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outboard engines. For this purpose, the thrust lever is limited at reverse idle, until both EIU 1 and 4
have released the interlock, confirming that both thrust reversers are fully deployed.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A330/A340 FLEET DSC-70-70 P 5/8
FCOM 19 AUG 10
IDLE PROTECTION
Applicable to:
The FADEC will automatically select idle thrust, if the reverse thrust is not selected and one of three
following conditions occurs :
‐ 4 doors are unstowed or,
‐ at least one door is unstowed and the thrust reverser system is pressurized, or
‐ the thrust reverser position is not determined and the reverser system is pressurized.
PROTECTION
Applicable to: ,
AUTO RESTOW FUNCTION AND IDLE PROTECTION
The FADEC will automatically command the engine to idle and the reverser to stow if at least one
door is unstowed by more than 5 % and reverse thrust is not selected while engine is running. The
affected reverser will remain pressurized after affected door is locked back.
If the door is still detected unstowed the engine will remain at idle for the rest of the flight.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A330/A340 FLEET DSC-70-70 P 6/8
FCOM 19 AUG 10
SCHEMATIC
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A330/A340 FLEET DSC-70-70 P 7/8
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A330/A340 FLEET DSC-70-70 P 8/8
FCOM 19 AUG 10
SCHEMATIC
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
A330/A340 FLEET DSC-70-80-10 P 1/6
FCOM 19 AUG 10
GENERAL
Applicable to: ,
The ignition and starting system is controlled by the FADEC, according to the :
‐ Engine start selector position
‐ Engine master switch position
‐ ENG MAN START pushbutton position
‐ ENG ANTI ICE pushbutton position
‐ Flight/ground aircraft condition.
In normal operation, the FADEC receives its inputs from the EIU.
In the event of an EIU signal loss, all the functions, except manual start and wet crank, will remain
available by using both a backup signal from the engine master switch, and the alternate start/ignition
signal.
GENERAL
Applicable to:
The ignition and starting system is controlled by the FADEC, according to the :
‐ Engine start selector position
‐ Engine master switch position
‐ ENG MAN START pushbutton position
‐ Flight/ground aircraft condition.
In normal operation, the FADEC receives its inputs from the EIU.
In the event of an EIU signal loss, all the functions, except manual start and wet crank, will remain
available by using both a backup signal from the engine master switch, and the alternate start/ignition
signal.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
A330/A340 FLEET DSC-70-80-10 P 2/6
FCOM 19 AUG 10
ARCHITECTURE
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
A330/A340 FLEET DSC-70-80-10 P 3/6
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
A330/A340 FLEET DSC-70-80-10 P 4/6
FCOM 19 AUG 10
ARCHITECTURE
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
A330/A340 FLEET DSC-70-80-10 P 5/6
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
Intentionally left blank
A330/A340 FLEET DSC-70-80-10 P 6/6
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - IGNITION SYSTEM
A330/A340 FLEET DSC-70-80-20 P 1/4
FCOM 19 AUG 10
GENERAL
Applicable to:
The ignition system is used to start the engine on ground, and to restart it in flight.
It consists of two identical independent circuits for each engine, normally controlled by the FADEC’s
channel A, with channel B on standby. Each FADEC channel can control both igniters.
GENERAL
Applicable to: ,
The ignition system is used to start the engine on ground, and to restart it in flight.
　
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