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Power management
~ automatic control of engine thrust rating
~ computation of thrust parameter limits
~ manual management of power as a function of thrust lever position
~ automatic management of power (A/-rHR demand).
Automatic engine starting sequence
control of :
- the start valve (ON/OFF)
- the HP fuel valve
- the fuel flow
- the ignition (ON/OFF)
monitoring of N1, N2, FF and EGT
initiation of abort and recycle (on the ground only)
Manual engine starting sequence
~ passive monitoring of engine
~ control of :
- the start valve
- the HP fuel valve
- the ignition
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.70.20 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃l POWER PLAFADEC ┃SEQ 001 1 ┃I REV 23 ┃
┃ .,,,.8, ,, ~e~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
Thrust reverser control
actuation of the blocker doors
engine setting during reverser operation
Fuel recirculation control
recirculation of fuel to the fuel tanks according to the engine oil temperature, the fue
system configuration and the flight phase.
Transmission of engine parameters and engine monitoring information to cockpit
indicators
the primary engine parameters
the starting system status
the thrust reverser system status
the FADEC system status
Detection, isolation, and recording of failures
FADEC cooling
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃I ~-~ A318 ┃POWER PLANT ┃1.70.20 P 5 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 005 I ┃I REV 28 ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual5(154)
