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• The door position is indefinite, and hydraulic pressure is detected in the HCU (downstream of
the pressurizing valve).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A318/A319/A320/A321 FLEET DSC-70-70 P 7/12
FCOM 19 AUG 10
SCHEMATIC
Applicable to: MSN
4566,,,
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A318/A319/A320/A321 FLEET DSC-70-70 P 8/12
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A318/A319/A320/A321 FLEET DSC-70-70 P 9/12
FCOM 19 AUG 10
SCHEMATIC
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A318/A319/A320/A321 FLEET DSC-70-70 P 10/12
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A318/A319/A320/A321 FLEET DSC-70-70 P 11/12
FCOM 19 AUG 10
SCHEMATIC
Applicable to: ,
, MSN
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
THRUST REVERSER SYSTEM
A318/A319/A320/A321 FLEET DSC-70-70 P 12/12
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
A318/A319/A320/A321 FLEET DSC-70-80-10 P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The FADEC controls the ignition and starting system according to :
the position ‐ of the engine start selector
‐ the position of the ENG MASTER switch
‐ the position of the ENG MAN START pushbutton switch
‐ the position of the ENG 1(2) ANTI ICE pushbutton switch
‐ the aircraft status (flight or ground).
The FADEC receives its inputs from the Engine Interface Unit (EIU).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - GENERAL
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-70-80-10 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - ARCHITECTURE
A318/A319/A320/A321 FLEET DSC-70-80-20 P 1/2
FCOM 19 AUG 10
ARCHITECTURE
Applicable to: ALL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - ARCHITECTURE
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-70-80-20 P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - IGNITION SYSTEM
A318/A319/A320/A321 FLEET DSC-70-80-30 P 1/4
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The ignition system is for engine starting on the ground and restarting in flight. It consists of two
identical independent circuits for each engine, normally controlled by the FADEC channel A and
channel B. Each FADEC channel can control both igniters.
Note: Supply for igniter A switches to the STAT INV BUS BAR as soon as the static inverter is
operative.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - IGNITION SYSTEM
A318/A319/A320/A321 FLEET DSC-70-80-30 P 2/4
FCOM 19 AUG 10
IGNITION FOR STARTING
Applicable to:
, ,
MSN
ON THE GROUND
‐ Automatic start :
• Only one igniter fires.
• The FADEC automatically alternates the igniters used on successive starts following the
sequence below :
▪ channel A, igniter A
▪ channel B, igniter A
▪ channel A, igniter B
▪ channel B, igniter B
• The ignition comes on automatically when N2 reaches 16 % and cuts off automatically when
N2 reaches 50 %.
‐ Manual start :
• Both igniters start firing when the MASTER switch is switched ON.
• Both stop firing when N2 reaches 50 %.
IN FLIGHT
‐ Both igniters start firing when the MASTER switch is switched ON.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
POWER PLANT
IGNITION AND STARTING - IGNITION SYSTEM
A318/A319/A320/A321 FLEET DSC-70-80-30 P 3/4
FCOM 19 AUG 10
IGNITION FOR STARTING
Applicable to: MSN
4566,,,
ON THE GROUND
‐ Automatic start :
• Only one igniter fires.
• The FADEC automatically alternates the igniters used on successive starts.
　
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