA. 30906 Weight and Balance Report 10/22/2012 BELOW Empty weight 16038.8
- 336. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/23/2012 A/C 7178.6 5070 TSMOH 3064.8 7774 INDEX NUMBER 187 ENG 1 6941.1 4938 APU TACH 4953.2 7766 APU TACH ADJ (-) 1884.4 ENG 2 7123.6 5041 APU CYC ADJ (+) 8 LOWER BEACON INOP. RELAMPED, NO HELP. BAD FLASHER UNIT. INSTALLED NEW LOWER BEACON UNIT, OP CKS OK. NEW LENS SEAL AND FLASHER UNIT SEAL ALSO INSTALLED. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF RED FLASHING ANTI- COLLISION UNIT LOWER 01-0790044-01 06543 01-0790044-03 01024 REPAIRED UNIT OBTAINED FROM DUNCAN AVIATION, 15745 SOUTH AIRPORT RD, BATTLE CREEK, MI 49015, AVIALL CERTIFICATE OF CONFORMANCE FOR PART DATED 5/14/08. AVTRACK TASK 3340002 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 337. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/5/2012 A/C 7187.6 5077 TSMOH 3068.6 7783 INDEX NUMBER 188 ENG 1 6950.1 4945 APU TACH 4957 7775 APU TACH ADJ (-) 1888.4 ENG 2 7132.6 5048 APU CYC ADJ (+) 8 LANDING LIGHT PULSE FEATURE INOP. REPLACED PULSE LIGHT CONTROL UNIT, SYSTEM OPS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF PULSE LITE CONTROLLER - 2401S AR01647 2400-25-4-4 K00482 NEW REPLACEMENT UNIT OBTAINED FROM PRECISE FLIGHT, INC. BEND OR 97708 TEL 541-382-8684. AVTRACK TASK 3340500 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 338. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/3/2012 A/C 7202.3 5087 TSMOH 3075.3 7796 INDEX NUMBER 189 ENG 1 6964.8 4955 APU TACH 4963.7 7788 APU TACH ADJ (-) 1888.4 ENG 2 7147.3 5058 APU CYC ADJ (+) 8 CAPTAIN'S PFD FAILED AFTER TAKEOFF. TEMPORARILY SWAPPED WITH CENTER MOUNTED MFD, PROBLEM FOLLOWS DISPLAY. REPLACED PFD UNIT. INSTALLED UNIT OPS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF DU-1080 PILOT PFD 7023460-02006 04030977 7023460-02006 06093737 SN 06093737 HAD 1314.3 HOURS AND 3814 CYCLES AT FAILURE. SERVICEABLE RENTAL/EXCHANGE UNIT OBTAINED FROM HONEYWELL 7227 W. HARRY, WICHITA KS 67209, CRS#LV2R992K, UNDER WO# 5004707229 DATED 10/8/2011. AVTRACK TASK 3460581 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 339. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/4/2012 A/C 7202.3 5087 TSMOH 3075.3 7796 INDEX NUMBER 190 ENG 1 6964.8 4955 APU TACH 4963.7 7788 APU TACH ADJ (-) 1888.4 ENG 2 7147.3 5058 APU CYC ADJ (+) 8 CREW REPORTS INTERMITTENT PROBLEM WITH CABIN TEMPERATURE CONTROL FUNCTION. REPLACED RELAY K18 IN LAVATORY COMPONENT PANEL. PART OBTAINED FROM ELECTRO ENTERPRISES INC, 3601 N I-35, PO BOX 11456, OKLAHOMA CITY, OK, 73136, PHONE 405-427-6591 OP CKS OK FROM CABIN AND COCKPIT. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF RELAY K18 - MHLO-12D- 26.5VDC NSN TRACE #598701 MHLO-12D- 26.5VDC NSN TRACE #204404 REPLACED RELAY HAD 598 HOURS AND 501 CYCLES BEFORE FAILURE. AVTRACK TASK 2420550 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 340. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/7/2013 A/C 7222.5 5099 TSMOH 3085.9 7810 INDEX NUMBER 191 ENG 1 6985 4967 APU TACH 4974.3 7802 APU TACH ADJ (-) 1888.4 ENG 2 7167.5 5070 APU CYC ADJ (+) 8 CAP CK’D CONCORDE RG-131 IRS BATTERY, S/N: 40273576, AVTRAK TASK# 241030. NEXT DUE CAP CK 1/8/2014, REINSTALLED SAME. REMOVED, INSPECTED, CAP CK’D AND RE-INSTALLED CONCORDE RG-126 AUXILIARY BATTERY SN 40413638 IN #3 POS, AVTRAK TASK# 241017, SN 40400072 IN #4 POS, AVTRAK TASK# 241018, SN 4018460 IN #5 POS, AVTRAK TASK# 241019. OK FOR SERVICE. NEXT DUE CAP CK 1/8/2014. REPLACED AIRSHOW 400 DATA INTEGRATION UNIT FOR INTERMITTENT FAILURE. NEW UNIT OPS OK. INSTALLED UNIT PURCHASED FROM DUNCAN AVIATION, REPAIRED BY ENSAMBLADORES ELECTRONICOS, DE MEXICO S.DE R.L. DE C.V., AVE SIERRA SAN AGUSTIN #2498 COL PORVENIR, MEXICALI, B.C., MEXICO CP 21185, AIR AGENCY CERTIFICATE EASA. 145.0328 UNDER WO# 2288940/001000/POOL DATED 10/25/2011 DATA PLATE REFLECTS INCORPORATION OF MODS E, H, J, N, P, R, T, U, Y, AB, AE, AH, AJ, AK. AVTRAK TASK# 3410555 UPDATED. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF AIRSHOW 400 - 920050 1387 920050 1110 REPLACED AIRSHOW UNIT HAD 306.6 HOURS AND 247 CYCLES BEFORE FAILURE. AVTRACK TASK 2420550 UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 341. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/10/2013 A/C 7222.5 5099 TSMOH 3085.9 7810 INDEX NUMBER 192 ENG 1 6985 4967 APU TACH 4974.3 7802 APU TACH ADJ (-) 1888.4 ENG 2 7167.5 5070 APU CYC ADJ (+) 8 REPLACED LH AND RH FIRE BOTTLE GONE INDICATOR FUSES FOR TIME. INSPECTED PILOTS EMERGENCY OXYGEN MASK FOR CONDITION AND SECURITY, OK FOR SERVICE AVTRAK TASKS# 262009.1, 262010.1 & 351005.1 UPDATED. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF INDICATOR FUSE LH & RH A1003(1) NSN A1003(1) NSN INDICATOR FUSES OBTAINED NEW FROM WESTERN AIRCRAFT; MANUFACTURE DATE: 09/05/2012. NEXT REPLACEMENT DUE BY 1/10/2016. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 342. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/10/2013 A/C 7222.5 5099 TSMOH 3085.9 7810 INDEX NUMBER 193 ENG 1 6985 4967 APU TACH 4974.3 7802 APU TACH ADJ (-) 1888.4 ENG 2 7167.5 5070 APU CYC ADJ (+) 8 REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S FOR NORMAL WEAR PER AMM 32-40-21. OK FOR SERVICE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF NLG WHEEL AND TIRE ASSY LH AH52339 DW061 AH52339 QA033 NLG WHEEL AND TIRE ASSY RH AH52339 149 1045 AH52339 QG038 REMOVED TIRES HAD 249 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4621, DATED 8/12/2011. AVTRAK RECORDS UPDATED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 343. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/11/2013 A/C 7222.6 5099 TSMOH 3085.9 7810 INDEX NUMBER 194 ENG 1 6985.1 4967 APU TACH 4974.3 7802 APU TACH ADJ (-) 1884.4 ENG 2 7167.6 5070 APU CYC ADJ (+) 8 CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 UPDATED AVTRAK RECORDS ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 344. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/16/2013 A/C 7228.1 5102 TSMOH 3087.9 7813 INDEX NUMBER 195 ENG 1 6990.6 4970 APU TACH 4976.3 7805 APU TACH ADJ (-) 1888.4 ENG 2 7173.1 5073 APU CYC ADJ (+) 8 REPLACED RH INBD AND OUTBD MAIN WHEEL AND TIRE ASSY’S FOR NORMAL WEAR PER AMM 32-40-12. OK FOR SERVICE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF MAIN WHEEL ASSY #3 AHA1814 LR165 AHA1814 WW032 MAIN WHEEL ASSY #4 AHA1814 SL105 AHA1814 LC290 TIRE GOODYR FLT EAGLE #3 237K23-2 12842833 237K23-2 11302980 TIRE GOODYR FLT EAGLE #4 237K23-2 11602508 237K23-2 11322953 REMOVED TIRES HAD 166 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 4606, DATED 2/1/2012. UPDATED AVTRAK TASK# 320007 & 320008. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 345. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/2/2013 A/C 7243.7 5109 TSMOH 3091.6 7822 INDEX NUMBER 196 ENG 1 7006.2 4977 APU TACH 4980 7814 APU TACH ADJ (-) 1888.4 ENG 2 7188.7 5080 APU CYC ADJ (+) 8 INSTALLED TWO CONCORDE RG-390E MAIN BATTERIES PURCHASED NEW FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE, AZUSA, CA 91702, TEL (626) 969-7227. UPDATED AVTRAK MAIN BATT CAP CK AND INSTALL RECORDS, TASKS 241015, 241016, 241021, 241022. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF LH MAIN BATTERY #1 RG-390E 40562003 RG-390E 40383367 RH MAIN BATTERY #2 RG-390E 40562002 RG-390E 40383366 CW ELT INSPECTION PER FAR 91-207, AVTRAK TASK 256000 CW CDS-R SYSTEM TEST PER PROCEDURE DOCUMENT 050908018 IAW STC ST01406WI-D ICA, AVTRAK TASK 340020. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 346. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/11/2013 A/C 7254 5117 TSMOH 3085.9 7810 INDEX NUMBER 197 ENG 1 7016.5 4985 APU TACH 3097 7833 APU TACH ADJ (-) 1884.4 ENG 2 7199 5088 APU CYC ADJ (+) 8 LT AND RT "IGNITION ON" LIGHTS DO NOT ILLUMINATE WHEN LH AND/OR RH IGNITION SWITCHES ON. IGNITION OPS NORMAL; LAMPS ILLUMINATE WHEN LIGHT TEST SW ACTIVATED. FOUND OPEN DIODES IN D15 AND D17 POSITION ON PRINTED CIRCUIT BOARD "S". REPLACED WITH NEW DIODES PN 568-7921-1-ND (CV7040 EQUIVALENT) OBTAINED FROM DIGI-KEY, 701 BROOKS AVE SOUTH, PO BOX 677 THIEF RIVER FALLS, MN 56701, TEL (800) 344-4539. OP CKS GOOD. LAVATORY LIGHT BAR FLUORESCENT LIGHTING INOP. NO OUTPUT FROM PI-156-4 INVERTER. EFFECTED MINOR ALTERATION OF LAVATORY WIRING. IN MIDDLE LAVATORY COMPONENT PANEL, REMOVED PI-156-4 INVERTER AND AL5117 POWER SUPPLY, WEIGHT CHANGE NEGLIGIBLE. SPLICED INLINE FUSEHOLDER WITH 3 AMP FUSE BETWEEN (REMOVED) INVERTER +28 VDC SUPPLY WIRE# LY8A20 AND LIGHT BAR SUPPLY WIRE# LY16A18. SPLICED GROUND WIRE# LY8B20N TO LIGHT BAR SUPPLY WIRE# LY15A18. REMOVED FIVE FLUORESCENT LAMPS FROM LIGHT BAR AND INSTALLED FIVE 28 VDC POWERED LED LAMPS, PN L1235250, MFG'D BY AIRCRAFT LIGHTING INTERNATIONAL, 45 EDISON AVE, WEST BABYLON, NY 11704 TEL (631) 474-2254. LIGHTS OP OK. UPDATED ARKANSAS MOD WIRING DIAGRAMS, PAGE 3005-6103 TO REFLECT CURRENT CONFIGURATION. ALTERATION COMPLETED IAW AC43-13-1B CHANGE 1. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 347. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/16/2013 A/C 7262.6 5130 TSMOH 3110.6 7849 INDEX NUMBER 198 ENG 1 7025.1 4998 APU TACH 4999 7841 APU TACH ADJ (-) 1888.4 ENG 2 7207.6 5101 APU CYC ADJ (+) 8 LH LANDING LIGHT INOP. REPLACED LH LANDING LIGHT SWITCH ASSY FOR PRECAUTIONARY. REPLACED FAILED LH LANDING LIGHT LAMP, OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF LOPRESTI BOOM BEAM LAMP ASSY LH LANDING LIGHT LSM-SCD-009-1 48896 LSM-SCD-009-1 48440 LANDING LIGHT SWITCH LH 2TP1-10 NSN 2TP1-10 NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 348. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/12/2013 A/C 7267.9 5138 TSMOH 3111.6 7858 INDEX NUMBER 199 ENG 1 7030.4 5006 APU TACH 5000 7850 APU TACH ADJ (-) 1888.4 ENG 2 7212.9 5109 APU CYC ADJ (+) 8 REPLACED LH AFCS FGC FOR INTERMITTENT AUTOPILOT DISCONNECT. CREW’S FLIGHT FAULT SUMMARY POSTFLT DATA RECORD INDICATES #1 FLIGHT GUIDANCE COMPUTER INTERNAL FAULT. INSTALLED REPAIRED FZ-800 IN LH POSITION, PERFORMED GROUND TEST OF AFCS, CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF #1 FZ-800 FLT GUIDANCE COMPUTER LH 7003974-732 91123099 700374-732 9003214 REMOVED UNIT HAD 243 HOURS AND 192 CYCLES AT FAILURE. INSTALLED UNIT OBTAINED FROM HONEYWELL, 7825 RIDGEPOINT DR, IRVING, TX 75063, CRS# TT1R518K, UNDER WO## 5006212541 DATED 4/4/2013. SERVICED AUX HYDRAULIC RESERVOIR. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 349. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/13/2013 A/C 7267.9 5138 TSMOH 3111.6 7858 INDEX NUMBER 200 ENG 1 7030.4 5006 APU TACH 5000 7850 APU TACH ADJ (-) 1884.4 ENG 2 7212.9 5109 APU CYC ADJ (+) 8 AVIATION PARTNERS, INC. SERVICE BULLETIN NUMBER SBH-13-001 COMPLETED ON 6/13/2013 BY GREG STULTZ, XX XXX LLC. "DO NOT EXCEED FL340" PLACARDS INSTALLED ON CAPT AND FO PFD UNIT. INSERTED SBH-13-001 "MAXIMUM PERMISSIBLE ALTITUDE" PAGE IN LIMITATIONS SECTION OF AIRPLANE FLIGHT MANUAL. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 350. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/18/2013 A/C 7269.2 5140 TSMOH 3112.1 7860 INDEX NUMBER 201 ENG 1 7031.7 5008 APU TACH 5000.5 7852 APU TACH ADJ (-) 1884.4 ENG 2 7214.2 5111 APU CYC ADJ (+) 8 CW AD 2013-11-16, EFFECTIVE 7/2/2013, HAWKER BEECHCRAFT CORPORATION MODEL BAE.125 SERIES 800A AIRPLANES MODIFIED BY AVIATION PARTNERS INC. STC ST01411SE. INSERTED REVISED OPERATIONAL LIMITATIONS-MAX PERMISSIBLE ALTITUDE PAGE IN AIRPLANE FLIGHT MANUAL. INSTALLED PLACARDS ON THE INSTRUMENT PANEL IN ACCORDANCE WITH PARAGRAPH 3.B. OF THE ACCOMPLISHMENT INSTRUCTIONS OF AVIATION PARTNERS SERVICE BULLETIN SBH-13-001, REVISION A, DATED MAY 3, 2013. "DO NOT EXCEED FL340" PLACARDS INSTALLED ON CAPT AND FO PFD UNIT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 351. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/11/2013 A/C 7282.3 5150 TSMOH 3123.4 7871 INDEX NUMBER 202 ENG 1 7044.8 5018 APU TACH 5011.8 7863 APU TACH ADJ (-) 1888.4 ENG 2 7227.3 5121 APU CYC ADJ (+) 8 REPLACED LH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS FOR NORMAL WEAR PER AMM 32-40-12-401. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF MAIN WHEEL ASSY #1 AHA1814 WW032 AHA1814 XB003 MAIN WHEEL ASSY #2 AHA1814 LC290 AHA1814 XB007 TIRE MICHELIN AIR #1 027-504-0 1323S00076 237K23-2 10182962 TIRE MICHELIN AIR #2 027-504-0 1322S00088 237K23-2 11332977 INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT #2, NORTH ROYALTON, OH 44133, CRS L5NR1270 UNDER WO 4882, DATED 4/10/13. OLD TIRES HAD 151 LANDINGS AT TIRE CHANGE. UPDATED AVTRAK TASK 3200005 & 3200006 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 352. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/15/2013 A/C 7282.3 5150 TSMOH 3123.4 7871 INDEX NUMBER 203 ENG 1 7044.8 5018 APU TACH 5011.8 7863 APU TACH ADJ (-) 1884.4 ENG 2 7227.3 5121 APU CYC ADJ (+) 8 COMPLETED AVTRAK TASKS 335010 AND 335310.1, REPLACED AND CHECKED FWD AND AFT EMERGENCY EXIT POWER SUPPLY “D” CELL NI-CAD BATTERIES WITH NEW, 2 EACH PER BATTERY PACK, PN AD-4002P, NSN, BATCH NUMBER AAIU667. BATTERIES OBTAINED FROM MFG’R, AREO DESIGN, INC, 385 INDUSTRIAL DR, MT. JULIET, TN, 37122, PH 800- 551-1158, PRODUCTION APPROVAL HOLDER No. (PAH#) PQ1465CE, FORM TRACKING# STN00026336, DATED 7/11/2013. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 353. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/16/2013 A/C 7282.3 5150 TSMOH 3123.4 7871 INDEX NUMBER 204 ENG 1 7044.8 5018 APU TACH 5011.8 7863 APU TACH ADJ (-) 1884.4 ENG 2 7227.3 5121 APU CYC ADJ (+) 8 CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001. CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002. CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003. CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 492004. DRAINED AND SERVICED APU OIL WITH MOBIL 254. REPLACED APU OIL FILTER ELEMENT. RAN APU, LEAK AND OP CKS OK. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 354. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/1/2013 A/C 7303 5163 TSMOH 3127.2 7886 INDEX NUMBER 205 ENG 1 7065.5 5031 APU TACH 5015.6 7878 APU TACH ADJ (-) 1888.4 ENG 2 7248 5134 APU CYC ADJ (+) 8 "SIDESCREEN OVERHEAT" ANNUNCIATION WHEN LH SCREEN HEAT SW IN ON POSITION. SWAPPED RH AND LH B SCREEN HEAT THERMAL CONTROLLERS. PROBLEM FOLLOWS TO RH SCREEN HEAT SW. REPLACED LH SCREEN HEAT CONTROLLER WITH NEW, OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF MARK 20 ( Mk. 20 ) CONTROLLER LH ND0075-2001 L405073 ND0075-2001 L205607 NEW PART OBTAINED FROM BUSINESS AEROTECH, 610-264-7319. 8130 FROM BEECHCRAFT CORP, 801 INDUSTRIAL BLVD, SUITE 100 GRAPEVINE, TX 76051 FAA PRODUCTION CERTIFICATE # 8 UNDER WO# 0000270294-000030 DATED 5/3/2013 OLD PART HAD 7303 HOURS AT REPLACEMENT. UPDATED AVTRAK TASK 3110539 & 3110540 WITH POSITION AND SN. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 355. Aircraft Logbook Entry XXXPartners Work Order: 301159 Date: August 22, 2013 Serial Number: 2581XX Tail Number: NXXGS Model: BAe125- 800A ACTT: 7311.5 LNDS: 5168 Engine Position: 1 Engine S/N: P-91363 Engine TSN: 7074 Engine Cycles: 5037 Engine Position: 2 Engine S/N: P-91371 Engine TSN: 7256.5 Engine Cycles: 5140 APU APU S/N: 877641 APU TSN: 3129.9 APU CSN: 7891 1. Addressed the following Service Bulletins and Airworthiness Directives: Complied with Aviation Partners, Inc. Service Bulletin SBH-13-002 Rev. A dated July 04, 2013 “Hawker Aileron Re-Balancing” per SB reworked as required both L/H and R/H ailerons. Complied with AD 2013-11-16 Amendment 39-17476 “API Winglets STC-ST01411SE to prevent wing/aileron oscillation, vibration” in accordance with the body of the AD and by incorporating API Service Bulletin SBH-13-002 rev A per AD (i) AMOC approval, removed Placards and AFM Limitations statement required by AD 2013-11-16(g)(h), Ref. FAA AMOC approval letter # 120S-13-410 dated 7/10/2013. All maintenance performed on this aircraft was performed in accordance with the current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. Details on file on W/O #: 301159. Date 8/22/2013 Signed: Paul D Frederick for , CRS# GW4R221M, Augusta, Ga. 30906
- 356. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/10/2013 A/C 7327 5183 TSMOH 3135.4 7904 INDEX NUMBER 206 ENG 1 7089.5 5051 APU TACH 5023.8 7896 APU TACH ADJ (-) 1888.4 ENG 2 7272 5154 APU CYC ADJ (+) 8 RH LANDING LIGHT INTERMITTENT. REPLACED RH LANDING LIGHT LAMP, OP CKS OK NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF LOPRESTI BOOM BEAM LAMP ASSY RH LSM-SCD-009-1 48143 LSM-SCD-009-1 48443 NEW PART OBTAINED FROM LOPRESTI SPEED MERCHANTS, 210 AIRPORT DR, EAST SEBASTIAN FL 32958, TEL: 772 562-4757, OLD PART HAD 150 HOURS AT REPLACEMENT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 357. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/25/2013 A/C 7336.7 5189 TSMOH 3141.6 7916 INDEX NUMBER 207 ENG 1 7099.2 5057 APU TACH 5030 7908 APU TACH ADJ (-) 1888.4 ENG 2 7281.7 5160 APU CYC ADJ (+) 8 COMPLETED 150-200 HOUR ENGINE INSPECTION, AVTRAK TASK CODE 720005, PER HONEYWELL MM 72-00-00 INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES IAW HONEYWELL AMM 79-20-03 AND 79-20-01. RAN ENGINES, LEAK CKS OK. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. COMPLETED INSPECTION OF PITOT/STATIC DRAIN TRAPS, AVTRAK TASK 340002. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF #1 AND #2 ENG OIL FILTERS LH & RH 3070945-1 LOT# 2010L06035 3070945-1 NSN UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 358. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/11/2013 A/C 7342 5190 TSMOH 3143.6 7920 INDEX NUMBER 208 ENG 1 7104.5 5058 APU TACH 5032 7912 APU TACH ADJ (-) 1884.4 ENG 2 7287 5161 APU CYC ADJ (+) 8 CW "E" INSPECTION, AVTRAK TASK 050520 CW WINGLET NAV LIGHT AND TIP STROBE INSPECTIONS, AVTRAK TASKS 334001-API & 334003-API. CW PERIODIC CABIN AND COCKPIT PORTABLE FIRE EXTINGUISHER UNIT CKS, AVTRAK TASKS 262135 & 26136. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 359. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/28/2013 A/C 7342 5190 TSMOH 3143.6 7920 INDEX NUMBER 209 ENG 1 7104.5 5058 APU TACH 5032 7912 APU TACH ADJ (-) 1884.4 ENG 2 7287 5161 APU CYC ADJ (+) 8 CW 200 HOUR LUBE, AVTRAK TASK 050050. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 360. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/11/2013 A/C 7347.7 5198 TSMOH 3146.7 7926 INDEX NUMBER 210 ENG 1 7110.2 5066 APU TACH 5035.1 7918 APU TACH ADJ (-) 1888.4 ENG 2 7292.7 5169 APU CYC ADJ (+) 8 CREW REPORTS STANDBY ATTITUDE INDICATOR EXHIBITS INTERMITTENT PRECESSION. REMOVED ATTITUDE INDICATOR AND SENT TO VENDOR FOR OVERHAUL. INSTALLED OH'D STBY ATTITUDE INDICATOR, OP CKS OK. PART OVERHAULED BY DUNCAN AVIATION, LINCOLN AIRPORT, LINCOLN, NE 68524 UNDER WO# 2LP9A DATED 11/7/2013. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF STBY ATTITUDE INDICATOR - 501-1197-32 5610 501-1197-32 5610 UPDATED AVTRAK RECORD 3400431. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 361. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/5/2013 A/C 7372.1 5215 TSMOH 3157.3 7943 INDEX NUMBER 211 ENG 1 7134.6 5083 APU TACH 5045.7 7935 APU TACH ADJ (-) 1884.4 ENG 2 7317.1 5186 APU CYC ADJ (+) 8 CW 400 HR COOLING TURBINE INSPECTION, OK FOR SERVICE, AFMS TASK 210001. CW 400 HR WATER SEPARATOR INSPECTION, OK FOR SERVICE, AFMS TASK 210006. CW 150 TO 200 HOUR THRUST REVERSER INSPECTION, LT ENGINE, AFMS TASK 783003. CW 150 TO 200 HOUR THRUST REVERSER INSPECTION, RT ENGINE, AFMS TASK 783004. UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 362. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/16/2014 A/C 7395.5 5231 TSMOH 3169.8 7962 INDEX NUMBER 212 ENG 1 7158 5099 APU TACH 5058.2 7954 APU TACH ADJ (-) 1888.4 ENG 2 7340.5 5202 APU CYC ADJ (+) 8 CREW REPORTS PILOTS FLIGHT DISPLAY UNIT SCREEN INTERMITTENTLY FAILS. REMOVED LH PFD AND SENT TO HONEYWELL FOR REPAIR. INSTALLED LOANER UNIT, OP CKS OK. PART ON REPAIRED BY HONEYWELL, 7227 W. HARRY, WICHITA KS UNDER WO# 5007029051 DATED 1/14/2014. MODS W, Y INCORPORATED. UNIT HAD 193.2 HOURS AND 144 CYCLES AT FAILURE. AVTRAK TASK 3460581 UPDATED. RH FMS CDU DISPLAY ALPHANUMERICS INDISTINCT, BLURRY. REPLACED RH FMS CDU WITH REPAIRED UNIT. PART ON REPAIRED BY HONEYWELL, 7227 W. HARRY, WICHITA KS UNDER WO# 5006981431, DATED 12/17/2013. MODS A-S INCORPORATED. UNIT HAD 1644.4 HOURS AND 1355 CYCLES AT FAILURE. AVTRAK TASK 3460552 UPDATED. COCKPIT PORTABLE FIRE EXTINGUISHER CHANGED FOR TIME. NEW PART OBTAINED FROM HRD AEROSYSTEMS, PART CERT FROM OEM FIRE FIGHTING ENTERPRISES LTD, 9 HUNTING GATE, WILBURY WAY, HITCHIN, HERTS, SG4 0TJ ENGLAND. TEL. +44 (0)1462 444740. EASA APPROVAL# UK.21G.2235, WORK ORDER# 119656, DATED 12/4/2013. AVTRAK TASK 262059 AND 262135 UPDATED. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF DU-1080 PFD #1 7023460-02006 01100368 7023460-02006 04030977 CD-800 FMS CDU #2 7004403-902 86100169 7004403-902 92010631 FFE 1211 PORTABLE FIRE EXTINGUISHER - BA51015-5 088333 BA51015-3 0654502 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 363. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/17/2014 A/C 7395.5 5231 TSMOH 3169.8 7962 INDEX NUMBER 213 ENG 1 7158 5099 APU TACH 5058.2 7954 APU TACH ADJ (-) 1888.4 ENG 2 7340.5 5202 APU CYC ADJ (+) 8 CABIN PORTABLE OXYGEN CYLINDER, PN 176965-SMB3, SN 620814, 60 MONTH HYDROSTATIC TEST RQMT CW BY TRI-STATE HYDRO-TEST, DOT RIN I086, CAMBRIDGE MD. AVTRAK TASK 352006 UPDATED. CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001. CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 364. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/25/2014 A/C 7407.1 5237 TSMOH 3173.8 7970 INDEX NUMBER 214 ENG 1 7169.6 5105 APU TACH 5062.2 7962 APU TACH ADJ (-) 1888.4 ENG 2 7352.1 5208 APU CYC ADJ (+) 8 2/25/2014 RVSM, FAR 91.411, FAR 91.413 PER SB 34-3440 AND STC ST01460WI-D CW by Red Eagle Avionics, Dave Gregg, CRS# EHER536D. CW AVTRAK TASKS 340005, 340005.1, 340017, 340018, 340021.1, 340021.2, 340020 JPEG picture of original log entry edited with MS Paint program, used "Rectangular Selection" tool to isolate area to be copied and pasted.
- 365. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/25/2014 A/C 7407.1 5237 TSMOH 3173.8 7970 INDEX NUMBER 215 ENG 1 7169.6 5105 APU TACH 5062.2 7962 APU TACH ADJ (-) 1888.4 ENG 2 7352.1 5208 APU CYC ADJ (+) 8 CW CAPACITY CK OF #1 AND #2 MAIN BATTERIES, AVTRAK TASK 241015, 241016. CW PRESSURE TEST OF STALL WARNING SYSTEM PER AMM 34-11-17, AVTRAK TASK 340009. CW 12 MONTH ELT INSP PER CFR 91.207 & 91.409, ARTEX INSTALL AND OP MANUAL PG 4-3, STEPS 1-4, 6-9, AVTRAK TASK 256000. CW CDSR SYSTEM TESTS PER PROCEDURE DOCUMENT AVTRAK TASK 340020. INSTALLED NEW RG-131 IRS BATTERY. TASK 241030 INSTALLED NEW RG-126 AUXILIARY BATTERIES IN #3, #4 AND #5 POSITIONS. AVTRAK TASKS 241017, 241018, 241019, REMOVED LOANER PFD UNIT AND INSTALLED REPAIRED PFD. REPAIRED BY HONEYWELL, CRS# LV2R992K UNDER WORK ORDER#5007124848 DATED 2/12/2014. AVTRAK TASK 3460581. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF DU-1080 PFD #1 7023460-02006 04030977 7023460-02006 01100368 IRS EMERGENCY BATTERY IRS RG-131 40633504 RG-131 40273576 AUXILIARY BATTERY 3 RG-126 40636573 RG-126 40413638 AUXILIARY BATTERY 4 RG-126 40636579 RG-126 40400072 AUXILIARY BATTERY 5 RG-126 40636584 RG-126 40184860 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 366. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/14/2014 A/C 7428 5251 TSMOH 3182.8 7984 INDEX NUMBER 216 ENG 1 7190.5 5119 APU TACH 5071.2 7976 APU TACH ADJ (-) 1888.4 ENG 2 7373 5222 APU CYC ADJ (+) 8 CREW REPORTED HYDRAULIC "HYD 2 LO PRESSURE" CAME ON DURING EXTENDED DESCENT AT LOW POWER. DID NOT RE-OCCUR ON SUBSEQUENT FLIGHTS; ON GROUND OPS NORMAL. SWAPPED LH AND RH LO PRESSURE WARNING SWITCH FOR TROUBLESHOOTING: QQ NOW P/N 15185-4SN1 S/N 2095. QP NOW P/N 15185-4SN1 S/N 2304. REPLACED RH ENGINE DRIVEN PUMP AS PRECAUTIONARY MEASURE, WORK ACCOMPLISHED PER AMM 29-10-54-401. RAN ENGS, LEAK AND OP CKS OK. OVERHAULED UNIT OBTAINED FROM PARKER HANNIFIN CORP, 2220 PALMER AVE, KALAMAZOO, MI 49001, CRS# UCER345K, UNDER WO# 000699976, DATED 2/08/2010. REMOVED PUMP HAD 3613.4 HOURS, 2810 CYCLES AND 15 YEARS 5 MO TIME IN SERVICE. UPDATED AVTRAK 2930002, 2930003, 2910502. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF #2 ENG DRIVEN HYDRAULIC PUMP ABEX AP05V-086-03 RH 4202203 42022-03 AH-17642 4202202 AH-17852 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 367. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/23/2014 A/C 7433.7 5255 TSMOH 3187.7 7992 INDEX NUMBER 217 ENG 1 7196.2 5123 APU TACH 5076.1 7984 APU TACH ADJ (-) 1888.4 ENG 2 7378.7 5226 APU CYC ADJ (+) 8 REPLACED RH INBD AND OUTBD MAIN WHEEL AND TIRE ASSY’S FOR NORMAL WEAR PER AMM 32-40-12. OK FOR SERVICE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF MAIN WHEEL ASSY #3 AHA1814 XB003 AHA1814 LR165 MAIN WHEEL ASSY #4 AHA1814 XB007 AHA1814 SL105 TIRE GOODYR FLT EAGLE #3 237K23-2 30842566 237K23-2 12842833 TIRE GOODYR FLT EAGLE #4 237K23-2 30842522 237K23-2 11602508 REMOVED TIRES HAD 153 LANDINGS AT REPLACEMENT. INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, CRS L5NR1270 UNDER WO 5044, DATED 10/07/2013. UPDATED AVTRAK TASK# 320007 & 320008. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 368. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/15/2014 A/C 7435.1 5258 TSMOH 3187.7 7992 INDEX NUMBER 218 ENG 1 7197.6 5126 APU TACH 5076.1 7984 APU TACH ADJ (-) 1888.4 ENG 2 7380.1 5229 APU CYC ADJ (+) 8 INVESTIGATED AND REPAIRED SLOW RATE OXYGEN SYSTEM LEAK. FOUND AND REPLACED LEAKING "FILTER AND BURSTING DISK" ASSY "STANDBY BURSTING DISK FILTER HOLDER" SEAL. REPLACED SEAL, LEAK CKS GOOD. AT O2 SYSTEM SUPPLY MANIFOLD; REMOVED AND CAPPED AUX 3rd BOTTLE OXYGEN SUPPLY LINE AND INSTALLED BLANKING PLUG AT PORT FOR AUX BOTTLE LINE. BLANKING PLUG LEAK CKS GOOD. CW FO/CREW OXYGEN MASK REGULATOR INSPECTION PER AMM 35-23-52-501. SWAPPED MAIN BATTERIES POSITION. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF SEAL - AGS11860 NSN AGS11860 NSN INSTALLED OXYGEN SYSTEM SEAL OBTAINED FROM BEECHCRAFT, COPY OF CAA ARCAA TAG ON FILE, CERTIFICATE REF NO. CSD207352 DATED 8/9/1996. UPDATED AVTRAK TASK# 351006.1. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 369. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/14/2013 A/C 7442.7 5263 TSMOH 3190.3 7997 INDEX NUMBER 219 ENG 1 7205.2 5131 APU TACH 5078.7 7989 APU TACH ADJ (-) 1888.4 ENG 2 7387.7 5234 APU CYC ADJ (+) 8 CW AD 2014-12-52, DATED 6/10/2014 & HONEYWELL INTERNATIONAL ALERT SERVICE BULLETINS (ASB) NO. TFE731-72-A3792, DATED JUNE 5, 2014, ASB NO. TFE731-72-A5242, DATED JUNE 5, 2014, AND ASB NO. TFE731-72-A5243, DATED JUNE 5, 2014. REVIEWED BOTH ENGINE LOG BOOKS TO DETERMINE THAT NO LPT2 BLADES P/N 3075424-1, -2, OR -3 WITH LESS THAN 250 OPERATING HOURS SINCE NEW ARE INSTALLED AT THIS TIME. NO FURTHER ACTION REQUIRED. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 370. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/11/2014 A/C 7469.1 5285 TSMOH 3202 8023 INDEX NUMBER 220 ENG 1 7231.6 5153 APU TACH 5090.4 8015 APU TACH ADJ (-) 1888.4 ENG 2 7414.1 5256 APU CYC ADJ (+) 8 CW LH AND RH 200-400 HR STARTER GENERATOR INSP PER AMM 24-30-21. CW SB TFE731-72-A3792 R1 AND AD 2014-12-52 (SUPERSEDES EMERGENCY AD 2014-12-52 PREVIOUSLY CW), EFFECTIVE 7/28/2014, ON ENG #1 AND ENG #2, NA AT THIS TIME. CW 150-200 HR AND 300-400 HR INSPECTIONS ON #1 AND #2 ENGINES PER HONEYWELL MM 72-00-00 INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES IAW HONEYWELL AMM 79-20-03 AND 79-20-01. RAN ENGINES, LEAK CKS OK. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. GENERATORS OP CKS OK. REPLACED WORN BRACKET, PN C46P18125-17, MID ENGINE, 12 O'CLOCK POS #1 ENG. REPLACED AND CHECKED FWD AND AFT EMERGENCY EXIT POWER SUPPLY “D” CELL NI-CAD BATTERIES WITH NEW, 2 EACH PER BATTERY PACK, PN AD-4002P, NSN, BATCH NUMBER AAJS-226. BATTERIES OBTAINED FROM MFG’R, AREO DESIGN, INC, 385 INDUSTRIAL DR, MT. JULIET, TN, 37122, PH 800- 551-1158, PRODUCTION APPROVAL HOLDER No. (PAH#) PQ1465CE, FORM TRACKING# STN00029469, DATED 6/30/14. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF BRACKET #1 C46P18125-17 NSN C46P18125-17B NSN ENG OIL FILTERS #1 & #2 3070945-1 LOT# 2011F18684 MLOT# 50221136 3070945-1 NSN UPDATED AVTRAK TASK# 240001.1, 240001.2, 335010, 335010.1, 720005, 720011, 950072-A3792.1 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 371. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/29/2014 A/C 7486.8 5294 TSMOH 3207.1 8034 INDEX NUMBER 221 ENG 1 7249.3 5162 APU TACH 5095.5 8026 APU TACH ADJ (-) 1888.4 ENG 2 7431.8 5265 APU CYC ADJ (+) 8 RELAMPED TAIL STROBE/NAV ASSY NAV LIGHT BULB, PN 678, OP CKS OK. TWO OF FOUR LED LIGHT BARS IN LH NAV LIGHT ASSY INOP. REPLACED LH WINGLET LED NAV LIGHT ASSY, WHELEN MODEL 9028502, PN 01-0790285-02, OP CKS OK. API PN ON: H800-353-1, SN ON: 170, PN OFF: H800-0353-1, SN OFF 00146. REMOVED PART HAD 2 YR, 10 M, 925 HRS, 401 CYCLES AT FAILURE. CW CAPACITY CK OF #1 AND #2 MAIN BATTERIES, CKS OK. AVTRAK TASK 241015, 241016. CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 492004. CW APU BIENNIAL/1500 HR/3000 CYCLE MAINTENANCE AVTRAK TASK 492005. DRAINED AND SERVICED APU OIL WITH MOBIL 254. REPLACED APU OIL FILTER ELEMENT WITH NEW DONALDSON/WESTERN FILTER, PN WF331667 (ALT PN FOR SUNDSTRAND 179411). CLEANED APU FUEL INLET FILTER PN 211-326, REPLACED PN 3500AS12 CRUSH GASKET (DONALDSON/WESTERN FILTER). APU LEAK AND OP CKS OK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 372. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/1/2014 A/C 7493.3 5298 TSMOH 3209.6 8038 INDEX NUMBER 222 ENG 1 7255.8 5166 APU TACH 5098 8030 APU TACH ADJ (-) 1888.4 ENG 2 7438.3 5269 APU CYC ADJ (+) 8 REPLACED CRACKED RH WING TIP STROBE LIGHT LENS WITH NEW. PN ON: 68-2290005-34. PART OBTAINED FROM CHIEF AIRCRAFT. CW API WINGLET TIP STROBE ASSY, LH AND RH INSPECTION, AVTRAK TASK 334003-API. CW API WINGLET NAV LIGHT LENS, LH AND RH INSPECTION, AVTRAK TASK 334001-API. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 373. Transcribed Gama AviationSupport Services Log entry DATE AFTT CYCLES 9/29/2014 7523.7 5335 GAMA SUPPORT SERVICES 3867 Southern Boulevard West Palm Beach FL 33406 Office 561-689-7675 Fax 561-689-1334 Certificate CRS - VYQD491Y Accomplished inbound/preliminary inspection Removed K9 power supply relay Installed New Customer supplied K9 power supply relay. No defects noted Removed #1 Radio Master switch assembly. Installed a New Customer supplied #1 Radio Master switch assembly. No defects noted. Accomplished Final inspection The following components were replaced. Part Name PN ON PN OFF SN ON SN OFF Relay MS24166-D1 MS24166-D1 NSN NSN Switch 99-222 99-222 NSN NSN
- 374. Aircraft Logbook Entry XXXPartners Inc. Work Order: 310473 Date: October 13, 2014 Serial Number: 2581XX Tail Number: NXXGS Model: Hawker 800 ACTT: 7533.7 LNDS: 5340 Engine Position: 1 Engine S/N: P-91363 Engine TSN: 7296.2 Engine Cycles: 5208 Engine Position: 2 Engine S/N: P-91371 Engine TSN: 7478.7 Engine Cycles: 5311 APU APU S/N: 877641 APU TSN: 3240.5 APU CSN: 8083 9. C/W the following Maintenance Schedule Inspection items: 12 Month “E1-E12” Manufacturer’s routine inspection. 24 Month “F1-F12” Manufacturer’s routine inspection. 10. C/W the following Maintenance Schedule Minor Inspection items: 200 Hour Lubrication. 400 Hour Lubrication. 11. C/W the following MS Structural inspection requirements: 550015, 2 Year elevator mass balance weights and spigots. IAW Hawker 800 AMM. 570010, 1200 Hours Wing bottom skin (L/H and R/H) adjacent to flap outboard hinge at Rib 8. 12. C/W the following MS Out of Phase inspection requirements: 300007, 1 Month purge of the airplane ice protection system. 13. Addressed the following Airworthiness Directives and MFG Service Bulletins: AD2014-17-02Amendment39-17955: Honeywell ASCa emergency locator transmitter units. o Determined to be not applicable due to MFG of installed equipment is Artex. AD2014-18-01Amendment39-17965: Rockwell Collins TDR-94D. o Determined to be not applicable due to equipment not installed. 14. C/W the following MS Life Limited/Component Overhaul requirements and Tasks: 342561-24M, Inspect Under Upper and Lower TCAS Antenna {ICA Document #44504900}. 261070- 60M-Removed and reinstalled (6ea.) inspected Aft Bay heat detector p/n 150D/01/100(2), inspected by StandardAero CRS# GW4R221M / EASA 145.4973 dated 10/08/2014 IAW Hawker 800 AMM 26-10-41. 261055, 60M-Removed and reinstalled inspected APU Fuel Pump Enclosure Fire Warning Switch p/n 17343-62 inspected by StandardAero CRS# GW4R221M / EASA 145.4973 dated 10/09/2014. 261056, 60M-Removed and reinstalled inspected APU lower Fuel Pump Enclosure Fire Warning Switch p/n 160275-1 inspected by StandardAero CRS# GW4R221M / EASA 145.4973 dated 10/08/2014. 261065, 60M-Removed and reinstalled inspected APU Generator Overheat Switch. Generator Exhaust Shroud p/n 67100-1-350F inspected by StandardAero CRS# GW4R221M / EASA 145.4973 dated 10/09/2014. 15. Performed the following miscellaneous maintenance: Installed new R/H wing landing light bulb p/n LSM-SCD-009-1. Removed and replaced various hardware, bonding jumpers, lamps, abrasion tape, sealant and paint as needed with new parts in accordance with Hawker 800 AMM. Details on file under StandardAero WO#: 310473. I certify this Aircraft has been inspected in accordance with a “E & F” inspection under FAR 91.409 F (3) and approved for return to service. Details under W/O#: 310473. Date: 10/13/2014, ACTT: 7533.7. Signed Thomas Styczynski for CRS# GW4R221M, Augusta, GA. 30906
- 375. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/15/2014 A/C 7534.9 5341 TSMOH 3241 8084 INDEX NUMBER 223 ENG 1 7297.4 5209 APU TACH 5129.4 8076 APU TACH ADJ (-) 1888.4 ENG 2 7479.9 5312 APU CYC ADJ (+) 8 CW TIME CHANGE RQMT ON PILOT POSITION EMERGENCY OXYGEN MASK. INSTALLED NEW MASK IN CAPT POSITION. OP CKS OK. MASK OBTAINED FROM WESTERN AIRCRAFT, OVERHAULED BY AVOX SYSTEMS INC. 225 ERIE STREET, LANCASTER, NY 14086, CRS LX1R312K UNDER WO# R62528 DATED 10/2/2014. REPLACED #1 AND #2 MAIN WHEEL AND TIRE ASSYS FOR TIRE CHANGE. WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT #2, NORTH ROYALTON, OH 44133, CRS L5NR1270 UNDER WO# 5207, DATED 6/4/2014. OLD TIRES HAD 191 LANDINGS AT TIRE CHANGE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF EMER OXYGEN MASK #1 MC10-14-124 AE352 MC10-14-124 63721 MAIN WHEEL ASSY #1 AHA1814 SL105 AHA1814 WW032 MAIN WHEEL ASSY #2 AHA1814 LR165 AHA1814 LC290 TIRE ASSY #1 237K23-2 31782572 027-504-0 1323S00076 TIRE ASSY #2 237K23-2 31772817 027-504-0 1322S00088 UPDATED AVTRAK TASK# 351005 320005 320006. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 376. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/16/2014 A/C 7534.9 5341 TSMOH 3241 8084 INDEX NUMBER 224 ENG 1 7297.4 5209 APU TACH 5129.4 8076 APU TACH ADJ (-) 1888.4 ENG 2 7479.9 5312 APU CYC ADJ (+) 8 CREW REPORTS INTERMITTENT SLIGHT VIBRATION IN CONTROL COLUMN. FOUND PLAY IN LH ELEVATOR TRIM TAB; REPLACED BOTH AFT LH TAB BEARINGS, PN CN6-35MESP56G AND PN CN6-35MESP56 AND BOLTS, PN DHS1433-6-1-2E. NO FREE MOVEMENT IN TAB SURFACE OBSERVABLE. OK FOR SERVICE. CW 400 HR WALK AROUND INSPECTION. OK FOR SERVICE. CW ELT 12 MONTH INSPECTION. CW CDS-R SYSTEM TEST. AVTRAK TASKS : 050800 256000 340020 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 377. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 11/6/2014 A/C 7549.2 5350 TSMOH 3241 8084 INDEX NUMBER 225 ENG 1 7311.7 5218 APU TACH 3245.7 8093 APU TACH ADJ (-) 1888.4 ENG 2 7494.2 5321 APU CYC ADJ (+) 8 CREW REPORTS #2 ENG INTERMITTENT N2 INDICATION FLUCTUATION AT CRUISE. POWER CHANGES MAKE FLUCTUATION CEASE. PER LMM 77-10-05 SWAPPED LH AND RH N2 TRANSDUCERS, PN 3070722-3, SKURKA (MANUFACTURER) PN H593-CP850 FOR TROUBLESHOOTING. LH SN NOW 5912, RH SN 4418. RAN ENGS, LEAK AND OP CKS OK. CREW REPORTS APU AMMETER INOP. CLEANED TERMINALS ON APU AMMETER, RESET APU CIRCUIT BREAKERS CB8 & CB9. RAN APU, OPS OK. REPLACED 6 INOP APU CONTROL PANEL 5 VOLT BACKGROUND LAMPS, PN 683-AS15. CREW REPORTS INTERMITTENT RH DISPLAY CONTROLLER APPEARS TO HAVE NO POWER WITH RH PFD BLANK. REPLACED RH PFD DISPLAY CONTROLLER WITH REPAIRED UNIT FROM HONEYWELL. OP CKS OK. DC-550 ON REPAIRED BY HONEYWELL, 7227 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K UNDER WO# 5006983493 DATED 2/11/2014. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S FOR NORMAL WEAR PER AMM 32-40-21. OK FOR SERVICE. REMOVED TIRES HAD 251 LANDINGS AT REPLACEMENT. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF RH PFD DISPLAY CONTROLLER DC-550 RH 7016986-108 03065072 7016986-108 06036287 NLG WHEEL ASSY LH AH52339 QA033 AH52339 DW061 NLG WHEEL ASSY RH AH52339 QG038 AH52339 149 1045 INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, 44133, CRS L5NR1270 UNDER WO# 4883, DATED 3/28/2013. UPDATED AVTRAK TASKS# 3400571 7710003.1 7710003.2 3200011 3200012. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 378. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/3/2014 A/C 7567.3 5369 TSMOH 3255.9 8116 INDEX NUMBER 226 ENG 1 7329.8 5237 APU TACH 3245.7 8093 APU TACH ADJ (-) 1888.4 ENG 2 7512.3 5340 APU CYC ADJ (+) 8 FOR MAINTENANCE CONVENIENCE, REPLACED #2 RADIO MASTER RELAY WITH NEW. OPS CK GOOD. PART OBTAINED FROM RAPID. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF RADIO MASTER RELAY MFG PN 6041H200 K10 MS24166-D1 NSN MS24166-D1 NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 379. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/23/2014 A/C 7573.3 5374 TSMOH 3258.2 8123 INDEX NUMBER 227 ENG 1 7335.8 5242 APU TACH 3245.7 8093 APU TACH ADJ (-) 1888.4 ENG 2 7518.3 5345 APU CYC ADJ (+) 8 COMPLETED 191-240 HOUR THRUST REVERSER INSPECTION PER NORDAM TR5000 MM. COMPLETED 391-440 HOUR THRUST REVERSER INSPECTION PER NORDAM TR5000MM. RH PFD HAS HEADING FLAG. REPLACED #2 AHARS UNIT, NO HELP. FOUND BROKEN WIRE AT CONNECTOR POSITION "E" ON #2 FLUX VALVE. REPLACED CONNECTOR, OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF AH-600 ATTITUDE AND HEADING REFERENCE UNIT #2 7003360-943 89071429 7003360-943 97083876 REPAIRED AHARS UNIT OBTAINED FROM HONEYWELL , 7227 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K UNDER WO# 5007646329 DATED 8/13/2014. OLD AHARS HAD 1001.1 HRS AND 837 CYCLES AT REPLACEMENT. UPDATED AVTRAK TASKS 3460522, 783003, 783004, 783007, 783008. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 380. Reg. # NXXGSDate: 1/6/2015 Work Order: Y3BU Model: Hawker 800A S/N: 2581XX TAT: 7594.7 Make: Honeywell Model: TFE731- 5R-1H Engine Position: #2 Engine S/N: P-91371 TSN: 7539.7 CSN: 5353 I) The following maintenance was performed by Duncan Aviation under work order# Y3BUA: A) Removed No. 2 engine N2 monopole TRANSDUCER P/N 3070722-3 S/N 4418. Installed NEW condition N2 monopole P/N 3070722-3 S/N 67998. Reference 8130-3 dated 5/Jan/2015 issued by Honeywell International, Inc ODA-602216-NM, form tracking number 20150000426791Y14 8004051099-10, Work order F23506. B) Post ground run leak and operational check The above described repair or maintenance is approved for return to service. A detailed record is on file under Work Order # Y3BUA. Signed_____________________________________________________ For Duncan Aviation CRS JGVR194F Phone: 800-228-4277
- 381. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/19/2015 A/C 7594.7 5382 TSMOH 3267.1 8130 INDEX NUMBER 228 ENG 1 7357.2 5250 APU TACH 5155.5 8122 APU TACH ADJ (-) 1888.4 ENG 2 7539.7 5353 APU CYC ADJ (+) 8 LH FUEL QTY INDICATOR NEEDLE STICKS INTERMITTANTLY, TAPPING GLASS FREES NEEDLE. REPLACED LH FUEL QTY INDICATOR PER AMM, CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF FUEL QUANTITY INDICATOR LH WL-1901KID-1 931073 WL-1901KID-1 TT5124 OVERHAULED INDICATOR OBTAINED FROM GLOBAL PARTS, INC. INDICATOR OVERHAULED BY PACIFIC SOUTHWEST INSTRUMENTS, CRS# KD3R627L, 1721 RAILROAD ST, CORONA CA 92880, TEL 951-737-0790 UNDER WO# 283255 DATED 12/15/2014. OLD INDICATOR ORIGINAL TO AIRPLANE. UPDATED AVTRAK TASK 2841005. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 382. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/2/2015 A/C 7594.7 5382 TSMOH 3267.2 8131 INDEX NUMBER 229 ENG 1 7357.2 5250 APU TACH 5155.6 8123 APU TACH ADJ (-) 1888.4 ENG 2 7539.7 5353 APU CYC ADJ (+) 8 CW APU SEMI-ANNUAL 125 HR OR 250 CYCLES AND SEMI-ANNUAL 250 HR OR 500 CYCLES INSPECTION PER SUNSTRAND MM. OK FOR SERVICE. UPDATED AVTRAK TASKS : 492001 492002 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 383. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/4/2015 A/C 7594.7 5382 TSMOH 3267.2 8131 INDEX NUMBER 230 ENG 1 7357.2 5250 APU TACH 5155.6 8123 APU TACH ADJ (-) 1888.4 ENG 2 7539.7 5353 APU CYC ADJ (+) 8 CW CAPACITY CK OF #1 AND #2 RG-390E MAIN BATTERIES. OK FOR SERVICE. INSTALLED SN 40562002 IN #1 POSITION, SN 40562003 IN #2 POSITION. CW CAPACITY CK OF RG-131 SN 40633504 IRS EMERGENCY BATTERY. OK FOR SERVICE. CW CAPACITY CK OF RG-126 #3, #4 AND #5 EMERGENCY BATTERIES. OK FOR SERVICE. INSTALLED SN 40636579 IN #3 POSITION, SN 40636573 IN #4 POSITION AND SN 40636584 IN #5 POSITION. UPDATED AVTRAK TASKS: 241015 241016 241030 241017 241018 241019. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 384. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/23/2015 A/C 7642.2 5424 TSMOH 3291.4 8176 INDEX NUMBER 231 ENG 1 7404.7 5292 APU TACH 5179.8 8168 APU TACH ADJ (-) 1888.4 ENG 2 7587.2 5395 APU CYC ADJ (+) 8 REPLACED #3 AND #4 MAIN WHEEL AND TIRE ASSYS FOR TIRE CHANGE PER AMM 32-40-12. WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT #2, NORTH ROYALTON, OH 44133, CRS L5NR1270 UNDER WO# 5355 DATED 12/9/2014. REMOVED TIRES HAD 169 LANDINGS AT REPLACEMENT. REPLACED RH AIRBRAKE JACK FOR TIME. INSTALLED SERVICEABLE RH AIRBRAKE JACK PER AMM 27-61-31. OP CKS OK. AIRBRAKE JACK OBTAINED FROM SOUTHWEST AVIATION SPECIALTIES, 8720 JACK BATES AVE., TULSA OK 74132 TEL: (918) 298-4044 UNDER WO# 15-0117 DATED 4/27/2010. AIRBRAKE JACK HAS 941.1 TTSOH, 2058.9 HOURS REMAINING TILL NEXT OH. CW 150-200 HR INSPECTIONS ON #1 AND #2 ENGINES PER HONEYWELL MM 72-00-00 INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES IAW HONEYWELL AMM 79-20-03 AND 79-20-01. RAN ENGINES, LEAK CKS OK. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF MAIN WHEEL ASSY #3 AHA1814 WW032 AHA1814 XB003 MAIN WHEEL ASSY #4 AHA1814 LC290 AHA1814 XB007 TIRE GOODYR FLT EAGLE #3 237K23-2 42612594 237K23-2 30842566 TIRE GOODYR FLT EAGLE #4 237K23-2 42622566 237K23-2 30842522 AIRBRAKE JACK RH AIR4652-1 9006707 AIR46521-1 LK0367 UPDATED AVTRAK TASK 3200007 3200008 276006 720005. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 385. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/29/2015 A/C 7642.2 5424 TSMOH 3291.4 8176 INDEX NUMBER 232 ENG 1 7404.7 5292 APU TACH 5179.8 8168 APU TACH ADJ (-) 1888.4 ENG 2 7587.2 5395 APU CYC ADJ (+) 8 REPLACED FORWARD AND AFT FIRE BOTTLE CARTRIDGES PER AMM 26-20-12 (FOR TIME) WITH NEW CARTRIDGES MFG'D BY AMETEK AMERON, APPROVAL # 262354014, 4750 LITTLEJOHN STREET, BALDWIN PARK CA 91706 UNDER WO# 18880.1, DATED 9/18/2014. DATE OF MFG FOR ALL 4 CARTRIDGES 8/2014. PARTS OBTAINED FROM HRD AEROSPACE 661-295-0670. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF FIRE EXTINGUISHER CARTRIDGE GJ-P2 M30900000M 06691 M30900000M 02190 FIRE EXTINGUISHER CARTRIDGE GJ-S1 M30900000M 06696 M30900000M 02230 FIRE EXTINGUISHER CARTRIDGE GH-P1 M30900000M 06685 M30900000M 02209 FIRE EXTINGUISHER CARTRIDGE GH-S2 M30900000M 06687 M30900000M 02226 UPDATED AVTRAK TASK 262015 262016 262017 262018. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 386. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 5/22/2015 A/C 7650.4 5432 TSMOH 3295.5 8184 INDEX NUMBER 233 ENG 1 7412.9 5300 APU TACH 5183.9 8176 APU TACH ADJ (-) 1888.4 ENG 2 7595.4 5403 APU CYC ADJ (+) 8 REPLACED FO EMERGENCY OXYGEN MASK ASSY (FOR TIME) WITH OVERHAULED PART BY AMERON GLOBAL, CRS OWR461N, 1350-2 LINCOLN AVE, HOLBROOK, NY 11741 UNDER WO# 313874, DATED 4/29/2015. PART OBTAINED FROM DUNCAN AVIATION. CW AD 2015-08-07, EFF 6/6/2015, CREW O2 MASKS CURRENTLY INSTALLED ARE NA BY PN/SN PER ZODIAC AEROSPACE SB MXH-35-240 APPENDIX 2. CW BEECHCRAFT SB 25-4155, REV 1, NA, APPLICABLE CABIN SEAT BELT BUCKLES NOT INSTALLED AT THIS TIME. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF INTERTECHNIQUE EROS F5341 CREW O2 MASK FO MC10-14-124 46651 MC10-14-124 58516 UPDATED AVTRAK TASKS 351006 98245155 9990-2015-08-07. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 387. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/1/2015 A/C 7650.4 5432 TSMOH 3295.5 8184 INDEX NUMBER 234 ENG 1 7412.9 5300 APU TACH 5183.9 8176 APU TACH ADJ (-) 1888.4 ENG 2 7595.4 5403 APU CYC ADJ (+) 8 ACCOMPLISHED MANDATORY HAWKER BEECHCRAFT SB 32-3979, REV. 1, REVISED MAY, 2015, FOUND NA BY SERIAL NUMBER. COMPLIANCE WORKSHEET FAXED TO BEECHCRAFT CORPORATION. MAIN LANDING GEAR SIDE AND DRAG STAYS LH MLG SN: DHL/DH/1503 LH MLG SIDE STAY SN: DHL/DH/1481 RH MLG SN: DHL/DH/1490 RH MLG SIDE STAY SN: DHL/DH/1488 NLG SN: DHL/DH/742 NLG DRAG STAY SN: DHL/DH/732 UPDATED AVTRAK RECORDS. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 388. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/11/2015 A/C 7651.8 5434 TSMOH 3297.2 8186 INDEX NUMBER 235 ENG 1 7414.3 5302 APU TACH 5185.6 8178 APU TACH ADJ (-) 1888.4 ENG 2 7596.8 5405 APU CYC ADJ (+) 8 RH LANDING LIGHT INOP. RH BULB SHATTERED. REPLACED RIGHT LANDING LIGHT REFLECTOR, BULB AND BALLAST ASSYS. CKS OK. NEW REFLECTOR, BULB AND BALLAST ASSYS FROM OEM LOPRESTI SPEED MERCHANTS, 210 AIRPORT EAST DR, EAST SEBASTIAN, FL 32958 PMA# PQ1372CE UNDER WO# REP7117C DATED 6/6/2015 NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF HID LANDING LIGHT REFLECTOR RH LSM-500-300-46L NSN LSM-500-300-46L NSN HID LAMP ASSY RH LSM-SCD-009-1 54220 LSM-SCD-009-1 NSN HID BALLAST 60 WATT RH LSM-SCD-019-1 54103 LSM-SCD-019-1 NSN ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 389. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/2/2015 A/C 7658.9 5440 TSMOH 3299.9 8195 INDEX NUMBER 236 ENG 1 7421.4 5308 APU TACH 5188.3 8187 APU TACH ADJ (-) 1888.4 ENG 2 7603.9 5411 APU CYC ADJ (+) 8 CREW REPORTS #1 HEADING INDICATION IS INACCURATE CAUSING HEADING COMPARISON ANNUNCIATION. REPLACED #1 COMPASS FLUX DETECTOR WITH NEW UNIT PER HONEYWELL 22-16-00 PG 707. CKS OK. FLUX DETECTOR OBTAINED FROM HONEYWELL, 21111 N. 19TH AVE, PHOENIX AZ 85027 UNDER PRODUCTION APPROVAL# PT1354NM, WO# 4701346657-000010 DATED 5/9/2011. PERFOMED COMPASS SWING ON MAGNETIC COMPASS, #1 & #2 COMPASS SYSTEM. #2 ADF FAILS POWER UP TEST. REPLACED #2 INTEGRATED NAVIGATION UNIT PER HONEYWELL 22-16-00 PG 702 WITH REPAIRED UNIT FROM HONEYWELL, CRS# LV2R992K, WO#5008487456 DATED 6/1/2015. OP CKS OK. CW EMERGENCY EXIT LIGHT BATTERY CK. OK FOR SERVICE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF FLUX VALVE FX-600 LH 7010133 1103J876 7010133 88100687 NAV UNIT RNZ-850 RH 7510100-731 04037330 7510100-731 88080165 UPDATED AVTRAK TASKS 3460530 340013.1 340013.2 340013.3 3420005 335010. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 390. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/2/2015 A/C 7658.9 5440 TSMOH 3299.9 8195 INDEX NUMBER 237 ENG 1 7421.4 5308 APU TACH 5188.3 8187 APU TACH ADJ (-) 1888.4 ENG 2 7603.9 5411 APU CYC ADJ (+) 8 APU WILL NOT START ON FIRST ATTEMPT. NO FUEL FOUND IN DRAIN CAN AFTER MULTIPLE STARTS. FOUND START FUEL NOZZLE PURGE RESTRICTOR (PN 179290-1) AND START FUEL NOZZLE (PN 4503159) CLOGGED WITH VARNISH AND COKE. CLEANED NOZZLE ASSY AND PURGE RESTRICTOR. APU STARTS AND OPS NORMAL. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 391. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/27/2015 A/C 7683.4 5453 TSMOH 3314.4 8211 INDEX NUMBER 238 ENG 1 7445.9 5321 APU TACH 5202.8 8203 APU TACH ADJ (-) 1888.4 ENG 2 7628.4 5424 APU CYC ADJ (+) 8 CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 492004. DRAINED AND SERVICED APU OIL WITH MOBIL 254. CLEANED APU FUEL INLET FILTER PN 211-326, REPLACED PN 3500AS12 CRUSH GASKET (DONALDSON/WESTERN FILTER). APU LEAK AND OP CKS OK. CW API WINGLET TIP STROBE ASSY, LH AND RH INSPECTION, AVTRAK TASK 334003-API. CW API WINGLET NAV LIGHT LENS, LH AND RH INSPECTION, AVTRAK TASK 334001-API. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 392. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/1/2015 A/C 7689.8 5456 TSMOH 3316.7 8214 INDEX NUMBER 239 ENG 1 7452.3 5324 APU TACH 5205.1 8206 APU TACH ADJ (-) 1888.4 ENG 2 7634.8 5427 APU CYC ADJ (+) 8 CW CAPACITY CK OF #1 AND #2 RG-390E MAIN BATTERIES. OK FOR SERVICE. INSTALLED SN 40562002 IN #1 POSITION, SN 40562003 IN #2 POSITION. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF MAIN BATTERY LH RG-390E 40562003 RG-390E 40562002 MAIN BATTERY RH RG-390E 40562002 RG-390E 40562003 RESEARCHED AD 2012-11-09 R1 DATED 8/1/2015, FOUND NA, CHEMICAL OXYGEN GENERATORS NOT INSTALLED IN THIS AC AT THIS TIME. UPDATED AVTRAK TASKS: 241015 241016. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 393. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/12/2015 A/C 7691.9 5457 TSMOH 3316.7 8214 INDEX NUMBER 240 ENG 1 7454.4 5325 APU TACH 5205.1 8206 APU TACH ADJ (-) 1888.4 ENG 2 7636.9 5428 APU CYC ADJ (+) 8 RESEARCHED AD 2015-16-04, EFFECTIVE 9/15/2015. FOUND NA AT THIS TIME BY PN. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 394. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/18/2015 A/C 7694.4 5459 TSMOH 3318 8218 INDEX NUMBER 241 ENG 1 7456.9 5327 APU TACH 5206.4 8210 APU TACH ADJ (-) 1888.4 ENG 2 7639.4 5430 APU CYC ADJ (+) 8 CREW REPORTS NLG SHIMMY ON TAKEOFF AND LANDING. GREASED NLG TORQUE LINKS. REPLACED LT AND RT NOSE LANDING GEAR WHEEL AND TIRE ASSY’S PER AMM 32-40-21. REMOVED TIRES HAD 109 LANDINGS AT REPLACEMENT. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF NOSE WHEEL ASSY LH AH52339 DW061 AH52339 QA033 NOSE WHEEL ASSY RH AH52339 8363/07138 AH52339 QG038 INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT 2, NORTH ROYALTON, OH, 44133, CRS L5NR1270 UNDER WO# 5427, DATED 4/15/2015. UPDATED AVTRAK TASKS# 3200011 3200012. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 395. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/21/2015 A/C 7698.7 5464 TSMOH 3321.9 8224 INDEX NUMBER 242 ENG 1 7461.2 5332 APU TACH 5210.3 8216 APU TACH ADJ (-) 1888.4 ENG 2 7643.7 5435 APU CYC ADJ (+) 8 CREW REPORTS RH FMS CDU ALPHANUMERIC DISPLAY SCRAMBLED. REPLACED RH FMS CONTROL DISPLAY UNIT. OP CKS OK. MOD STATAUS:A-S NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF CD-800 FMS CDU RH 7004403-902 88090372 70044003-902 86100169 INSTALLED UNIT REPAIRED BY HONEYWELL, CRS LV2R992K UNDER WO# 5008586923, DATED 7/21/2015. UPDATED AVTRAK TASKS# 3460522. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 396. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 8/25/2015 A/C 7698.7 5464 TSMOH 3321.9 8224 INDEX NUMBER 243 ENG 1 7461.2 5332 APU TACH 5210.3 8216 APU TACH ADJ (-) 1888.4 ENG 2 7643.7 5435 APU CYC ADJ (+) 8 TWO OF FOUR LED LIGHT BARS IN LH NAV LIGHT ASSY INOP. REPLACED LH WINGLET LED NAV LIGHT ASSY, WHELEN MODEL 9028502, PN 01-0790285-02, WHELEN SN 5161630. OP CKS OK. REMOVED PART HAD 1 YR 1 M, 229 HRS, 130 CYCLES AT FAILURE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF API NAV LAMP ASSY LH H800-0353-1 00184 H800-0353-1 170 INSTALLED UNIT REPAIRED BY WHELEN ENGINEERING COMPANY, APPROVAL/CERTIFICATE# PT01610NE UNDER WO# 20805-1545, DATED 4/23/2015. UPDATED AVTRAK TASKS# 334002.1 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 397. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/2/2015 A/C 7698.7 5464 TSMOH 3321.9 8224 INDEX NUMBER 244 ENG 1 7461.2 5332 APU TACH 5210.3 8216 APU TACH ADJ (-) 1888.4 ENG 2 7643.7 5435 APU CYC ADJ (+) 8 REPLACED OBSOLETE FLOPPY DISK DATA LOADER DL-900 WITH USB DATA LOADER DL-950. OP CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF FMS DATA LOADER - G7226-01 2662 7016600-901 98011164 INSTALLED UNIT OBTAINED FROM STANDARD AERO, NEW FROM MANUFACTURER, GABLES ENGINEERING, INC., 247 GRECO AVE, CORAL GABLES FL, 33146, APPROVAL/CERTIFICATE# PAH-PMA-PQ1196CE-D, UNDER WO# 873897, DATED 9/1/2015. UPDATED AVTRAK TASKS# 3460553 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 398. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/5/2015 A/C 7702.8 5469 TSMOH 3324.9 8231 INDEX NUMBER 245 ENG 1 7465.3 5337 APU TACH 5213.3 8223 APU TACH ADJ (-) 1888.4 ENG 2 7647.8 5440 APU CYC ADJ (+) 8 APU POST FLIGHT FOUND NO FUEL IN APU FUEL DRAIN CAN AFTER MULTIPLE STARTS. FOUND START FUEL NOZZLE PURGE RESTRICTOR (PN 179290-1) AND START FUEL NOZZLE (PN 4503159) CLOGGED WITH VARNISH AND COKE. REPLACED NOZZLE ASSY AND PURGE RESTRICTOR. APU STARTS AND OPS NORMAL. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF FUEL NOZZLE PURGE RESTRICTOR APU 179290-1 06084597 179290-1 11992864 HOLDER ASSEMBLY 4503159 4503159 NSN 4503159 NSN INSTALLED PARTS OBTAINED FROM GLOBAL PARTS GROUP. START FUEL NOZZLE NEW FROM BEECHCRAFT CORP., 801 INDUSTRIAL BLVD, SUITE 100 GRAPEVINE TX, APPROVAL/CERTIFICATE# ODA-230339-CE, UNDER WO# 0000605779-000010, DATED 8/28/2015. NOZZLE RESTRICTOR OVERHAULED BY INTERCONTINENTAL AVIONIC AND INSTRUMENT CORP., 22 CANFIELD RD, TYLER HILL PA 18469, CRS# OVIR338K UNDER WO# 8257 DATED 5/20/2015. PARTS OFF HAD 5 Y 4 M, 588.1 APU HOURS AND 999 APU CYCLES AT REPLACEMENT. UPDATED AVTRAK TASKS# 4930002 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 399. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 9/21/2015 A/C 7716 5477 TSMOH 3329.8 8240 INDEX NUMBER 246 ENG 1 7478.5 5345 APU TACH 5218.2 8232 APU TACH ADJ (-) 1888.4 ENG 2 7661 5448 APU CYC ADJ (+) 8 REPLACED #1 AND #2 FMS NZ-2000 COMPUTER BATTERY WITH NEW OBTAINED FROM HONEYWELL. COMPUTERS OPERATE NORMALLY. CK'D PITOT STATIC DRAIN TRAPS FOR MOISTURE, NONE NOTED. OK FOR SERVICE. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF NZ-2000 BATTERY #1 7020116-1 NSN 7020116-1 NSN NZ-2000 BATTERY #2 7020116-1 NSN 7020116-1 NSN NZ-2000 BATTERIES FROM HONEYWELL INTERNATIONAL INC, 21111 N. 19TH AVENUE, PHOENIX, AZ 85027. PRODUCTION APPROVAL/CERTIFICATE# PT1254NM, UNDER WO# 109112015, DATED 9/15/2015. UPDATED AVTRAK TASKS# 340002.1 340001.1 340002 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 400. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/8/2015 A/C 7724.9 5485 TSMOH 3334.6 8249 INDEX NUMBER 247 ENG 1 7487.4 5353 APU TACH 5223 8241 APU TACH ADJ (-) 1888.4 ENG 2 7669.9 5456 APU CYC ADJ (+) 8 #2 STARTER GENERATOR GARLOCK SEAL FOUND LEAKING OIL. REPLACED WITH NEW SEAL. LEAK CKS OK. REPLACED #2 STARTER GENERATOR FOR TIME. OVHD INSTALLED UNIT CKS OK. REPLACED #1 AC WILD FREQUENCY GENERATOR FOR TIME. OHD INSTALLED UNIT CKS OK. INSPECTED #1 AND #2 STARTER GENERATOR. REPLACED ELT BATTERY FOR TIME. NEW BATTERY REPLACEMENT DATE 04/2021. CW ANNUAL ELT OP CK PER FAR 91.207(d), CKS OK. UPDATED AVTRAK TASKS 256000 256002 256005 24001.1 240001.2 243006 NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF GARLOCK SEAL #2 3072784-2 NSN 3072784-2 NSN STARTER GENERATOR #2 23080-005 5768 23080-005 2428 WILD FREQ AC GEN #1 BA2801-1 2162 BA2801-1 1304 ELT BATTERY - 452-0133 NSN 452-0133 NSN NEW GARLOCK SEAL OBTAINED FROM HONEYWELL INTERNATIONAL INC, 1944 E. SKY HARBOR CIRCLE, PHOENIX, AZ 85027 UNDER SALES ORDER# 6385431. STARTER GENERATOR OVERHAULED BY DUNCAN AVIATION, LINCOLN AIRPORT, LINCOLN NE 68524 CRS# JGVR194F DATED 4/10/2015. AC GENERATOR OVERHAULED BY CONSOLIDATED AIRCRAFT SUPPLY, 55 RAYNOR AVE, RONKONKOMA, NY 11779, TEL (631) 981-7700 CRS# GI1R167 UNDER WO# 155511 DATED 10/3/2015. NEW ELT BATTERY UNIT OBTAINED FROM KATERNOR INC. 169 54TH ST. BROOKLYN, NY 11220 UNDER ORDER# 1443223. UPDATED AVTRAK TASKS# 340002.1 340001.1 340002 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 401. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 10/14/2015 A/C 7724.9 5485 TSMOH 3334.6 8249 INDEX NUMBER 248 ENG 1 7487.4 5353 APU TACH 5223 8241 APU TACH ADJ (-) 1888.4 ENG 2 7669.9 5456 APU CYC ADJ (+) 8 CW "E" INSPECTION. CW CABIN AND COCKPIT FIRE EXTINGUISHER INSPECTIONS. CW 200 HR LUBRICATION. CW ICA FOR HONEYWELL CDSR SYSTEM TEST. UPDATED AVTRAK TASKS: 050520 262135 262136 340020. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 402. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/2/2015 A/C 7740.7 5496 TSMOH 3343.7 8260 INDEX NUMBER 249 ENG 1 7503.2 5364 APU TACH 5232.1 8252 APU TACH ADJ (-) 1888.4 ENG 2 7685.7 5467 APU CYC ADJ (+) 8 RESEARCHED AD 2015-23-09, CREW OXYGEN MASKS. FOUND NA BY SERIAL NUMBER; CURRENTLY INSTALLED MASK SN'S NOT LISTED IN ZODIAC SB MCF-SBU-35-001 Rev 1, APPENDIX 1. UPDATED AVTRAK TASK: 9990-2015-23-09 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 403. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/15/2015 A/C 7746.7 5501 TSMOH 3345 8266 INDEX NUMBER 250 ENG 1 7509.2 5369 APU TACH 5233.4 8258 APU TACH ADJ (-) 1888.4 ENG 2 7691.7 5472 APU CYC ADJ (+) 8 REPLACED LH INBD AND OUTBD MAIN WHEEL AND TIRE ASSYS FOR NORMAL WEAR PER AMM 32-40-12-401. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF WHEEL ASSY #1 MAIN AHA1814 XB003 AHA1814 LR165 WHEEL ASSY #2 MAIN AHA1814 XB007 AHA1814 SL105 GOODYEAR FLT EAGLE #1 TIRE 237K23-2 40652804 237K23-2 71412957 GOODYEAR FLT EAGLE #2 TIRE 237K23-2 50132801 237K23-2 11412977 INSTALLED WHEELS OVERHAULED BY NORTHCOAST LANDING SYSTEMS, INC, 13005 YORK DELTA DR, UNIT #2, NORTH ROYALTON, OH 44133, CRS L5NR1270 UNDER WO 5486, DATED 7/14/2015. OLD TIRES HAD 160 LANDINGS AT TIRE CHANGE. UPDATED AVTRAK TASK 3200005 & 3200006 THIS LOGBOOK ENTRY IS THE LAST IN XX XXX LLC BINDER #1. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 404. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 12/17/2015 A/C 7746.1 5501 TSMOH 3345.9 8266 INDEX NUMBER 251 ENG 1 7508.6 5369 ENG 2 7691.1 5472 THIS IS THE FIRST ENTRY FOR AIRFRAME LOGBOOK BINDER #2 ADJUSTED APU HOUR METER AND EVENT METER TO REFLECT ACTUAL APU TOTAL TIME AND TOTAL CYCLES. NOTIFIED AVTRAK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 405. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 1/6/2016 A/C 7754.9 5506 TSMOH 3348.5 8271 INDEX NUMBER 252 ENG 1 7517.4 5374 APU TACH 5236.9 8263 APU TACH ADJ (-) 1888.4 ENG 2 7699.9 5477 APU CYC ADJ (+) 8 CW TEST OF CVR ULB DK100, OK FOR SERVICE. REPLACED LH AND RH FIRE BOTTLE GONE INDICATOR FUSES FOR TIME. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF INDICATOR FUSE LH & RH A1003(1) NSN A1003(1) NSN UPDATED AVTRAK TASKS 237012 262009 262010 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 408. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/6/2016 A/C 7766.5 5512 TSMOH 3351.5 8277 INDEX NUMBER 254 ENG 1 7529 5380 ENG 2 7711.5 5483 CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW LH AND RH OXYGEN BOTTLES 5 YEAR HYDROSTATIC TEST REQUIREMENT, SERVICED BOTTLES WITH OXYGEN, LEAK CKS GOOD. BOTH BOTTLES HYDROSTATIC TESTED AT HOOPES FIRE PREVENTION, INC., DOT ID# B905, 124 SANDY DRIVE, NEWARK DE 19713 TEL (302) 323-0220 ON 2-2-2016 UNDER WO# NXXGS . UPDATED AVTRAK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 409. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/8/2016 A/C 7766.5 5512 TSMOH 3351.5 8277 INDEX NUMBER 255 ENG 1 7529 5380 ENG 2 7711.5 5483 FOUND LEAK IN STANDBY STATIC SYSTEM. SPECIAL FLIGHT PERMIT PROCURRED TO REPAIR AIRCRAFT. THIS AIRCRAFT HAS BEEN INSPECTED AND HAS BEEN FOUND SAFE FOR THE INTENDED FLIGHT IN ACCORDANCE WITH SPECIAL FLIGHT PERMIT DATED 2/8/2016. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 410. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/9/2016 A/C 7766.5 5512 TSMOH 3351.5 8277 INDEX NUMBER 256 ENG 1 7529 5380 APU TACH 5239.9 8269 APU TACH ADJ (-) 1888.4 ENG 2 7711.5 5483 APU CYC ADJ (+) 8 INSTALLED TWO CONCORDE RG-390E MAIN BATTERIES PURCHASED NEW FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE, AZUSA, CA 91702, TEL (626) 969-7227. UPDATED AVTRAK MAIN BATT CAP CK AND INSTALL RECORDS, TASKS 241015, 241016, 241021, 241022. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF LH MAIN BATTERY #1 RG-390E 40784520 RG-390E 40562003 RH MAIN BATTERY #2 RG-390E 40785710 RG-390E 40562002 UPDATED AVTRAK TASKS 237012 262009 262010 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 411. Augusta, Georgia Aircraft LogbookEntry XXX Partners Inc. Work Order: 323954 Date: February 12, 2016 Serial Number: 2581XX [NA04XX] Tail Number: NXXGS Model: Hawker 800A ACTT: 7,767.9 LNDS: 5,513 Engine Position: 1 Engine S/N: P-91363 Engine TSN: 7,530.4 Engine Cycles: 5,381 Engine Position: 2 Engine S/N: P-91371 Engine TSN: 7,712.9 Engine Cycles: 5,484 1. C/W the following Maintenance Schedule Out of Phase Inspection items IAW Hawker 800 AFMS: 210001 400 Hour Cooling Turbine-drain and replenish the oil {Mobil Jet II}, Inspect magnetic detector plug. 210006 400 Hour water separator inspection for satisfactory condition. 340013 - 36 Month, Main and standby compass check swing. IAW Hawker 800A AMM 34-23-14. 2. C/W the following MS Life Limited/Component Overhaul Requirements, and tasks IAW Hawker 800 AFMS: 400 Hour-Strobe light intensity check-Tail strobe. 3. Performed the following miscellaneous maintenance: Installed new “S8” drain valve insert p/n 25SF2551-1 with new drain screw p/n MS3212-31L. IAW Hawker 800A AMM 34-00-00, 34-11-19-501. [Reference SB 34-3282]. Installed new “S8” drain body reservoir p/n 25-7SF231. IAW Hawker 800A AMM 34-00-00, 34-11-19-501. o I certify that the Standby static system was tested and inspected and found to comply with Appendix E of FAR 43. Installed new upper Fwd ADF antenna p/n 7510300-901 s/n 1412N357. Removed p/n 7510300-901 s/n 04118911 in accordance with Hawker 800A AMM 34-51-05. Installed new upper Aft ADF antenna p/n 7510300-901 s/n 1507N865. Removed p/n 7510300-901 s/n 88100194 in accordance with Hawker 800A AMM 34-51-05. Installed Repaired #2 Flux detector p/n 7010133 s/n 97123920 in accordance with Hawker 800A AMM 34-20-15-501. Removed p/n 7010133 s/n 98054125. Unit repaired by Honeywell International under work order 274278 dated Aug 24 2012. Swapped Compass controller/compensators sides. Controller P/N: 7004545-902 s/n: 88110550 moved to #2 side and S/N: 88110552 moved to #1 side. All maintenance performed on this aircraft was performed in accordance with the current regulations of the Federal Aviation Administration and is approved for return to service with respect to the work performed. Details on file on W/O #: 323954. Date 02/12/2016 Signed: Chris Mann for , CRS# GW4R221M, Augusta, Ga. 30906
- 412. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 2/14/2016 A/C 7769.1 5514 TSMOH 3352.3 8279 INDEX NUMBER 257 ENG 1 7531.6 5382 APU TACH 5240.7 8271 APU TACH ADJ (-) 1888.4 ENG 2 7714.1 5485 APU CYC ADJ (+) 8 DURING COMPASS SWING ON 2/12/2016 STANDARDAERO TECHS NOTED #2 HEADING ANOMOLIES THAT POINTED TO THE #2 AHARS HAVING AN INTERMITTENT HEADING DRIFT. REPLACED #2 AHARS UNIT AS PRECAUTIONARY MEASURE. NEW UNIT OK FOR SERVICE. CW CAPACITY CK OF RG-126 #3, #4 AND #5 EMERGENCY BATTERIES. OK FOR SERVICE. INSTALLED SN 40636579 IN #3 POSITION, SN 40636573 IN #4 POSITION AND SN 40636584 IN #5 POSITION. CW CAPACITY CK OF RG-131 IRU EMERGENCY BATTERY. OK FOR SERVICE UPDATED AVTRAK TASKS 3460522 241017 241018 241019 241030 NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF AH-600 ATTITUDE AND HEADING REFERENCE UNIT #2 7003360-943 95043143 7003360-943 89071429 REPAIRED AHARS UNIT OBTAINED FROM HONEYWELL , 7227 W. HARRY, WICHITA, KS 67209, CRS# LV2R992K UNDER WO# 321642311 DATED 1/16/2016. AHARS OFF HAD 195.8 HOURS AND 140 CYCLES AT REPLACEMENT. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 413. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/17/2016 A/C 7799 5523 TSMOH 3357 8292 INDEX NUMBER 258 ENG 1 7561.5 5391 APU TACH 5245.4 8284 APU TACH ADJ (-) 1888.4 ENG 2 7744 5494 APU CYC ADJ (+) 8 COMPLETED 191-240 HOUR THRUST REVERSER INSPECTION PER NORDAM TR5000 MM. REPLACED APU FIRE BOTTLE & APU FWD AND AFT FIRE BOTTLE CARTRIDGES IAW AMM 26-20-54 FOR TIME. OK FOR SERVICE. FWD & AFT FIRE BOTTLE SQUIB MFG DATE OF 10/15. UPDATED AVTRAK TASKS 781021 781022 262127 262139 262002.3 262002.4 NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF APU FIRE EXTINGUISHER APU 30402104 B-5143 30402104 20376B2 APU FIRE EXTINGUISHER CARTRIDGE FWD AE13083-5 NSN M13083-5 23706 APU FIRE EXTINGUISHER CARTRIDGE AFT AE13083-5 NSN M13083-5 23693 APU FIRE EXTINGUISHER BOTTLE ASSY OH'D BY AEROSPACE TURBINE ROTABLES, 1919 E. NORTHERN ST, WICHITA, KS 67216 TEL (316) 943-6100 CRS# NV2R045L UNDER WO# WO85319 DATED 03/03/2016. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 414. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 3/30/2016 A/C 7803.7 5526 TSMOH 3359.3 8296 INDEX NUMBER 259 ENG 1 7566.2 5394 ENG 2 7748.7 5497 REPLACED RG-131 IRS BATTERY WITH NEW. UPDATED AVTRAK TASK 241030. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF IRU BATTERY - RG-131 40781145 RG-131 40633504 INERTIAL REFERENCE BATTERY ASSY PURCHASED NEW FROM ADVANCED POWER PRODUCTS, 955 N. TODD AVE, AZUSA, CA 91702, TEL (626) 969-7227. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 415. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 5 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/1/2016 A/C 7803.7 5526 TSMOH 3359.3 8296 INDEX NUMBER 260 ENG 1 7566.2 5394 ENG 2 7748.7 5497 CW VISUAL INSPECTION OF PANEL GG TERMINAL BLOCK M PER 400 HOUR REQUIREMENT. NO FAULTS NOTED. CW 150-200 HR AND 300-400 HR INSPECTIONS ON #1 AND #2 ENGINES PER HONEYWELL MM 72-00-00 INCLUDING CHIP DETECTOR CHECK, REPLACEMENT OF ENGINE OIL FILTER AND S.O.A.P. SAMPLING ON #1 AND #2 ENGINES IAW HONEYWELL AMM 79-20-03 AND 79-20-01. RAN ENGINES, LEAK CKS OK. SOAP SAMPLES SENT TO JET CARE FOR ANALYSIS. SERVICED BOTH ENG OIL LEVELS TO FULL. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF ENG OIL FILTERS #1 & #2 3070945-1 LOT# 2013C16822 DM10764307 3070945-1 NSN UPDATED AVTRAK TASKS 240029 057120 057110 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 416. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/5/2016 A/C 7803.7 5526 TSMOH 3359.3 8296 INDEX NUMBER 261 ENG 1 7566.2 5394 ENG 2 7748.7 5497 RESEARCHED AD 2016-07-02 FOUND TO BE NA AT THIS TIME; LH AND RH ENG ITT DUCT SERIAL NUMBERS DO NOT MATCH ANY LISTED IN HONEYWELL SB TFE731-72-3789 REV 0 TABLE 2. UPDATED AVTRAK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 417. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/8/2016 A/C 7803.7 5526 TSMOH 3359.3 8296 INDEX NUMBER 262 ENG 1 7566.2 5394 ENG 2 7748.7 5497 REPLACED FUEL FILTERS ON #1 AND #2 ENGINES PER 650 HOUR TIME REQUIREMENT PER HONEYWELL MM 73-21-02. RAN ENGINES, LEAK CKS OK.. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF ENG FUEL FILTERS #1 & #2 897830-1 LOT# 880451 897830-1 NSN UPDATED AVTRAK TASKS 731120 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 418. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 4/28/2016 A/C 7814.6 5535 TSMOH 3364.1 8306 INDEX NUMBER 263 ENG 1 7577.1 5403 ENG 2 7759.6 5506 REPLACED FAILED LH CABIN UPWASH FLUORESCENT LIGHTING INVERTER. CKS OK. REPLACED 3 FAILED FORWARD RH CABIN LIGHTING FLUORESCENT OVERWINDOW LAMPS. CKS OK. NOMENCLATURE POSITION P/N ON S/N ON P/N OFF S/N OFF LIGHTING INVERTER ASSY UPPER LH 18-996 6429 18-996 5178 FLUORESCENT BULBS RH #1, #2, #3 WINDOW N1235320 NSN AL-1235-T-320 NSN UPDATED AVTRAK TASK 3300559 INSTALLED INVERTER OBTAINED FROM DODSON INTERNATIONAL, 2155 VERMONT RD, RANTOUL KS 66079 TEL (785) 878-8000 IN "SERVICEABLE, AS REMOVED" CONDITION. INSTALLED FLORO LAMPS OBTAINED NEW FROM AIRCRAFT LIGHTING INTERNATIONAL, 45 EDISON AVE # B, WEST BABYLON, NY 11704 TEL (631) 474-2254 ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 419. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/15/2016 A/C 7815.6 5536 TSMOH 3366.2 8310 INDEX NUMBER 264 ENG 1 7578.1 5404 ENG 2 7760.6 5507 RESEARCHED AD 2016-11-20 FOUND TO BE NA AT THIS TIME BY PART NUMBER. UPDATED AVTRAK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 420. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 6/17/2016 A/C 7815.6 5536 TSMOH 3366.2 8310 INDEX NUMBER 265 ENG 1 7578.1 5404 ENG 2 7760.6 5507 REPLACED AND CHECKED FWD AND AFT EMERGENCY EXIT POWER SUPPLY “D” CELL NI-CAD BATTERIES WITH NEW, 2 EACH PER BATTERY PACK, PN AD-4002P, NSN, BATCH NUMBER AAKO-883. BATTERIES OBTAINED FROM MFG’R, AREO DESIGN, INC, 385 INDUSTRIAL DR, MT. JULIET, TN, 37122, PH 800- 551-1158, PRODUCTION APPROVAL HOLDER No. (PAH#) PQ1465CE, FORM TRACKING# STN00036341, DATED 6/15/16. UPDATED AVTRAK 335010. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 421. XX XXX LLC MAINTENANCELOG RECORD AIRCRAFT REG NXXGS LH ENGINE SERIAL P91363 RH ENGINE SERIAL P91371 AIRCRAFT SERIAL 2581XX APU SERIAL 877641 APU TYPE T-62-40C8D1 AIRCRAFT TYPE BAe 125-800A ENGINE TYPE TFE731-5R-1H FORM VER 6 TOTAL LDGS APU HRS CYCLES EVENT DATE 7/19/2016 A/C 7823.1 5546 TSMOH 3369 8313 INDEX NUMBER 266 ENG 1 7585.6 5414 ENG 2 7768.1 5517 CW APU SEMI-ANNUAL/125 HR/250 CYCLE INSPECTION AVTRAK TASK 492001 CW APU SEMI-ANNUAL/250 HR/500 CYCLE MAINTENANCE AVTRAK TASK 492002 CW APU ANNUAL/500 HR/1000 CYCLE MAINTENANCE AVTRAK TASK 492003 CW APU ANNUAL/1000 HR/2000 CYCLE MAINTENANCE AVTRAK TASK 492004. CW APU BIENNIAL/1500 HR/3000 CYCLE MAINTENANCE AVTRAK TASK 492005. DRAINED AND SERVICED APU OIL WITH MOBIL 254. REPLACED APU OIL FILTER ELEMENT WITH NEW DONALDSON/WESTERN FILTER, PN WF331667 (ALT PN FOR SUNDSTRAND 179411). CLEANED APU FUEL INLET FILTER PN 211-326, REPLACED PN 3500AS12 CRUSH GASKET (DONALDSON/WESTERN FILTER). APU LEAK AND OP CKS OK. ALL MAINTENANCE PERFORMED ON THIS AIRCRAFT WAS PERFORMED IAW THE CURRENT REGULATIONS OF THE FEDERAL AVIATION ADMINISTRATION AND IS APPROVED FOR RETURN TO SERVICE WITH RESPECT TO THE WORK PERFORMED. SIGNATURE: CERTIFICATE NO. A&P 3357851 GREGORY A. STULTZ
- 422. ● Jet EastCorporate Aviation, LLC ● TRENTON-MERCER AIRPORT ● TRENTON, NJ 08628 ● Phone (215)-937-9020 ● Fax (609)-600-1718 REG # NXXGS DATE: 8/29/2016 MAKE: HAWKER W/O #: 16TR72247 MODEL: 800A CYC: 5552 AIRFRAME LOG S/N: 2581XX TT: 7835.2 COMPLIED WITH THE FOLLOWING CAMP INSPECTION CODES 1. 050130 COMPLIED WITH INSPECTION B (B1 THRU B12) WORK DONE IAW HAWKER 800A AFMS 050130 2. 050520 COMPLIED WITH INSPECTION E (E1 THRU E12) WORK DONE IAW HAWKER 800A AFMS 050520 3. 050650 COMPLIED WITH INSPECTION F (F1 THRU F12) WORK DONE IAW HAWKER 800A AFMS 050650 4. 050780 COMPLIED WITH INSPECTION G WORK DONE IAW HAWKER 800A AFMS 050780 5. 050790 COMPLIED WITH 400 HOUR LUBRICATION WORK DONE IAW HAWKER 800A AFMS 050790 6. 050800 COMPLIED WITH 400 HOUR DETAILED WALK-AROUND INSPECTION WORK DONE IAW HAWKER 800A AFMS 050800 7. 212015 COMPLIED WITH BENCH CHECK-DUCT TEMP OVERHEAT SWITCHES WORK DONE IAW HAWKER 800A AFMS 212015 8. 320032.1 COMPLIED WITH INSPECTION – LEFT MAIN GEAR FAIRING STRUT (X-RAY) ACCOMLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 320032 9. 320032.2 COMPLIED WITH INSPECTION – RIGHT MAIN GEAR FAIRING STRUT (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 320032 10. 342561 COMPLIED WITH INSPECTING UNDER UPPER AND LOWER TCAS ANTENNAS PER STC-ST00302WI, DOCUMENT ICA #44504900. 11. 351008 COMPLIED WITH OVERHAUL – B/E AEROSPACE/PURITAN BENNETT PASSENGER OXYGEN MASKS WORK DONE IAW HAWKER 800A AFMS 351008 12. 510001 COMPLIED WITH INSPECTION – NOSE GEAR BAY SIDEWALLS (EDDY CURRENT) WORK DONE IAW HAWKER 800A AFMS 510001 13. 510003 COMPLIED WITH INSPECTION – FLIGHT COMPARTMENT SKIN/WINDOW (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 510003 14. 510009 COMPLIED WITH INSPECTION – ENTRY DOOR SURROUND (BOROSCOPE) WORK DONE IAW HAWKER 800A AFMS 510009 15. 520008 COMPLIED WITH INSPECTION – MAIN ENTRY DOOR STRUCTURAL (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 520008 16. 530001 COMPLIED WITH INSPECTION – SKIN EXTERIOR UNDER DORSAL INTAKE, FORWARD OF FRAME 19 WORK DONE IAW HAWKER 800A AMFS 530001 17. 530002 COMPLIED WITH INSPECTION - FUSELAGE SKIN UNDER WING FAIRINGS (BOROSCOPE) WORK DONE IAW HAWKER 800A AFMS 530002 18. 530003 COMPLIED WITH INSPECTION – WING FUSELAGE ATTACH LINKS, BRACKETS AND BOLTS (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 530003 19. 530011 COMPLIED WITH INSPECTION – LEFT FRONT FACE REAR PRESSURE BULKHEAD (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 530011 20. 550006.1 COMPLIED WITH INSPECTION – LEFT ELEVATOR INTERNAL (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 55006 PAGE 1 OF 3
- 423. ● Jet EastCorporate Aviation, LLC ● TRENTON-MERCER AIRPORT ● TRENTON, NJ 08628 ● Phone (215)-937-9020 ● Fax (609)-600-1718 REG # NXXGS DATE: 8/29/2016 MAKE: HAWKER W/O #: 16TR72247 MODEL: 800A CYC: 5552 AIRFRAME LOG S/N: 2581XX TT: 7835.2 COMPLIED WITH THE FOLLOWING CAMP INSPECTION CODES 21. 550006.2 COMPLIED WITH INSPECTION – RIGHT ELEVATOR INTERNAL (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 550006 22. 550007.1 COMPLIED WITH INSPECTION – LEFT ELEVATOR (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 550007 23. 550007.2 COMPLIED WITH INSPECTION – RIGHT ELEVATOR (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 550007 24. 550008.1 COMPLIED WITH INSPECTION – LEFT ELEVATOR TRIM TAB CONNECTION RODS (INSPECT/LUBRICATE) WORK DONE IAW HAWKER 800A AFMS 550008 25. 550008.2 COMPLIED WITH INSPECTION – RIGHT ELEVATOR TRIM TAB CONNECTION RODS (INSPECT/LUBRICATE) WORK DONE IAW HAWKER 800A AFMS 550008 26. 550009 COMPLIED WITH INSPECTION – RUDDER (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 550009 27. 550010 COMPLIED WITH INSPECTION – RUDDER TRIM AND ANTI-SERVO TAB CONNECTING RODS (INSPECT/LUBRICATE) IAW HAWKER 800A AFMS 550010 28. 550011 COMPLIED WITH INSPECTION – RUDDER INTERNAL (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 550011 29. 550015 COMPLIED WITH INSPECTION – ELEVATOR MASS BALANCE WEIGHTS, SPIGOTS AND ATTACHMENTS (DETAILED VISUAL) WORK DONE IAW 800A AFMS 550015 30. 570007.1 COMPLIED WITH INSPECTION – LEFT WING BOTTOM SKINS/STRINGERS (X- RAY) ACCOMLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 570007 31. 570007.2 COMPLIED WITH INSPECTION – RIGHT WING BOTTOM SKINS/STRINGERS (X- RAY) ACCOMLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 570007 32. 570008.1 COMPLIED WITH INSPECTION – LEFT LANDING GEAR AND SIDESTAY ATTACHMENT FITTINGS (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570008 33. 570008.2 COMPLIED WITH INSPECTION – RIGHT LANDING GEAR AND SIDESTAY ATTACHMENT FITTINGS (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570008 34. 570010.1 COMPLIED WITH INSPECTION – LH WING BOTTOM SKIN ADJACENT TO FLAP OUTBOARD HINGE AT RIB 8 WORK DONE IAW HAWKER 800A AFMS 570010 – API* 35. 570010.2 COMPLIED WITH INSPECTION – RH WING BOTTOM SKIN ADJACENT TO FLAP OUTBOARD HINGE AT RIB 8 WORK DONE IAW HAWKER 800A AFMS 570010 – API* 36. 570012.1 COMPLIED WITH INSPECTION – LH WING REAR SPAR, REAR FACE WORK DONE IAW HAWKER 800A AFMS 570012 – API* 37. 570012.2 COMPLIED WITH INSPECTION – RH WING REAR SPAR, REAR FACE WORK DONE IAW HAWKER 800A AFMS 570012 – API* 38. 570013.3 COMPLIED WITH INSPECTION – LEFT AIRBRAKE (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570013 39. 570013.4 COMPLIED WITH INSPECTION – RIGHT AIRBRAKE (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570013 PAGE 2 OF 3
- 424. ● Jet EastCorporate Aviation, LLC ● TRENTON-MERCER AIRPORT ● TRENTON, NJ 08628 ● Phone (215)-937-9020 ● Fax (609)-600-1718 REG # NXXGS DATE: 8/29/2016 MAKE: HAWKER W/O #: 16TR72247 MODEL: 800A CYC: 5552 AIRFRAME LOG S/N: 2581XX TT: 7835.2 COMPLIED WITH THE FOLLOWING CAMP INSPECTION CODES 40. 570014.3 COMPLIED WITH INSPECTION – LEFT AILERON INTERNAL (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 570014 41. 570014.4 COMPLIED WITH INSPECTION – RIGHT AILERON INTERNAL (X-RAY) ACCOMLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 570014 42. 570015.1 COMPLIED WITH INSPECTION – LEFT AILERON (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570015 43. 570015.2 COMPLIED WITH INSPECTION – RIGHT AILERON (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570015 44. 570016.1 COMPLIED WITH INSPECTION – LEFT AILERON TRIM AND SERVO TABS CONNECTING RODS (LUBRICATE) WORK DONE IAW HAWKER 800A AFMS 570016 45. 570016.2 COMPLIED WITH INSPECTION – RIGHT AILERON TRIM AND SERVO TABS CONNECTING RODS (LUBRICATE) WORK DONE IAW HAWKER 800A AFMS 570016 46. 570017.3 COMPLIED WITH INSPECTION – LEFT FLAP AND FLAP VANE (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 570017 47. 570017.4 COMPLIED WITH INSPECTION – RIGHT FLAP AND FLAP VANE (X-RAY) ACCOMPLISHED BY STRUCTURAL TESTING SYSTEMS WORK ORDER# 12861 WORK DONE IAW HAWKER 800A AFMS 570017 48. 570027.1 COMPLIED WITH INSPECTION – LEFT WING LEADING EDGE (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570027 49. 570027.2 COMPLIED WITH INSPECTION – RIGHT WING LEADING EDGE (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570027 50. 570030.1 COMPLIED WITH INSPECTION – LEFT AILERON AT OUTBOARD HINGE CASTING (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570030 51. 570030.2 COMPLIED WITH INSPECTION-RIGHT AILERON AT OUTBOARD HINGE CASTING (DETAILED VISUAL) WORK DONE IAW HAWKER 800A AFMS 570030 REPLACED THE FOLLOWING SERIALIZED COMPONENTS 1. REMOVED LH WINDSHIELD P/N NF.24016-415 ISS.2, S/N L171139, INSTALLED NEW WINDSHIELD P/N NF.24016-415 ISS.2, S/N L437357, DOM FEB, 2016. WORK DONE IAW HAWKER 800A AMM 56-10-11 2. REINSTALLED #1 LH LEADING EDGE TKS PANEL P/N 25-8WS1513-23, S/N T87L31, AFTER OVERHAUL WORK DONE IAW HAWKER 800A AMM 30-10-72 PERFORMED THE FOLLOWING REPAIRS 1. COMPLIED WITH REPLACEMENT OF MED SPRINGS WORK DONE IAW HAWKER 800A AMM 52-11-11. INSTALLED (4) NEW SPRINGS P/N N2441 .DOT3. 2. REMOVED CORROSION AND TREATED WING SKINS AT L&R WINGLETS, REPAIRED RH LOWER WING SKIN IAW AVIATION PARTNERS INC. (API) ENGINEERING SERVICE RESPONSE LETTER# SRH-16-2016, DATED 8-16-16 PAGE 3 OF 3 I certify that this aircraft has been inspected and repaired and determined to be in airworthy condition and return to service. Pertinent details of the inspection are on file at this agency under the work order number shown above. Signed______________________________ for Jet East Corporate Aviation, LLC CRSJ21R713Y