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┃ aw aw ,, ~L,~ A319             ┃                ┃                      ┃
┃                                ┃                ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃                ┃SEQ 100 I ┃I REV 24  ┃
┃      A~7-~'M" A321             ┃  NORMAL LAW    ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━━┻━━━━━┛
LEFT INTENTIONALLY BLANK
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                          ┃1.27.20     P 8       ┃
┃                                ┃                          ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃I        FLIGHNORMALRLAW  ┃SEQ 005 1 ┃I REV 23  ┃
┃  .,,,.8, ,, ~L,~ A319          ┃                          ┃          ┃          ┃
┃ Lli,~ A320                     ┃                          ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                          ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                          ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
If one engine fails, the FAC modifies the sideslip indication slightly to show the pilot how
much rudder to use to get the best climb performance (ailerons to neutral and spoilers
retracted).
In takeoff configuration (1,2,3) when the FAC detects asymmetric thrust (35 % N1) and at
least one engine is above 80% N1, the slideslip indication on the PFD changes from yellow
Io blue.
The pilot's response is normal and instinctive ~ zero the slip indication by applying the right
amount of rudder to get the best climb performance.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━┓
┃I  -~ A318                      ┃         FLIGHT CONTROLS      ┃1.27.30     P 1   ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(88)