O documento descreve o sistema de ar condicionado de uma aeronave B727-200, incluindo os packs de resfriamento, controle de temperatura e distribuição de ar. Os packs de resfriamento fornecem ar frio e quente através de trocadores de calor e unidades de ar frio para manter a temperatura adequada nas cabines. O sistema controla a mistura desse ar e também aquece os compartimentos de carga.
This document provides training material on flight controls for the Boeing 727-200. It describes the primary and auxiliary flight control surfaces including ailerons, elevators, rudders, flaps, and spoilers. It also summarizes the hydraulic and electrical systems used to power and control these surfaces. The document is intended solely for training and may not be distributed outside the client organization without permission.
This document provides a description and overview of the autopilot and yaw damper system for a B727-200 aircraft. It describes the major components, including the Sperry SP-50 MB V Automatic Flight Control System, which provides three-axis flight stabilization and automatic approach capability. It details the functions of the yaw, roll, and pitch axes, and describes the components that control and provide inputs to each axis, such as rudder power units, aileron servos, elevator power units, and sensors. The document also notes the locations of components throughout the aircraft.
This document provides a summary of instrument panels and systems on a Boeing 727-200 aircraft. It describes the layout of the main instrument panels used by pilots and crew. It also provides details on the types of instrument indicators and how they are mounted. The document then summarizes several key aircraft systems including the flight data recorder, clocks, and aural warning system. It explains the components and functions of these systems.
The document provides training material on landing gear for the B727-200 aircraft. It describes the landing gear components and systems, including the main and nose gears, retraction/extension mechanisms, safety sensors, and electrical/electronic modules. It contains detailed sections on the description, operation, and maintenance of the landing gear and related systems. The training material is for student use only and cannot be distributed without permission.
Este documento é um treinamento sobre manutenção de linha e base para o Boeing 727-200. Ele fornece informações gerais sobre as dimensões, pesos e locais de serviço da aeronave. Também descreve os painéis de instrumentos do capitão e primeiro oficial, além do painel superior, painel inferior e painel de controle auxiliar.
Airbus a319 a320 a321 aircraft operating manualsn7
This document provides an operations manual for the Airbus A319/320/321 aircraft, summarizing key performance, systems and operational limits. It includes information on weight and balance limits, fuel requirements, avionics and autopilot limits, engine and systems specifications, airspeed limitations for different configurations, and center of gravity envelopes. The manual is intended to provide pilots with essential reference information to safely operate the aircraft.
This document discusses the primary flight controls of aircraft:
1. The elevator controls pitch around the lateral axis using upward and downward deflection. Larger aircraft use hydraulic or electric systems.
2. The rudder controls yaw around the normal axis and is operated by rudder pedals, which also control steering while taxiing. Some aircraft with V-tails use linked ruddervator surfaces.
3. Ailerons control roll around the longitudinal axis and work differentially to bank the aircraft, sometimes assisted by differential rudder inputs to coordinate the turn. Some light aircraft use flaperons.
O documento descreve o sistema de ar condicionado de uma aeronave B727-200, incluindo os packs de resfriamento, controle de temperatura e distribuição de ar. Os packs de resfriamento fornecem ar frio e quente através de trocadores de calor e unidades de ar frio para manter a temperatura adequada nas cabines. O sistema controla a mistura desse ar e também aquece os compartimentos de carga.
This document provides training material on flight controls for the Boeing 727-200. It describes the primary and auxiliary flight control surfaces including ailerons, elevators, rudders, flaps, and spoilers. It also summarizes the hydraulic and electrical systems used to power and control these surfaces. The document is intended solely for training and may not be distributed outside the client organization without permission.
This document provides a description and overview of the autopilot and yaw damper system for a B727-200 aircraft. It describes the major components, including the Sperry SP-50 MB V Automatic Flight Control System, which provides three-axis flight stabilization and automatic approach capability. It details the functions of the yaw, roll, and pitch axes, and describes the components that control and provide inputs to each axis, such as rudder power units, aileron servos, elevator power units, and sensors. The document also notes the locations of components throughout the aircraft.
This document provides a summary of instrument panels and systems on a Boeing 727-200 aircraft. It describes the layout of the main instrument panels used by pilots and crew. It also provides details on the types of instrument indicators and how they are mounted. The document then summarizes several key aircraft systems including the flight data recorder, clocks, and aural warning system. It explains the components and functions of these systems.
The document provides training material on landing gear for the B727-200 aircraft. It describes the landing gear components and systems, including the main and nose gears, retraction/extension mechanisms, safety sensors, and electrical/electronic modules. It contains detailed sections on the description, operation, and maintenance of the landing gear and related systems. The training material is for student use only and cannot be distributed without permission.
Este documento é um treinamento sobre manutenção de linha e base para o Boeing 727-200. Ele fornece informações gerais sobre as dimensões, pesos e locais de serviço da aeronave. Também descreve os painéis de instrumentos do capitão e primeiro oficial, além do painel superior, painel inferior e painel de controle auxiliar.
Airbus a319 a320 a321 aircraft operating manualsn7
This document provides an operations manual for the Airbus A319/320/321 aircraft, summarizing key performance, systems and operational limits. It includes information on weight and balance limits, fuel requirements, avionics and autopilot limits, engine and systems specifications, airspeed limitations for different configurations, and center of gravity envelopes. The manual is intended to provide pilots with essential reference information to safely operate the aircraft.
This document discusses the primary flight controls of aircraft:
1. The elevator controls pitch around the lateral axis using upward and downward deflection. Larger aircraft use hydraulic or electric systems.
2. The rudder controls yaw around the normal axis and is operated by rudder pedals, which also control steering while taxiing. Some aircraft with V-tails use linked ruddervator surfaces.
3. Ailerons control roll around the longitudinal axis and work differentially to bank the aircraft, sometimes assisted by differential rudder inputs to coordinate the turn. Some light aircraft use flaperons.
This slide is prepared by me for the students studying in 1st Semester of Aircraft Maintenance Engineering. This is only the the introduction of Maintenance Practices involved in Aircraft Maintenance. Reference is taken from various aviation books and websites. Suggestions are welcome. Pls leave a like
PS- after downloading please don't change the name of author as you will be disregarding all the hard work done by me.
This document provides information on fueling procedures for the Airbus A330-200 and A330-300 aircraft. It describes the differences in fuel tank configuration between the two models and outlines the general warnings and safety procedures that must be followed for all fueling operations. Standard fueling procedures are explained for both automatic and manual refueling modes. Overwing fueling and fuel transfer procedures are also summarized.
Frankfinn aviation presentation powerpoint fileVikas Pal
Vikas submitted an aviation project to his teacher Mrs. Simranjit Kaur. The project contained information on current affairs in the aviation industry from newspaper and magazine articles. It identified and described functions of various aircraft parts like the cockpit, cargo area, slide raft container, jump seat, passenger service unit, and more. Emergency equipment like oxygen bottles, fire extinguishers, life jackets, megaphones, and ELT beacons were also explained. Details were provided on transporting different types of passengers including minors, VVIPs, expectant mothers, and passengers with disabilities. Large commercial aircraft like the Airbus A380 and Boeing 747 were described. The Tenerife airport disaster
This document provides an overview of low visibility operations (LVO) including Category II, Category IIIA, and low visibility takeoffs. It defines key concepts such as decision height, runway visual range, operating minima, and requirements for aircraft, airfields, and flight crews to conduct these special operations. Category II allows for a manual landing at DH between 100-200 feet while Category IIIA requires an automatic landing system and has a DH under 100 feet or no DH with an RVR no less than 200 meters.
Flight controls allow pilots to control the forces of flight and maneuver aircraft. This chapter focuses on basic flight control systems, from early mechanical systems to modern fly-by-wire designs. It describes the primary flight controls - ailerons, elevators, and rudders - and how they control roll, pitch, and yaw respectively. Adverse yaw created by ailerons is also discussed, as are methods to reduce it like differential ailerons. The chapter provides examples of different flight control configurations for various aircraft types.
The document describes the fire protection systems on an aircraft, including smoke detection and fire extinguishing systems for the crew rest compartment, lavatories, wheel wells, pneumatic ducts, cargo compartments, and engines. It provides details on the components, locations, and functions of the smoke detectors, fire detectors, fire extinguishing bottles, and test buttons for these various systems.
The pneumatic system provides compressed air for aircraft functions like air conditioning, engine starting, and anti-ice systems. It obtains air from the engine bleed ports and controls the air pressure, temperature, and cleanliness. Leak detection loops monitor the hot air ducts and can isolate leaks by closing valves. The pneumatic system is controlled and monitored via panels and ECAM displays.
This document provides a technical training manual for maintenance personnel on the indicating and recording systems of single aisle aircraft, specifically focusing on the CFM56-5B/ME engines. It covers topics such as the Electronic Instrument System architecture and components, the Engine/Warning Display and its presentation of parameters and messages, ECAM advisory and failure related modes, and other systems like the Centralized Fault Display System, printer, and digital flight data recording. The manual is intended solely for training purposes and not as a reference document, as it will not be updated.
This document provides an overview of airworthiness directives, service bulletins, and maintenance requirements for aircraft. It defines airworthiness directives as legally enforceable regulations issued by the FAA to correct an unsafe condition. Service bulletins are notices from manufacturers about product improvements. The document outlines required inspections, owner responsibilities, and record keeping duties. It also explains how to find current airworthiness directives and service bulletins on the FAA and manufacturer websites.
The document discusses aircraft maintenance programmes and their importance in airworthiness management. It defines a maintenance programme as a schedule of maintenance tasks with documented management procedures. It notes key information sources for maintenance programmes include the MPD, CMM, SBs, and STCs. Approval of maintenance programmes may be issued to Sub Part G organisations. Effective maintenance programme management requires qualified specialists, applicable procedures, and oversight functions. Programmes aim to optimize maintenance tasks through reliability monitoring and review.
The document provides information on warning systems for the Boeing 737 NG, including visual, aural and tactile warnings. It describes conditions that trigger red warning lights for issues that require immediate attention, such as engine fires. Amber caution lights indicate issues needing timely attention. Blue, green and dim/bright blue lights provide non-critical information. The stick shaker and aural warnings alert to impending stalls. Ground proximity warning systems monitor altitude and terrain clearance in different phases of flight.
The document discusses lighting on a DA-40 NG aircraft. Landing and taxi lights are located in the left wing and are controlled via switches on the lighting panel. Interior lights can be turned on or off using controls on the lighting panel located in the cockpit.
This document discusses aircraft fuel systems. It describes the different types of fuels used for reciprocating and turbine engines. It then discusses key components of fuel systems like pumps, tanks, lines, valves, filters and strainers. It explains that the purpose of a fuel system is to store and deliver clean fuel at the proper pressure to the engine under various flight conditions. Fuel systems can be classified as gravity feed or pressure feed systems depending on how fuel is moved through the system. The document also outlines the different types of fuel tanks and lines used in aircraft, as well as components like selectors valves and quantity indicators.
The document discusses the electrical system of a B727-200 aircraft. It describes how three engine-driven generators produce electrical power and how a constant speed drive regulates their output frequency. It also explains how the generators can operate independently or be paralleled together, and how electrical power is distributed to different buses including essential, standby, battery, and load buses. The battery and battery charger are also described.
- The document presents a seminar on aircraft cabin pressurization systems given by Mr. Shrinivas Kale.
- It includes sections on introduction, literature review, problem formulation, objectives, methodology, hypothesis, work plan and references.
- The literature review summarizes several papers on topics related to aircraft cabin pressurization, environmental control systems, and thermal comfort experiments.
This document summarizes an FAA presentation on aircraft modifications. It discusses the regulations regarding modifications, including parts 21, 43, 91, and 135. It explains that for an aircraft to be considered airworthy, it must conform to its type design and be in a condition for safe operation. The presentation also discusses major vs minor alterations, field approvals, instructions for continued airworthiness, and other key topics relating to modifying aircraft.
This document discusses powered flaps systems for aircraft. It presents on flap synchronizing and asymmetric protection. It provides a resume on powered flaps systems, specifically highlighting advantages of using PDU motors to power the flaps.
El documento describe los requisitos técnicos y operacionales para realizar aterrizajes y despegues bajo condiciones de baja visibilidad. Estos incluyen sistemas de aterrizaje automático, luces de pista y calles de rodaje, señalización, equipos de medición de visibilidad como el RVR, y protección de las señales del ILS mediante áreas críticas y sensibles.
AIRBUS A320 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING ACNat Rice
This document provides a summary of revisions made in Revision No. 31 dated May 01/16 of the Airbus A320 Aircraft Characteristics - Airport and Maintenance Planning document. Key changes include updates to interior arrangement diagrams, terminal operations times, hydraulic and ground service connection diagrams, landing gear footprint diagrams, maximum pavement load data, and tire pressure updates. Figures and data were revised for several sections including cargo compartments, doors, escape slides, ground towing requirements, and runway length calculations.
The fuel system is designed to provide an uninterrupted flow of clean fuel from the fuel tanks to the engine. The fuel must be available to the engine under all conditions of engine power, altitude, attitude, and during all approved flight maneuvers . Fuel systems differ greatly from aircraft to aircraft due to the relative size and complexity of the aircraft in which they are installed.
This slide is prepared by me for the students studying in 1st Semester of Aircraft Maintenance Engineering. This is only the the introduction of Maintenance Practices involved in Aircraft Maintenance. Reference is taken from various aviation books and websites. Suggestions are welcome. Pls leave a like
PS- after downloading please don't change the name of author as you will be disregarding all the hard work done by me.
This document provides information on fueling procedures for the Airbus A330-200 and A330-300 aircraft. It describes the differences in fuel tank configuration between the two models and outlines the general warnings and safety procedures that must be followed for all fueling operations. Standard fueling procedures are explained for both automatic and manual refueling modes. Overwing fueling and fuel transfer procedures are also summarized.
Frankfinn aviation presentation powerpoint fileVikas Pal
Vikas submitted an aviation project to his teacher Mrs. Simranjit Kaur. The project contained information on current affairs in the aviation industry from newspaper and magazine articles. It identified and described functions of various aircraft parts like the cockpit, cargo area, slide raft container, jump seat, passenger service unit, and more. Emergency equipment like oxygen bottles, fire extinguishers, life jackets, megaphones, and ELT beacons were also explained. Details were provided on transporting different types of passengers including minors, VVIPs, expectant mothers, and passengers with disabilities. Large commercial aircraft like the Airbus A380 and Boeing 747 were described. The Tenerife airport disaster
This document provides an overview of low visibility operations (LVO) including Category II, Category IIIA, and low visibility takeoffs. It defines key concepts such as decision height, runway visual range, operating minima, and requirements for aircraft, airfields, and flight crews to conduct these special operations. Category II allows for a manual landing at DH between 100-200 feet while Category IIIA requires an automatic landing system and has a DH under 100 feet or no DH with an RVR no less than 200 meters.
Flight controls allow pilots to control the forces of flight and maneuver aircraft. This chapter focuses on basic flight control systems, from early mechanical systems to modern fly-by-wire designs. It describes the primary flight controls - ailerons, elevators, and rudders - and how they control roll, pitch, and yaw respectively. Adverse yaw created by ailerons is also discussed, as are methods to reduce it like differential ailerons. The chapter provides examples of different flight control configurations for various aircraft types.
The document describes the fire protection systems on an aircraft, including smoke detection and fire extinguishing systems for the crew rest compartment, lavatories, wheel wells, pneumatic ducts, cargo compartments, and engines. It provides details on the components, locations, and functions of the smoke detectors, fire detectors, fire extinguishing bottles, and test buttons for these various systems.
The pneumatic system provides compressed air for aircraft functions like air conditioning, engine starting, and anti-ice systems. It obtains air from the engine bleed ports and controls the air pressure, temperature, and cleanliness. Leak detection loops monitor the hot air ducts and can isolate leaks by closing valves. The pneumatic system is controlled and monitored via panels and ECAM displays.
This document provides a technical training manual for maintenance personnel on the indicating and recording systems of single aisle aircraft, specifically focusing on the CFM56-5B/ME engines. It covers topics such as the Electronic Instrument System architecture and components, the Engine/Warning Display and its presentation of parameters and messages, ECAM advisory and failure related modes, and other systems like the Centralized Fault Display System, printer, and digital flight data recording. The manual is intended solely for training purposes and not as a reference document, as it will not be updated.
This document provides an overview of airworthiness directives, service bulletins, and maintenance requirements for aircraft. It defines airworthiness directives as legally enforceable regulations issued by the FAA to correct an unsafe condition. Service bulletins are notices from manufacturers about product improvements. The document outlines required inspections, owner responsibilities, and record keeping duties. It also explains how to find current airworthiness directives and service bulletins on the FAA and manufacturer websites.
The document discusses aircraft maintenance programmes and their importance in airworthiness management. It defines a maintenance programme as a schedule of maintenance tasks with documented management procedures. It notes key information sources for maintenance programmes include the MPD, CMM, SBs, and STCs. Approval of maintenance programmes may be issued to Sub Part G organisations. Effective maintenance programme management requires qualified specialists, applicable procedures, and oversight functions. Programmes aim to optimize maintenance tasks through reliability monitoring and review.
The document provides information on warning systems for the Boeing 737 NG, including visual, aural and tactile warnings. It describes conditions that trigger red warning lights for issues that require immediate attention, such as engine fires. Amber caution lights indicate issues needing timely attention. Blue, green and dim/bright blue lights provide non-critical information. The stick shaker and aural warnings alert to impending stalls. Ground proximity warning systems monitor altitude and terrain clearance in different phases of flight.
The document discusses lighting on a DA-40 NG aircraft. Landing and taxi lights are located in the left wing and are controlled via switches on the lighting panel. Interior lights can be turned on or off using controls on the lighting panel located in the cockpit.
This document discusses aircraft fuel systems. It describes the different types of fuels used for reciprocating and turbine engines. It then discusses key components of fuel systems like pumps, tanks, lines, valves, filters and strainers. It explains that the purpose of a fuel system is to store and deliver clean fuel at the proper pressure to the engine under various flight conditions. Fuel systems can be classified as gravity feed or pressure feed systems depending on how fuel is moved through the system. The document also outlines the different types of fuel tanks and lines used in aircraft, as well as components like selectors valves and quantity indicators.
The document discusses the electrical system of a B727-200 aircraft. It describes how three engine-driven generators produce electrical power and how a constant speed drive regulates their output frequency. It also explains how the generators can operate independently or be paralleled together, and how electrical power is distributed to different buses including essential, standby, battery, and load buses. The battery and battery charger are also described.
- The document presents a seminar on aircraft cabin pressurization systems given by Mr. Shrinivas Kale.
- It includes sections on introduction, literature review, problem formulation, objectives, methodology, hypothesis, work plan and references.
- The literature review summarizes several papers on topics related to aircraft cabin pressurization, environmental control systems, and thermal comfort experiments.
This document summarizes an FAA presentation on aircraft modifications. It discusses the regulations regarding modifications, including parts 21, 43, 91, and 135. It explains that for an aircraft to be considered airworthy, it must conform to its type design and be in a condition for safe operation. The presentation also discusses major vs minor alterations, field approvals, instructions for continued airworthiness, and other key topics relating to modifying aircraft.
This document discusses powered flaps systems for aircraft. It presents on flap synchronizing and asymmetric protection. It provides a resume on powered flaps systems, specifically highlighting advantages of using PDU motors to power the flaps.
El documento describe los requisitos técnicos y operacionales para realizar aterrizajes y despegues bajo condiciones de baja visibilidad. Estos incluyen sistemas de aterrizaje automático, luces de pista y calles de rodaje, señalización, equipos de medición de visibilidad como el RVR, y protección de las señales del ILS mediante áreas críticas y sensibles.
AIRBUS A320 AIRCRAFT CHARACTERISTICS AIRPORT AND MAINTENANCE PLANNING ACNat Rice
This document provides a summary of revisions made in Revision No. 31 dated May 01/16 of the Airbus A320 Aircraft Characteristics - Airport and Maintenance Planning document. Key changes include updates to interior arrangement diagrams, terminal operations times, hydraulic and ground service connection diagrams, landing gear footprint diagrams, maximum pavement load data, and tire pressure updates. Figures and data were revised for several sections including cargo compartments, doors, escape slides, ground towing requirements, and runway length calculations.
The fuel system is designed to provide an uninterrupted flow of clean fuel from the fuel tanks to the engine. The fuel must be available to the engine under all conditions of engine power, altitude, attitude, and during all approved flight maneuvers . Fuel systems differ greatly from aircraft to aircraft due to the relative size and complexity of the aircraft in which they are installed.
1. LINE AND BASE MAINTENACE TRAINING
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AIRWAYS CONSULTORIA AERONÁUTICA LTDA
2. AIRWAYS TREINAMENTOS FUEL
GLOBEX 042008/01
28.2
MATERIAL DIDÁTICO
ESTE DOCUMENTO SERÁ UTILIZADO SOMENTE COMO TREINAMENTO
Este material é para uso exclusivo do aluno. Nenhuma de suas partes pode ser veiculada, transcrita
ou reproduzida para distribuição fora da organização do cliente, sem prévio consentimento por escrito
da AIRWAYS CONSULTORIA AERONÁUTICA LTDA.
3. AIRWAYS TREINAMENTOS FUEL
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5. AIRWAYS TREINAMENTOS FUEL
GLOBEX 042008/01
28.5
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in
ng
g i
is
s a
ac
cc
co
om
mp
pl
li
is
sh
he
ed
d t
th
hr
ro
ou
ug
gh
h t
th
he
e t
ta
an
nk
k N
Nº
º 1
1 a
an
nd
d 3
3 o
ov
ve
er
rw
wi
in
ng
g f
fi
il
ll
le
er
r p
po
or
rt
ts
s.
. T
Th
he
e w
wi
in
ng
g
t
ta
an
nk
ks
s a
ar
re
e f
fi
il
ll
le
ed
d d
di
ir
re
ec
ct
tl
ly
y.
. T
Ta
an
nk
k N
Nº
º 2
2 a
an
nd
d t
th
he
e a
au
ux
xi
il
li
ia
ar
ry
y t
ta
an
nk
k a
ar
re
e s
se
er
rv
vi
ic
ce
ed
d b
by
y g
gr
ro
ou
un
nd
d t
tr
ra
an
ns
sf
fe
er
r f
fr
ro
om
m e
ei
it
th
he
er
r t
ta
an
nk
ks
s N
Nº
º 1
1
o
or
r 3
3.
.
F
FU
UE
EL
L F
FE
EE
ED
D S
SY
YS
ST
TE
EM
M
F
Fu
ue
el
l i
is
s s
su
up
pp
pl
li
ie
ed
d u
un
nd
de
er
r p
pr
re
es
ss
su
ur
re
e f
fr
ro
om
m e
ea
ac
ch
h m
ma
ai
in
n t
ta
an
nk
k t
to
o i
it
ts
s c
co
or
rr
re
es
sp
po
on
nd
di
in
ng
g e
en
ng
gi
in
ne
e.
. A
An
n a
al
lt
te
er
rn
na
at
te
e m
me
et
th
ho
od
d,
,
u
us
si
in
ng
g t
th
he
e c
cr
ro
os
ss
sf
fe
ee
ed
d m
ma
an
ni
if
fo
ol
ld
d,
, p
pe
er
rm
mi
it
ts
s f
fu
ue
el
l t
to
o b
be
e s
su
up
pp
pl
li
ie
ed
d f
fr
ro
om
m a
a t
ta
an
nk
k t
to
o a
an
ny
y o
or
r a
al
ll
l e
en
ng
gi
in
ne
es
s.
. T
Th
he
e a
au
ux
xi
il
li
ia
ar
ry
y t
ta
an
nk
k i
in
n
A
Ap
pl
l.
. S
S/
/N
N 2
21
13
30
03
3 a
an
nd
d l
li
ik
ke
e c
co
on
nf
fi
ig
gu
ur
ra
at
ti
io
on
n i
is
s c
co
on
nn
ne
ec
ct
te
ed
d t
th
hr
ro
ou
ug
gh
h t
th
he
e N
Nº
º 2
2 s
sy
ys
st
te
em
m.
.
F
Fu
ue
el
l b
bo
oo
os
st
t p
pu
um
mp
ps
s i
in
n t
ta
an
nk
k N
Nº
º 2
2 o
of
f A
Ap
pl
l.
. S
S/
/N
N 2
20
06
63
34
4 a
an
nd
d l
li
ik
ke
e c
co
on
nf
fi
ig
gu
ur
ra
at
ti
io
on
n,
, o
op
pe
er
ra
at
te
e a
at
t a
a h
hi
ig
gh
he
er
r p
pr
re
es
ss
su
ur
re
e a
an
nd
d
o
ov
ve
er
rr
ri
id
de
e t
th
he
e p
pu
um
mp
p o
ou
ut
tp
pu
ut
t o
of
f t
th
ha
an
nk
ks
s 1
1 a
an
nd
d 3
3 w
wh
he
en
n t
th
he
e p
pu
um
mp
p o
ou
ut
tp
pu
ut
t o
of
f t
ta
an
nk
ks
s 1
1 a
an
nd
d 3
3 w
wh
he
en
n m
ma
an
ni
if
fo
ol
ld
de
ed
d t
to
og
ge
et
th
he
er
r.
.
T
Th
he
e f
fu
ue
el
l b
bo
oo
os
st
t p
pu
um
mp
ps
s i
in
n N
Nº
º 2
2 t
ta
an
nk
k a
an
nd
d t
th
he
e a
af
ft
t a
au
ux
xi
il
li
ia
ar
ry
y t
ta
an
nk
k o
of
f A
Ap
pl
l.
. S
S/
/N
N 2
21
13
30
03
3 a
an
nd
d l
li
ik
ke
e c
co
on
nf
fi
ig
gu
ur
ra
at
ti
io
on
n a
ar
re
e h
hi
ig
gh
h
c
ca
ap
pa
ac
ci
it
ty
y p
pu
um
mp
ps
s a
an
nd
d o
ov
ve
er
rr
ri
id
de
e t
th
he
e p
pu
um
mp
p o
ou
ut
tp
pu
ut
t o
of
f t
ta
an
nk
ks
s 1
1 a
an
nd
d 3
3 w
wh
he
en
n m
ma
an
ni
if
fo
ol
ld
de
ed
d t
to
og
ge
et
th
he
er
r.
.
6. AIRWAYS TREINAMENTOS FUEL
GLOBEX 042008/01
28.6
A
A f
fu
ue
el
l b
bo
oo
os
st
t p
pu
um
mp
p b
by
yp
pa
as
ss
s v
va
al
lv
ve
e a
al
ll
lo
ow
ws
s e
en
ng
gi
in
ne
e d
dr
ri
iv
ve
en
n p
pu
um
mp
ps
s t
to
o d
dr
ra
aw
w f
fu
ue
el
l f
fr
ro
om
m t
th
he
e m
ma
ai
in
n t
ta
an
nk
ks
s i
if
f a
al
ll
l
p
pu
um
mp
ps
s i
in
n t
th
he
e t
ta
an
nk
k a
ar
re
e i
in
no
op
pe
er
ra
at
ti
iv
ve
e.
.
p
p A
AP
PU
U f
fu
ue
el
l f
fe
ee
ed
d i
is
s o
ob
bt
ta
ai
in
ne
ed
d f
fr
ro
om
m t
tw
wo
o l
lo
oc
ca
at
ti
io
on
ns
s.
. W
Wh
he
en
n b
bo
oo
os
st
t p
pu
um
mp
p p
pr
re
es
ss
su
ur
re
e i
is
s n
no
ot
t a
av
va
ai
il
la
ab
bl
le
e f
fu
ue
el
l i
is
s
p
pr
ro
ov
vi
id
de
ed
d b
by
y s
su
uc
ct
ti
io
on
n f
fe
ee
ed
d f
fr
ro
om
m t
ta
an
nk
k N
Nº
º 2
2.
.
P
Pr
re
es
ss
su
ur
ri
iz
ze
ed
d f
fu
ue
el
l i
is
s a
a a
av
va
ai
il
la
ab
bl
le
e f
fr
ro
om
m a
an
ny
y b
bo
oo
os
st
t p
pu
um
mp
p w
wh
he
en
n i
it
t i
is
s f
fe
ee
ed
di
in
ng
g t
th
he
e N
Nº
º 2
2 m
ma
an
ni
if
fo
ol
ld
d.
.
F
FU
UE
EL
L D
DU
UM
MP
P S
SY
YS
ST
TE
EM
M
F
Fu
ue
el
l m
ma
ay
y b
be
e d
du
um
mp
pe
ed
d f
fr
ro
om
m a
al
ll
l t
ta
an
nk
ks
s t
th
hr
ro
ou
ug
gh
h t
th
he
e f
fu
ue
el
li
in
ng
g a
an
nd
d d
du
um
mp
p m
ma
an
ni
if
fo
ol
ld
d.
. A
A d
du
um
mp
p l
le
ev
ve
el
l s
sh
hu
ut
to
of
ff
f s
se
en
ns
so
or
r
i
in
n t
th
he
e m
ma
ai
in
n t
ta
an
nk
ks
s t
te
er
rm
mi
in
na
at
te
es
s d
du
um
mp
pi
in
ng
g a
at
t a
ap
pp
pr
ro
ox
xi
im
ma
at
te
el
ly
y 3
35
50
00
0 p
po
ou
un
nd
ds
s/
/1
15
59
90
0 k
ki
il
lo
og
gr
ra
am
ms
s.
. T
Th
he
e a
au
ux
xi
il
li
ia
ar
ry
y t
ta
an
nk
k
d
du
um
mp
ps
s t
th
hr
ro
ou
ug
gh
h t
th
he
e n
nu
um
mb
be
er
r 2
2 t
ta
an
nk
k s
sy
ys
st
te
em
m a
an
nd
d c
ca
an
n b
be
e c
co
om
mp
pl
le
et
te
el
ly
y e
em
mp
pt
ti
ie
ed
d.
.
F
FU
UE
EL
L T
TR
RA
AN
NS
SF
FE
ER
R
O
On
n t
th
he
e g
gr
ro
ou
un
nd
d,
, f
fu
ue
el
l m
ma
ay
y b
be
e t
tr
ra
an
ns
sf
fe
er
rr
re
ed
d b
be
et
tw
we
ee
en
n a
an
ny
y m
ma
ai
in
n t
ta
an
nk
k t
th
hr
ro
ou
ug
gh
h t
th
he
e d
de
ef
fu
ue
el
li
in
ng
g v
va
al
lv
ve
e w
wh
hi
ic
ch
h
c
co
on
nn
ne
ec
ct
ts
s t
th
he
e c
cr
ro
os
ss
sf
fe
ee
ed
d m
ma
an
ni
if
fo
ol
ld
d t
to
o t
th
he
e f
fu
ue
el
li
in
ng
g a
an
nd
d d
du
um
mp
p m
ma
an
ni
if
fo
ol
ld
d.
. F
Fu
ue
el
l m
ma
ay
y b
be
e t
tr
ra
an
ns
sf
fe
er
rr
re
ed
d t
to
o t
th
he
e a
au
ux
xi
il
li
ia
ar
ry
y
t
ta
an
nk
k d
di
ir
re
ec
ct
tl
ly
y f
fr
ro
om
m t
th
he
e N
Nº
º 2
2 t
ta
an
nk
k.
.