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MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-11
ATA 36ATA 36PneumaticsPneumatics
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-22
Air Supply System
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-33
****
•
• Pressurization System without Jet Pump SupplyPressurization System without Jet Pump Supply
A300 / Some A310 Pneumatic System – General Schematic - GE CF6 Engine
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-44
****
•A310 Pneumatic System - General Schematic - PW JT9D Engines
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-55
Engine Air Bleed - Typical Schematic for GE and PW Engines
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-66
A300 Pneumatic System Electrical Power Supply – Typical Layout
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-77
Bleed Air Supply System – Nacelle and Pylon Component Locations
GE CF6-80C2A5FEngine 1
A 3 0 0 S H O W N
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-88
A310 Pneumatic System - Nacelle and Pylon Component Locations
PW JT9D-7R4 PW JT9D-7R4 Engine 1Engine 1
A310 SHOWN
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-99
A310/A310 Pneumatic System – Air Bleed System Components and Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1010
Electronic Rack 90VUElectronic Rack 90VU
ENGINE 2
ENGINE 1
AvionicsAvionicsBayBay
FWDFWD
A300/A310 Pneumatic System Controllers and 103VU Relay Panel - Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1111
A300 Air Bleed System Panel Locations – Controls and Indicating
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1212
COMPT TEMP/AIR BLEED Panels 436 / 437 VU
436VU
437VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1313
A300/A310 AIR BLEED Panel 436VU – Bleed Valve Indications
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1414
A300/A310 AIR BLEED Panel 436VU – Bleed Valve Indications
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1515
A300/A310 AIR BLEED Panel 436VU – Bleed Valve Indications
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1616
A300/A310 AIR BLEED Panel 436VU – X FEED (Crossfeed) Control and Indicating
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1717
A300/A310 ECAM System – ECAM Control Panel and RH ECAM Display
ECAM CONTROL PANEL
RH ECAM
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1818
A300/A310 RH ECAM Display Unit – AIR BLEED Page
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-1919
A300/A310 RH ECAM Display Unit – AIR BLEED Page
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2020
A300/A310 RH ECAM Display Unit – AIR BLEED Page
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2121
A300 HP Valve - Manual Override/Visual Position Indicator
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2222
PW JT9-7R4 Engine 1PW JT9-7R4 Engine 1
A310 Pneumatic System High Pressure (HP) Bleed Valve FIN DV225 (DV226)
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2323
JT9D-7R4 EngineJT9D-7R4 Engine
A310 Pneumatic System - High Pressure (HP) Valve - Installation Features
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2424
GE CF6-80C2A5F EngineGE CF6-80C2A5F EngineOne Valve per EngineOne Valve per EngineEngine 1 - FIN A004Engine 1 - FIN A004Engine 2 - FIN B004Engine 2 - FIN B004
*IP - Intermediate Pressure*IP - Intermediate Pressure *IP*IP
A300 Pneumatic System - 8th Stage Check Valve FIN A004 (B004) - Installation
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2525
PW JT9D-7R4 EnginePW JT9D-7R4 EngineTwo Valves per EngineTwo Valves per Engine
Engine 1 - FIN B004Engine 1 - FIN B004Engine 2 - FIN D004Engine 2 - FIN D004
A310 Pneumatic System - 8th Stage Check Valves - Component Installation
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2626
A300 Pneumatic System - Bleed Valve (Pressure Regulating and Shutoff/PRSOV)
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2727
A300 Pneumatic System - Bleed Air Valve FIN DV224 (Eng 1/2) - Component Installation
GE CF6-80C2A5F
ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2828
A310 Bleed Air System - Bleed and Pressure Regulator Shutoff Valve - Component Features
JT9D-7R4 EngineJT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-2929
JT9D-7R4 EngineJT9D-7R4 Engine
A310 Bleed Air System - Bleed and Pressure Regulator Shutoff Valve - Component Installation
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3030
JT9D-7R4 EngineJT9D-7R4 Engine
A310 Bleed Air System - Bleed and Pressure Regulator Shutoff Valve - Lockout and Filters
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3131
A310 - Bleed Air System Overpressure Valve (OPV) - Component Installation
PW JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3232
Engine Bleed Air System - Over Pressure Valve (OPV) - Schematic and Features
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3333
A300/A310 Bleed Air System - Overpressure Valve - Component Installation
GE CF6-80A3 ENGINE ANDGE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3434
A300 Bleed Air System - Fan Air Valve (FAV) FIN 51HA (52HA) - Component ValveIdentification Names
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3535
Ambient Air to PrecoolerAmbient Air to Precooler(Heat Exchanger)(Heat Exchanger)
NOTE:NOTE:FAV - On AircraftFAV - On Aircraft
N650FE to N653FEN650FE to N653FE
A300 Bleed Air System - Fan Air Valve (FAV) - Component Features
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3636
A300 Bleed Air System - Fan Air Valve (FAV) - Mechanical Lockout and Test Port
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3737
FAV Air FilterFAV Air FilterFAV Engine 1 - FIN 51 HAFAV Engine 1 - FIN 51 HAFAV Engine 2 - FIN 52 HAFAV Engine 2 - FIN 52 HA
A300 Engine Bleed Air System - Fan Air Valve (FAV) - Filter Element
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3838
AircraftAircraftConfiguration 01Configuration 01
A310 Fan Air Valve (FAV) FIN 51HA (52HA) - General View
JT9D-7R4 EngineJT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-3939
PlugPlug
GasketGasket
SpringSpring
FilterFilter
A310 Bleed Air System - Fan Air Valve (FAV) - Air Filter Element
Aircraft Configuration 02Aircraft Configuration 02
PW JT9D-7R4 Engine
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4040
A300/A310 Bleed Air System - Cooling Air Inlet Duct to Precooler Base Unit
NOTE
COOLING AIR EXTRACTED
FROM FAN AIR STREAMTO THE FAN AIR VALVE(FAV) IS DUCTED TO THEPRECOOLER BASE UNIT.
COOL FAN AIR ISDIRECTED THROUGH THEBLEED AIR SYSTEMPRECOOLER UNIT FORCOOLING HOT BLEED AIRFOR PNEUMATIC USERS.
THE USED COOLING AIR ISDIRECTED OVER BOARDON TOP OF THE PYLONASSEMBLY TO LOUVEREDPANEL ASSEMBLY.
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4141
A300/A310 Pneumatic Bleed Air System Precooler - Component Installation
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4242
Regulator PressureRegulator Pressure Sensor Sensor
High StageHigh StagePressure SensorPressure Sensor
A300/A310 Pneumatic System - Sensors - Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4343
A300/A310 Wing-to-Pylon Connection - Component Installation and Sensors
PRECOOLER TEMPERATURECONTROL SENSOR
FIN 53HA (54HA)
PRECOOLER OUTLETTEMPERATURE SENSOR
FIN 4HX (5HX)
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4444
A300/A310 Pneumatic System - Pressure Sensors - Pylon Location
RegulatorRegulator Pressure Sensor Pressure SensorFIN 49HA (50HA)FIN 49HA (50HA)
UPPER UNITUPPER UNIT
A300 SHOWN
High StageHigh StagePressure SensorPressure SensorFIN 47HA (48HA)FIN 47HA (48HA)
LOWER UNITLOWER UNIT
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4545
RegulatorRegulatorPressure SensorPressure Sensor
High StageHigh StagePressure SensorPressure Sensor
PRECOOLER OUTLETTEMPERATURE SENSOR4HX (5HX)
A310 Pneumatic System - Pressure Sensors - Installation of Sensors
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4646
Warning Logic - Engine Bleed Air WarningWarning Logic - Engine Bleed Air WarningDepicted below are various warnings displayed in the Flight Deck in the event a fault occurs in the aircraft pneumaticDepicted below are various warnings displayed in the Flight Deck in the event a fault occurs in the aircraft pneumaticsystem. Also graphically shown are the various flight phases at which warnings will or will not be shown.system. Also graphically shown are the various flight phases at which warnings will or will not be shown.
Warning Logic - JT9D Engine Bleed Air System
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4747
WLDPWLDP
A310 PW JT9D-7R4 Engine Bleed Air Warning Logic - Configuration 01
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4848
Warning Logic - Engine Bleed Air WarningWarning Logic - Engine Bleed Air WarningDepicted below are various warnings displayed in the Flight Deck in the event a fault occurs in the aircraft pneumaticDepicted below are various warnings displayed in the Flight Deck in the event a fault occurs in the aircraft pneumaticsystem. Also graphically shown are the various flight phases at which warnings will or will not be shown.system. Also graphically shown are the various flight phases at which warnings will or will not be shown.
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-4949
A310 PW JT9D-7R4 Engine Bleed Air Warning Logic - Configuration 01
WLDPWLDP
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5050
FWDFWD
GE CF6-80C2A5F EngineGE CF6-80C2A5F Engine
FIN T603 -FIN T603 -Engine 1/2Engine 1/2
FADECFADEC
A300 Pneumatic System - High Stage Temperature Sensor (T3) - Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5151
A310 Pneumatic System - High Stage Temperature Sensor - Component Installation
PW JT9D-7R4 ENGINEPW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5252
A300 BLEED AIR SYSTEM - 14th Stage Manifold - Component Installation
GE CF6-80C2A5F ENGINEENGINE NUMBER 1
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5353
A300 BLEED AIR SYSTEM - 8th Stage Manifold - Component Installation
GE CF6-80C2A5F ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5454
To Left Hand side ofTo Left Hand side ofEngine to PRSOVEngine to PRSOV
(Bleed Valve(Bleed Valve))
A310 BLEED AIR SYSTEM- Low Pressure Bleed Air Check Valve and Duct Assembly Component Installation
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5555
From 8 th StageEngine Port(RH Side of
Engine)
To Precooler(Heat Exchanger)
Air Flow
StarterAir Duct
AirFlow
PS4 Air
PS4 Air
15th Stage(PS4 Air) Air
Flow In
**8th StageAir Flow In
*Bleed Air Port forHydraulic ReservoirSystem- Engine 1 only- Engine 2 Plug inserted in port hole.
A310 BLEED AIR SYSTEM - 8th and 15th Stage Collector Duct Assembly - Component Installation
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5656
A310 BLEED AIR SYSTEM - Left 8th Stage Low Pressure Bleed and Duct AssemblyComponent Installation
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5757
88thth/15/15thth
Stage AirStage AirFlow OutFlow Out
Air Flow to PrecoolerAir Flow to Precooler
Air Flow OutAir Flow Out
A310 BLEED AIR SYSTEM - Bleed Air Pressure Regulator Valve Outlet Duct AssemblyComponent Installation
PW JT9D-7R4 ENGINE
PRSOV
PRSOV = PRESSUREREGULATING SHUT OFF
VALVE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5858
DiffuserDiffuserSectionSection
**PS4 AirPS4 AirFlow OutFlow Out
**
****
**
A310 BLEED AIR SYSTEM - 15th State High Pressure Manifold - Component Installation
PW JT9D-7R4 ENGINE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-5959
A300/A310 Pneumatic Bleed Air Duct - Clamp Location and Features (Typical)
WING FRONT SPAR AREA
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6060
A300/A310 Bleed Air Duct - Clamp Installation and Duct Alignment
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6161
Some A310 Pneumatic System Controller / GE CF6-80A3 and PWJT9D-7R4 Engines - (Front Face Labels - BITE Check)
FIN 41HA (42HA)FIN 41HA (42HA
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6262
A300 / Some A310 Pneumatic System Controller - Front Face
FIN 41HA (42HA)
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6363
or PW Engineor PW Engine
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram
FIN 41HA (42HA)
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6464
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram 1
FIN 41HA (42HA)
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6565
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram 2
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6666
A300 / Some A310 Pneumatic Controller - Initiated Built-In-Test Flow Diagram 3
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6767
A300/A310 APU Bleed Air System - Flight Deck Controls and Indications
AIR BLEED PANEL 436VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6868
A300/A310 APU Bleed Air System - Component Location in Fuselage
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-6969
Only on some A310s
A300/A310 Pneumatic System – High Pressure (HP) Ground Connectors – Component Location
A310 SHOWN
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7070
A300/A310 APU Bleed Air and Crossfeed - Schematic
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7171
A300/A310 Bleed Air System – Crossfeed (X-FEED) Valve FIN 16HV – Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7272
A300/A310 Bleed Air System – Crossfeed Valve (X-FEED) FIN 16HV – Component Installation
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7373
Located in Bulk CargoLocated in Bulk CargoBay Area – Above andBay Area – Above andAft of Bulk Cargo DoorAft of Bulk Cargo Door
A300/A310 APU Bleed Air – Component Location in Fuselage
APU ECB UNIT
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7474
A300/A310 APU Bleed Air System – Bleed (Load Control) Valve FIN 66KD - General Features
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7575
A300 / Some A310 APU Bleed Air System – Check Valve FIN 360022 – Component Installation
NOTESOME A310 HAVE SIX
(PIE CUT SHAPE) FLAPPER TYPECHECK VALVE COMPONENT UNITS
WITH SPRINGS TO RESEAT FLAPPERUNDER NO PNEUMATIC LOAD
CONDITIONS
DOUBLE FLAPPERTYPE CHECK
VALVE
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7676
NACA = National Advisory Committee ofNACA = National Advisory Committee ofAeronautics U. S. A.Aeronautics U. S. A.
- Now NASA Since 1958.- Now NASA Since 1958.
A300/A310 Wing Leading Edge Air Cooling Area (Slat Number 1 Area)- General Features
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7777
A300/A310 Pneumatic System - Overheat Detection Controllers - Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7878
A300/Some A310s Maintenance Panel 472VU - AIR BLEED & COMPT TEMP Test Panel
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-7979
A300/A310 Air Bleed - Monitoring and Bleed Fault Test - Flight Deck Configurations
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8080
A300/A310 Air Bleed System - Manifold Air Leak Test Panel
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8181
A300/A310 Pneumatic System - Control and Indicating - Location
COMPT TEMP PANEL 437VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8282
A300/A310 Pneumatic System - Bleed Air Pressure Indication - Overhead Panel 437VU
COMPT TEMP PANEL 437VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8383
A300/A310 PRECOOLER OUTLET TEMP - SCHEMATIC
MAINTENANCE PANEL 471VU
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8484
A300/A310 Manifold Air Leak Detection - Controls and Indications - Location
MAINTENANCE PANEL 471VU
90VU ELECTRONIC RACK
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8585
A300/A310 Pneumatic System - Overheat Detection Controller FIN 12HF/13HF - Location
90VU ELECTRONIC RACK
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8686
A300/A310 Manifold Air Leak Detection - Detection Loops Layout
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8787
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 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8888
A300/A310 Wing Overheat Detection - Loop Sections Layout
A300 SHOWN
ALL AREAS SHOWN -124 DEGREES C
DOUBLE LOOPS
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-8989
A300/A310 Pneumatic System - Overheat Sensing Elements - Location in Fuselage
A310 SHOWN
ALL AREAS SHOWN - 124 DEGREES C
DOUBLE LOOPS
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9090
A300/A310 Aft Fuselage Overheat Detection - Overheat Sensing Elements
154 DEGREE CSINGLE LOOP
124 DEGREE C SINGLE LOOP
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9191
A300/A310 Manifold Air Leak Detection - Ambient Overheat Detection Loop
GROMMET
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9292
NOTENOTESome A310 have Master Caution Lights and other A310 haveSome A310 have Master Caution Lights and other A310 have
WLDP (WARNING LIGHT DISPLAY PANEL)WLDP (WARNING LIGHT DISPLAY PANEL)
A300/A310 Pneumatic System - Manifold Leak Detection - Schematic
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9393
GE CF6-80C2A5F (FADEC Engine)GE CF6-80C2A5F (FADEC Engine)
A300/A310 Engine Bleed System - Troubleshooting Guidelines and Information
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9494
A300/A310 Engine Bleed System - Troubleshooting Guidelines and Information
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9595
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9696
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9797
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9898
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-9999
A300 Engine Bleed Air System - Troubleshooting Guidelines and Component Location
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-100100
A310 Bleed Air Pneumatic Controller FIN 41HA (42HA) - BITE Test
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-101101
A300/A310 Bleed Air Pneumatic Controller FIN 41HA (42HA) - BITE Sequence
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-102102
Warning Logic - Pneumatic System
Depicted below are various warnings displayed in the flight deck in the event a fault occurs in theaircraft Pneumatic System. Also graphically shown are the various Flight Phases at which warningswill or will not be shown.
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-103103
Warning Logic - Pneumatic System
MTT M540000 / R3.3 01AUG01MTT M540000 / R3.3 01AUG01For Training Purposes OnlyFor Training Purposes Only
ATA 36ATA 36A300/A310A300/A310
36-36-104104
THIS PAGE INTENTIONALLY
LEFT BLANK
ATA 36 - END
COURSE CODE - M450000