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If one channel fails, the other automatically takes control.
The system has a magnetic alternator for an internal power source.
FADEC is mounted on the fan case.
The Engine Interface Unit (EIU) transmits to FADEC the data it uses for engine management.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                          ┃1.70.20     P 2       ┃
┃                                ┃                          ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃l         POWER PLAFADEC  ┃SEQ 105 1 ┃I REV 24  ┃
┃ aw aw ,, ~L,~ A319             ┃                          ┃          ┃          ┃
┃ Lli,~ A320                     ┃                          ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                          ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                          ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃I  -~ A318                      ┃POWER PLANT ┃1.70.20     P 3   ┃
┃  .*,,.8, ,, ~L,~ A319          ┃            ┃                  ┃
┃ Lli,~ A320                     ┃            ┃                  ┃
┃                                ┃            ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃     FADEC  ┃SEQ 001 ┃REV 23  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
The FADEC system performs the following functions
Control of gas generator
~ control of fuel flow
~ acceleration and deceleration schedules
~ variable bleed valve and variable stator vane schedules
~ control of turbine clearance
~ idle setting
Protection against engine exceeding limits
~ protection against N1 and N2 overspeed
~ monitoring of EGT during engine start
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(153)