Emergency Airworthiness Directive (AD) 2014-25-52 is sent to owners and operators of Airbus Model A330-200 Freighter, -200, and -300 series airplanes and Model A340-200, -300, -500, and -600 series airplanes.
Emergency Airworthiness Directive (AD) 2014-26-53 is sent to owners and operators of Airbus Model A319-115, A319-133, A320-214, A320-232, and A320-233 airplanes.
Qantas repair - Presentation Transcript
VH-OJH INCIDENT 23 SEPTEMBER 1999 PETER THOMAS OJH PROJECT COORDINATOR
THE FIRST DAY
VH-OJH left the end of RWY 21L at BKK INTERNATIONAL AIRPORT on the night of 23 SEPTEMBER 1999. The A/C travelled a further 200 metres across the RWY run-off area.
On its way the A/C collided with the RWY 03R Localiser Antenna before coming to rest in a RWL position.
pth13: Localiser Antenna
pth13: “ The Day After”
pth13: No.3 Pylon pth13: Note failure of Diagonal Brace “end fitting”
pth13: Golf Course Road
THE RECOVERY
The importance of keeping the “Station Aircraft Recovery List” updated, including checking Emergency Contacts and Equipment Suppliers phone numbers.
An assistant is required to keep notes during the initial Recovery planning period.
pth13: Construction of a road to return to RWY 21L.
pth13: Road constructed to allow unloading of aft cargo and parking of crane.
pth13: Stabilising R/H wing to prevent A/C movement.
pth13: Fuselage damage due to ingress of NLG Assy.
pth13: “ Classic” failure of R/H WLG.
ARRIVAL OF PARTS
To ensure swift delivery of Parts, Materials and Tooling a Custom’s Agent must be engaged who has contacts at the HIGHEST LEVELS”. Arranging a “Custom’s Carnet” is of utmost importance to overcome “heavy” Customs Duties.
To ensure these deliveries are completed with the utmost promptness, cooperation with all levels of the Airport Authority is required.
INCIDENT SITE SCRAP
All scrap had to be collected for documentation.
To conform to “Customs” regulations all parts and raw materials movements had to be thoroughly documented and presented to the Authorities for approval so as not to incur large Customs duties. This procedure was also required for all scrap material.
JANUARY 23 2000 REPAIR BEGINS
The Boeing Team begins the repair by first stabilising and “jigging” the Aircraft to prevent fuselage movement during the removal of the lower sections of Sections41 and 42.
pth13: A/C was “tied” to the tail jack and the jack was cabled to the ground. Jack point was “drilled” to allow fitment of a rod between the jack adaptor and the jack point.
pth13: Installation of “Tower Jacks”
pth13: Fuselage “stabilisation” complete.
AIRCRAFT REPAIR BEGINS
Removal of Section 41 and 42 begins.
Replacement of the damaged “window-belt” has to be done before removal of the lower Section 41. This is to ensure the alignment of the Aircraft is maintained.
pth13: “ Window belt” repair.
pth13: No.3 Pylon repair.
pth13: “ Wiring pull-back”
pth13: “ Wiring pull-back” completed.
pth13: Sections 41/42 removed.
pth13: “ Aligning Sect.41.
pth13: Installation of Sect.42 “plug”.
pth13: “ Final Alignment”
pth13: Skin “finish” after repair.
STORES PERSONNEL
A team of Stores Personnel was required to acquit all the Parts demands and to administer a Parts store to ensure a “smooth” production flow is maintained.
Boeing were ordering “hundreds” of parts daily from Seattle and expecting 2 days delivery at the site.
pth13: Mick Gledhill
DOCUMENTING AND CERTIFICATION
To lessen the impact of the “cost” of the repair to QANTAS a lot of rotable parts were supplied by QANTAS. The Insurance Company will only pay “Market Price” for these parts.
A Team of LAME’s were needed to document and certify these parts as a lot of the Parts were delivered straight from the Vendor. This included all the Landing Gear assembly’s.
pth13: Mark Coffey
pth13: First Engine installed by QANTAS LAME’s
pth13: Zones 1 & 2 rework by QANTAS.
pth13: A “few” of the 300+ F/G repairs to the L/E.
HI - BLOW TEST
“ Seats” all the rivets and frame joints.
Exposes any fuselage skin joints leakage.
Fuselage blown to 12.5 psid.
pth13: “ Hi-Blow” relief vlv.
ROLL-OUT AFTER REPAIR
Rollout from Hangar after approx. 6 months.
Due to publicity sensitivity the A/C had t
Emergency Airworthiness Directive (AD) 2014-25-52 is sent to owners and operators of Airbus Model A330-200 Freighter, -200, and -300 series airplanes and Model A340-200, -300, -500, and -600 series airplanes.
Emergency Airworthiness Directive (AD) 2014-26-53 is sent to owners and operators of Airbus Model A319-115, A319-133, A320-214, A320-232, and A320-233 airplanes.
Qantas repair - Presentation Transcript
VH-OJH INCIDENT 23 SEPTEMBER 1999 PETER THOMAS OJH PROJECT COORDINATOR
THE FIRST DAY
VH-OJH left the end of RWY 21L at BKK INTERNATIONAL AIRPORT on the night of 23 SEPTEMBER 1999. The A/C travelled a further 200 metres across the RWY run-off area.
On its way the A/C collided with the RWY 03R Localiser Antenna before coming to rest in a RWL position.
pth13: Localiser Antenna
pth13: “ The Day After”
pth13: No.3 Pylon pth13: Note failure of Diagonal Brace “end fitting”
pth13: Golf Course Road
THE RECOVERY
The importance of keeping the “Station Aircraft Recovery List” updated, including checking Emergency Contacts and Equipment Suppliers phone numbers.
An assistant is required to keep notes during the initial Recovery planning period.
pth13: Construction of a road to return to RWY 21L.
pth13: Road constructed to allow unloading of aft cargo and parking of crane.
pth13: Stabilising R/H wing to prevent A/C movement.
pth13: Fuselage damage due to ingress of NLG Assy.
pth13: “ Classic” failure of R/H WLG.
ARRIVAL OF PARTS
To ensure swift delivery of Parts, Materials and Tooling a Custom’s Agent must be engaged who has contacts at the HIGHEST LEVELS”. Arranging a “Custom’s Carnet” is of utmost importance to overcome “heavy” Customs Duties.
To ensure these deliveries are completed with the utmost promptness, cooperation with all levels of the Airport Authority is required.
INCIDENT SITE SCRAP
All scrap had to be collected for documentation.
To conform to “Customs” regulations all parts and raw materials movements had to be thoroughly documented and presented to the Authorities for approval so as not to incur large Customs duties. This procedure was also required for all scrap material.
JANUARY 23 2000 REPAIR BEGINS
The Boeing Team begins the repair by first stabilising and “jigging” the Aircraft to prevent fuselage movement during the removal of the lower sections of Sections41 and 42.
pth13: A/C was “tied” to the tail jack and the jack was cabled to the ground. Jack point was “drilled” to allow fitment of a rod between the jack adaptor and the jack point.
pth13: Installation of “Tower Jacks”
pth13: Fuselage “stabilisation” complete.
AIRCRAFT REPAIR BEGINS
Removal of Section 41 and 42 begins.
Replacement of the damaged “window-belt” has to be done before removal of the lower Section 41. This is to ensure the alignment of the Aircraft is maintained.
pth13: “ Window belt” repair.
pth13: No.3 Pylon repair.
pth13: “ Wiring pull-back”
pth13: “ Wiring pull-back” completed.
pth13: Sections 41/42 removed.
pth13: “ Aligning Sect.41.
pth13: Installation of Sect.42 “plug”.
pth13: “ Final Alignment”
pth13: Skin “finish” after repair.
STORES PERSONNEL
A team of Stores Personnel was required to acquit all the Parts demands and to administer a Parts store to ensure a “smooth” production flow is maintained.
Boeing were ordering “hundreds” of parts daily from Seattle and expecting 2 days delivery at the site.
pth13: Mick Gledhill
DOCUMENTING AND CERTIFICATION
To lessen the impact of the “cost” of the repair to QANTAS a lot of rotable parts were supplied by QANTAS. The Insurance Company will only pay “Market Price” for these parts.
A Team of LAME’s were needed to document and certify these parts as a lot of the Parts were delivered straight from the Vendor. This included all the Landing Gear assembly’s.
pth13: Mark Coffey
pth13: First Engine installed by QANTAS LAME’s
pth13: Zones 1 & 2 rework by QANTAS.
pth13: A “few” of the 300+ F/G repairs to the L/E.
HI - BLOW TEST
“ Seats” all the rivets and frame joints.
Exposes any fuselage skin joints leakage.
Fuselage blown to 12.5 psid.
pth13: “ Hi-Blow” relief vlv.
ROLL-OUT AFTER REPAIR
Rollout from Hangar after approx. 6 months.
Due to publicity sensitivity the A/C had t
Final project report on grocery store management system..pdfKamal Acharya
In today’s fast-changing business environment, it’s extremely important to be able to respond to client needs in the most effective and timely manner. If your customers wish to see your business online and have instant access to your products or services.
Online Grocery Store is an e-commerce website, which retails various grocery products. This project allows viewing various products available enables registered users to purchase desired products instantly using Paytm, UPI payment processor (Instant Pay) and also can place order by using Cash on Delivery (Pay Later) option. This project provides an easy access to Administrators and Managers to view orders placed using Pay Later and Instant Pay options.
In order to develop an e-commerce website, a number of Technologies must be studied and understood. These include multi-tiered architecture, server and client-side scripting techniques, implementation technologies, programming language (such as PHP, HTML, CSS, JavaScript) and MySQL relational databases. This is a project with the objective to develop a basic website where a consumer is provided with a shopping cart website and also to know about the technologies used to develop such a website.
This document will discuss each of the underlying technologies to create and implement an e- commerce website.
Final project report on grocery store management system..pdfKamal Acharya
In today’s fast-changing business environment, it’s extremely important to be able to respond to client needs in the most effective and timely manner. If your customers wish to see your business online and have instant access to your products or services.
Online Grocery Store is an e-commerce website, which retails various grocery products. This project allows viewing various products available enables registered users to purchase desired products instantly using Paytm, UPI payment processor (Instant Pay) and also can place order by using Cash on Delivery (Pay Later) option. This project provides an easy access to Administrators and Managers to view orders placed using Pay Later and Instant Pay options.
In order to develop an e-commerce website, a number of Technologies must be studied and understood. These include multi-tiered architecture, server and client-side scripting techniques, implementation technologies, programming language (such as PHP, HTML, CSS, JavaScript) and MySQL relational databases. This is a project with the objective to develop a basic website where a consumer is provided with a shopping cart website and also to know about the technologies used to develop such a website.
This document will discuss each of the underlying technologies to create and implement an e- commerce website.
Industrial Training at Shahjalal Fertilizer Company Limited (SFCL)MdTanvirMahtab2
This presentation is about the working procedure of Shahjalal Fertilizer Company Limited (SFCL). A Govt. owned Company of Bangladesh Chemical Industries Corporation under Ministry of Industries.
NO1 Uk best vashikaran specialist in delhi vashikaran baba near me online vas...Amil Baba Dawood bangali
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Hierarchical Digital Twin of a Naval Power SystemKerry Sado
A hierarchical digital twin of a Naval DC power system has been developed and experimentally verified. Similar to other state-of-the-art digital twins, this technology creates a digital replica of the physical system executed in real-time or faster, which can modify hardware controls. However, its advantage stems from distributing computational efforts by utilizing a hierarchical structure composed of lower-level digital twin blocks and a higher-level system digital twin. Each digital twin block is associated with a physical subsystem of the hardware and communicates with a singular system digital twin, which creates a system-level response. By extracting information from each level of the hierarchy, power system controls of the hardware were reconfigured autonomously. This hierarchical digital twin development offers several advantages over other digital twins, particularly in the field of naval power systems. The hierarchical structure allows for greater computational efficiency and scalability while the ability to autonomously reconfigure hardware controls offers increased flexibility and responsiveness. The hierarchical decomposition and models utilized were well aligned with the physical twin, as indicated by the maximum deviations between the developed digital twin hierarchy and the hardware.
Welcome to WIPAC Monthly the magazine brought to you by the LinkedIn Group Water Industry Process Automation & Control.
In this month's edition, along with this month's industry news to celebrate the 13 years since the group was created we have articles including
A case study of the used of Advanced Process Control at the Wastewater Treatment works at Lleida in Spain
A look back on an article on smart wastewater networks in order to see how the industry has measured up in the interim around the adoption of Digital Transformation in the Water Industry.
1. ATA 52 Information Group EASA 2022-0090 Date 18-05-2022
Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism –
Inspection
Applicability : A321 aero planes
Affected Part : Doors – Airbus Cabin Flex / Over wing Emergency Exit Slide
Back Ground :
During an emergency slide deployment test on an A321NEO Airbus Cabin Flex (ACF) over wing
emergency exit, the slide did not deploy. Investigation identified that the slide release mechanism cable
junction was disconnected inside the surrounding collets and knurled sleeve nut.
The mushroom head connector was not inserted into the T-slot cable joint. This condition, if not
detected and corrected, could prevent emergency slide deployment, possibly resulting in injury to
occupants during an emergency evacuation.
2. ATA 52 Information Group EASA 2022-0090 Date 18-05-2022
Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism –
Inspection
To address this potential unsafe condition, Airbus issued the AOT, providing instructions to inspect
the slide release mechanism cable lock wire and junction and the associated corrective actions.
For the reasons described above, this AD requires a one-time detailed inspection (DET) of the
installation of the ACF over wing emergency exit slide release mechanism on both left-hand (LH)
and right-hand (RH) sides of the fuselage.
Applicability:
For all A321 aero planes, within 4 months after 01 June 2022, accomplish a DET of the slide
release mechanism cable lock wire and junction of each ACF over wing emergency exit, on both
LH and RH sides, in accordance with the instructions of the AOT.
3. ATA 52 Information Group EASA 2022-0090 Date 18-05-2022
Subject Doors – Airbus Cabin Flex / Overwing Emergency Exit Slide Release Mechanism –
Inspection
Objective/Action:
During the DET, if any discrepancies are detected, as defined in the AOT, accomplish the applicable
corrective action(s) within the compliance time as defined in, and in accordance with the
instructions of, the AOT.
Ref. Publications: Airbus AOT A52N014-22 original issue dated 21 March 2022, or Revision 01 dated 19
April 2022.
