ATA 36 Pneumatics MTT M540000 / R3.3 01AUG01 For Training Purposes Only 36-1 361 ATA 36 A300/A310 Air Supply System
Views 117 Downloads 2 File size 6MB
ATA 36 Pneumatics
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-1 361
ATA 36 A300/A310
Air Supply System
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-2 362
ATA 36 A300/A310
A300 / Some A310 Pneumatic System – General Schematic - GE CF6 Engine
•
*
*
•
Pressurization System without Jet Pump Supply
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-3 363
ATA 36 A300/A310
A310 Pneumatic System - General Schematic - PW JT9D Engines
•
*
*
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-4 364
ATA 36 A300/A310
Engine Air Bleed - Typical Schematic for GE and PW Engines
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-5 365
ATA 36 A300/A310
A300 Pneumatic System Electrical Power Supply – Typical Layout
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-6 366
ATA 36 A300/A310
Bleed Air Supply System – Nacelle and Pylon Component Locations
A300 SHOWN
GE CF6-80C2A5F Engine 1
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-7 367
ATA 36 A300/A310
A310 Pneumatic System - Nacelle and Pylon Component Locations
A310 SHOWN
PW JT9D-7R4 Engine 1
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-8 368
ATA 36 A300/A310
A310/A310 Pneumatic System – Air Bleed System Components and Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-9 369
ATA 36 A300/A310
A300/A310 Pneumatic System Controllers and 103VU Relay Panel - Location
Electronic Rack 90VU ENGINE 2
FW
D
ENGINE 1
Avionics Bay
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-10 3610
ATA 36 A300/A310
A300 Air Bleed System Panel Locations – Controls and Indicating
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-11 3611
ATA 36 A300/A310
COMPT TEMP/AIR BLEED Panels 436 / 437 VU
437VU
436VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-12 3612
ATA 36 A300/A310
A300/A310 AIR BLEED Panel 436VU – Bleed Valve Indications
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-13 3613
ATA 36 A300/A310
A300/A310 AIR BLEED Panel 436VU – Bleed Valve Indications
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-14 3614
ATA 36 A300/A310
A300/A310 AIR BLEED Panel 436VU – Bleed Valve Indications
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-15 3615
ATA 36 A300/A310
A300/A310 AIR BLEED Panel 436VU – X FEED (Crossfeed) Control and Indicating
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-16 3616
ATA 36 A300/A310
A300/A310 ECAM System – ECAM Control Panel and RH ECAM Display
RH ECAM
ECAM CONTROL PANEL
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-17 3617
ATA 36 A300/A310
A300/A310 RH ECAM Display Unit – AIR BLEED Page
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-18 3618
ATA 36 A300/A310
A300/A310 RH ECAM Display Unit – AIR BLEED Page
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-19 3619
ATA 36 A300/A310
A300/A310 RH ECAM Display Unit – AIR BLEED Page
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-20 3620
ATA 36 A300/A310
A300 HP Valve - Manual Override/Visual Position Indicator
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-21 3621
ATA 36 A300/A310
A310 Pneumatic System High Pressure (HP) Bleed Valve FIN DV225 (DV226)
PW JT9-7R4 Engine 1
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-22 3622
ATA 36 A300/A310
A310 Pneumatic System - High Pressure (HP) Valve - Installation Features
JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-23 3623
ATA 36 A300/A310
A300 Pneumatic System - 8th Stage Check Valve FIN A004 (B004) - Installation
GE CF6-80C2A5F Engine One Valve per Engine Engine 1 - FIN A004 Engine 2 - FIN B004 *IP - Intermediate Pressure
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
*IP
36-24 3624
ATA 36 A300/A310
A310 Pneumatic System - 8th Stage Check Valves - Component Installation
PW JT9D-7R4 Engine Two Valves per Engine Engine 1 - FIN B004 Engine 2 - FIN D004
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-25 3625
ATA 36 A300/A310
A300 Pneumatic System - Bleed Valve (Pressure Regulating and Shutoff/PRSOV)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-26 3626
ATA 36 A300/A310
A300 Pneumatic System - Bleed Air Valve FIN DV224 (Eng 1/2) - Component Installation
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-27 3627
ATA 36 A300/A310
A310 Bleed Air System - Bleed and Pressure Regulator Shutoff Valve - Component Features
JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-28 3628
ATA 36 A300/A310
A310 Bleed Air System - Bleed and Pressure Regulator Shutoff Valve - Component Installation
JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-29 3629
ATA 36 A300/A310
A310 Bleed Air System - Bleed and Pressure Regulator Shutoff Valve - Lockout and Filters
JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-30 3630
ATA 36 A300/A310
A310 - Bleed Air System Overpressure Valve (OPV) - Component Installation
PW JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-31 3631
ATA 36 A300/A310
Engine Bleed Air System - Over Pressure Valve (OPV) - Schematic and Features
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-32 3632
ATA 36 A300/A310
A300/A310 Bleed Air System - Overpressure Valve - Component Installation
GE CF6-80A3 ENGINE AND GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-33 3633
ATA 36 A300/A310
A300 Bleed Air System - Fan Air Valve (FAV) FIN 51HA (52HA) - Component Valve Identification Names
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-34 3634
ATA 36 A300/A310
A300 Bleed Air System - Fan Air Valve (FAV) - Component Features Ambient Air to Precooler (Heat Exchanger) GE CF6-80C2A5F ENGINE
NOTE: FAV - On Aircraft N650FE to N653FE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-35 3635
ATA 36 A300/A310
A300 Bleed Air System - Fan Air Valve (FAV) - Mechanical Lockout and Test Port
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-36 3636
ATA 36 A300/A310
A300 Engine Bleed Air System - Fan Air Valve (FAV) - Filter Element
GE CF6-80C2A5F ENGINE
FAV Air Filter FAV Engine 1 - FIN 51 HA FAV Engine 2 - FIN 52 HA
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-37 3637
ATA 36 A300/A310
A310 Fan Air Valve (FAV) FIN 51HA (52HA) - General View
JT9D-7R4 Engine
Aircraft Configuration 01
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-38 3638
ATA 36 A300/A310
A310 Bleed Air System - Fan Air Valve (FAV) - Air Filter Element
PW JT9D-7R4 Engine
Filter Spring Gasket Plug
Aircraft Configuration 02 MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-39 3639
ATA 36 A300/A310
A300/A310 Bleed Air System - Cooling Air Inlet Duct to Precooler Base Unit
NOTE COOLING AIR EXTRACTED FROM FAN AIR STREAM TO THE FAN AIR VALVE (FAV) IS DUCTED TO THE PRECOOLER BASE UNIT. COOL FAN AIR IS DIRECTED THROUGH THE BLEED AIR SYSTEM PRECOOLER UNIT FOR COOLING HOT BLEED AIR FOR PNEUMATIC USERS. THE USED COOLING AIR IS DIRECTED OVER BOARD ON TOP OF THE PYLON ASSEMBLY TO LOUVERED PANEL ASSEMBLY.
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-40 3640
ATA 36 A300/A310
A300/A310 Pneumatic Bleed Air System Precooler - Component Installation
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-41 3641
ATA 36 A300/A310
A300/A310 Pneumatic System - Sensors - Component Location
Regulator Pressure Sensor
High Stage Pressure Sensor
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-42 3642
ATA 36 A300/A310
A300/A310 Wing-to-Pylon Connection - Component Installation and Sensors PRECOOLER OUTLET TEMPERATURE SENSOR FIN 4HX (5HX )
PRECOOLER TEMPERATURE CONTROL SENSOR FIN 53HA (54HA)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-43 3643
ATA 36 A300/A310
A300/A310 Pneumatic System - Pressure Sensors - Pylon Location
Regulator Pressure Sensor FIN 49HA (50HA) UPPER UNIT
A300 SHOWN High Stage Pressure Sensor FIN 47HA (48HA) LOWER UNIT
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-44 3644
ATA 36 A300/A310
A310 Pneumatic System - Pressure Sensors - Installation of Sensors
Regulator Pressure Sensor
PRECOOLER OUTLET TEMPERATURE SENSOR 4HX (5HX)
High Stage Pressure Sensor
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-45 3645
ATA 36 A300/A310
Warning Logic - JT9D Engine Bleed Air System
Warning Logic - Engine Bleed Air Warning Depicted below are various warnings displayed in the Flight Deck in the event a fault occurs in the aircraft pneumatic system. Also graphically shown are the various flight phases at which warnings will or will not be shown.
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-46 3646
ATA 36 A300/A310
A310 PW JT9D-7R4 Engine Bleed Air Warning Logic - Configuration 01
WLDP
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-47 3647
ATA 36 A300/A310
Warning Logic - Engine Bleed Air Warning Depicted below are various warnings displayed in the Flight Deck in the event a fault occurs in the aircraft pneumatic system. Also graphically shown are the various flight phases at which warnings will or will not be shown.
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-48 3648
ATA 36 A300/A310
A310 PW JT9D-7R4 Engine Bleed Air Warning Logic - Configuration 01
WLDP
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-49 3649
ATA 36 A300/A310
A300 Pneumatic System - High Stage Temperature Sensor (T3) - Component Location GE CF6-80C2A5F Engine
FIN T603 Engine 1/2
FADEC
FWD
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-50 3650
ATA 36 A300/A310
A310 Pneumatic System - High Stage Temperature Sensor - Component Installation
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-51 3651
ATA 36 A300/A310
A300 BLEED AIR SYSTEM - 14th Stage Manifold - Component Installation
GE CF6-80C2A5F ENGINE ENGINE NUMBER 1
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-52 3652
ATA 36 A300/A310
A300 BLEED AIR SYSTEM - 8th Stage Manifold - Component Installation
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-53 3653
ATA 36 A300/A310
A310 BLEED AIR SYSTEM- Low Pressure Bleed Air Check Valve and Duct Assembly Component Installation
To Left Hand side of Engine to PRSOV (Bleed Valve) Valve)
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-54 3654
ATA 36 A300/A310
A310 BLEED AIR SYSTEM - 8th and 15th Stage Collector Duct Assembly - Component Installation
*Bleed Air Port for Hydraulic Reservoir System - Engine 1 only - Engine 2 Plug inserted in port hole.
From 8 th Stage Engine Port (RH Side of Engine) To Precooler (Heat Exchanger) Air Flow
8th Stage Air Flow In
* Air Flow Starter Air Duct
PS4 Air 15th Stage (PS4 Air) Air Flow In
PW JT9D-7R4 ENGINE
PS4 Air
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-55 3655
ATA 36 A300/A310
A310 BLEED AIR SYSTEM - Left 8th Stage Low Pressure Bleed and Duct Assembly Component Installation
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-56 3656
ATA 36 A300/A310
A310 BLEED AIR SYSTEM - Bleed Air Pressure Regulator Valve Outlet Duct Assembly Component Installation Air Flow to Precooler
PRSOV 8th/15th Stage Air Flow Out
PW JT9D-7R4 ENGINE PRSOV = PRESSURE REGULATING SHUT OFF VALVE
Air Flow Out
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-57 3657
ATA 36 A300/A310
A310 BLEED AIR SYSTEM - 15th State High Pressure Manifold - Component Installation
PW JT9D-7R4 ENGINE
* *
Diffuser Section
* *PS4 Air Flow Out
* MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-58 3658
ATA 36 A300/A310
A300/A310 Pneumatic Bleed Air Duct - Clamp Location and Features (Typical)
WING FRONT SPAR AREA
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-59 3659
ATA 36 A300/A310
A300/A310 Bleed Air Duct - Clamp Installation and Duct Alignment
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-60 3660
ATA 36 A300/A310
Some A310 Pneumatic System Controller / GE CF6-80A3 and PW JT9D-7R4 Engines - (Front Face Labels - BITE Check)
FIN 41HA (42HA
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
FIN 41HA (42HA)
36-61 3661
ATA 36 A300/A310
A300 / Some A310 Pneumatic System Controller - Front Face
FIN 41HA (42HA)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-62 3662
ATA 36 A300/A310
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram
or PW Engine
FIN 41HA (42HA)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-63 3663
ATA 36 A300/A310
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram 1
FIN 41HA (42HA)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-64 3664
ATA 36 A300/A310
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram 2
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-65 3665
ATA 36 A300/A310
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram 3
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-66 3666
ATA 36 A300/A310
A300/A310 APU Bleed Air System - Flight Deck Controls and Indications
AIR BLEED PANEL 436VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-67 3667
ATA 36 A300/A310
A300/A310 APU Bleed Air System - Component Location in Fuselage
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-68 3668
ATA 36 A300/A310
A300/A310 Pneumatic System – High Pressure (HP) Ground Connectors – Component Location
Only on some A310s
A310 SHOWN
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-69 3669
ATA 36 A300/A310
A300/A310 APU Bleed Air and Crossfeed - Schematic
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-70 3670
ATA 36 A300/A310
A300/A310 Bleed Air System – Crossfeed (X-FEED) Valve FIN 16HV – Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-71 3671
ATA 36 A300/A310
A300/A310 Bleed Air System – Crossfeed Valve (X-FEED) FIN 16HV – Component Installation
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-72 3672
ATA 36 A300/A310
A300/A310 APU Bleed Air – Component Location in Fuselage
APU ECB UNIT
Located in Bulk Cargo Bay Area – Above and Aft of Bulk Cargo Door
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-73 3673
ATA 36 A300/A310
A300/A310 APU Bleed Air System – Bleed (Load Control) Valve FIN 66KD - General Features
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-74 3674
ATA 36 A300/A310
A300 / Some A310 APU Bleed Air System – Check Valve FIN 360022 – Component Installation NOTE SOME A310 HAVE SIX (PIE CUT SHAPE) FLAPPER TYPE CHECK VALVE COMPONENT UNITS WITH SPRINGS TO RESEAT FLAPPER UNDER NO PNEUMATIC LOAD CONDITIONS
DOUBLE FLAPPER TYPE CHECK VALVE
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-75 3675
ATA 36 A300/A310
A300/A310 Wing Leading Edge Air Cooling Area (Slat Number 1 Area)- General Features
NACA = National Advisory Committee of Aeronautics U. S. A. - Now NASA Since 1958.
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-76 3676
ATA 36 A300/A310
A300/A310 Pneumatic System - Overheat Detection Controllers - Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-77 3677
ATA 36 A300/A310
A300/Some A310s Maintenance Panel 472VU - AIR BLEED & COMPT TEMP Test Panel
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-78 3678
ATA 36 A300/A310
A300/A310 Air Bleed - Monitoring and Bleed Fault Test - Flight Deck Configurations
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-79 3679
ATA 36 A300/A310
A300/A310 Air Bleed System - Manifold Air Leak Test Panel
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-80 3680
ATA 36 A300/A310
A300/A310 Pneumatic System - Control and Indicating - Location
COMPT TEMP PANEL 437VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-81 3681
ATA 36 A300/A310
A300/A310 Pneumatic System - Bleed Air Pressure Indication - Overhead Panel 437VU
COMPT TEMP PANEL 437VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-82 3682
ATA 36 A300/A310
A300/A310 PRECOOLER OUTLET TEMP - SCHEMATIC
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-83 3683
ATA 36 A300/A310
A300/A310 Manifold Air Leak Detection - Controls and Indications - Location
90VU ELECTRONIC RACK
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-84 3684
ATA 36 A300/A310
A300/A310 Pneumatic System - Overheat Detection Controller FIN 12HF/13HF - Location
90VU ELECTRONIC RACK
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-85 3685
ATA 36 A300/A310
A300/A310 Manifold Air Leak Detection - Detection Loops Layout
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-86 3686
ATA 36 A300/A310
A300/A310 GE/PW Engine Pylon Overheat Detection - Component Location
ENGINE 1 PYLON - INBRD SIDE ENGINE 2 PYLON - OUTBRD SIDE
204 DEGREES C SINGLE LOOP
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-87 3687
ATA 36 A300/A310
A300/A310 Wing Overheat Detection - Loop Sections Layout
A300 SHOWN
ALL AREAS SHOWN 124 DEGREES C DOUBLE LOOPS
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-88 3688
ATA 36 A300/A310
A300/A310 Pneumatic System - Overheat Sensing Elements - Location in Fuselage
A310 SHOWN
ALL AREAS SHOWN - 124 DEGREES C DOUBLE LOOPS
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-89 3689
ATA 36 A300/A310
A300/A310 Aft Fuselage Overheat Detection - Overheat Sensing Elements
124 DEGREE C SINGLE LOOP 154 DEGREE C SINGLE LOOP
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-90 3690
ATA 36 A300/A310
A300/A310 Manifold Air Leak Detection - Ambient Overheat Detection Loop
GROMMET
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-91 3691
ATA 36 A300/A310
A300/A310 Pneumatic System - Manifold Leak Detection - Schematic NOTE Some A310 have Master Caution Lights and other A310 have WLDP (WARNING LIGHT DISPLAY PANEL)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-92 3692
ATA 36 A300/A310
A300/A310 Engine Bleed System - Troubleshooting Guidelines and Information
GE CF6-80C2A5F (FADEC Engine)
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-93 3693
ATA 36 A300/A310
A300/A310 Engine Bleed System - Troubleshooting Guidelines and Information
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-94 3694
ATA 36 A300/A310
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-95 3695
ATA 36 A300/A310
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-96 3696
ATA 36 A300/A310
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-97 3697
ATA 36 A300/A310
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-98 3698
ATA 36 A300/A310
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-99 3699
ATA 36 A300/A310
A310 Bleed Air Pneumatic Controller FIN 41HA (42HA) - BITE Test
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-100 36100
ATA 36 A300/A310
A300/A310 Bleed Air Pneumatic Controller FIN 41HA (42HA) - BITE Sequence
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-101 36101
ATA 36 A300/A310
Warning Logic - Pneumatic System
Depicted below are various warnings displayed in the flight deck in the event a fault occurs in the aircraft Pneumatic System. Also graphically shown are the various Flight Phases at which warnings will or will not be shown.
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-102 36102
ATA 36 A300/A310
Warning Logic - Pneumatic System
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-103 36103
ATA 36 A300/A310
THIS PAGE INTENTIONALLY LEFT BLANK ATA 36 - END COURSE CODE - M450000
MTT M540000 / R3.3 01AUG01 For Training Purposes Only
36-104 36104
ATA 36 A300/A310