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- 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 (ElU)
 ARCHITECTURE ]
                 ON PEDESTAL
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┃                                ┃                                ┃1.70.80     P 2       ┃
┃                                ┃                                ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃l        IGNITIONLAND STARTING  ┃SEQ 005 1 ┃I REV 31  ┃
┃ aw aw ,, ~L,~ A319             ┃                                ┃          ┃          ┃
┃ Lli,~ A320                     ┃                                ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                                ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                                ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
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.
┏━┳━━━━━━━━━━┳━━┓
┃| ┃          CHANNEL A ┃    ┃
┃  ┃-  ^~ COMMAND       ┃    ┃
┣━╋━━━━━━━━━━╋━━┫
┃J ┃~CH~ANNEL B         ┃ y  ┃
┃  ┃                    ┃IGr ┃
┃  ┃          COMMAND   ┃    ┃
┃  ┃          CHANNEL A ┃    ┃
┃  ┃-  ~COM_MAND        ┃    ┃
┣━╋━━━━━━━━━━╋━━┫
┃i ┃~ CH~ANNEL B        ┃ y  ┃
┃  ┃                    ┃IGr ┃
┃  ┃          COMMAND   ┃    ┃
┃  ┃       FADEC        ┃    ┃
┗━┻━━━━━━━━━━┻━━┛
ITER A
ITER B
Note : Supply for igniter A switches to the STAT INV BUS BAR as soon as the static
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(169)