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┃I  -~ A318                      ┃         FLIGHT CONTROLS      ┃1.27.30     P 3   ┃
┃  .*,,.8, ,, ~L,~ A319          ┃                              ┃                  ┃
┃ Lli,~ A320                     ┃                              ┃                  ┃
┃                                ┃                              ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃RECONFIGURATION CONTROL LAWS  ┃SEQ 001 ┃REV 23  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                              ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━┻━━━━┛
 FAILURE
(SEE p.2)
L/G  DOWN                        A/C  ON  GRND
   (1)
(1) OR SLATS OR FLAPS ~  2 IF LGCIU 1+2 FAULT
(2) OR SLATS OR FLAPS <  2 IF LGCIU 1+2 FAULT
PITCH CONTROL
GROUND MODE
Under alternate law the ground mode becomes active on the ground five seconds after
touchdown.
It is identical to the ground mode of the normal law.
FLIGHT MODE
n flight, the alternate law pitch mode follows a load-factor demand law much as the norma
aw pitch mode does, but it has less built-in protection (reduced protections).
FLARE MORE
In pitch alternate law the flight mode changes to the flare mode when the pilot selects
landing gear down. The flare mode is a direct stick-to-elevator relationship.
(See DIRECT LAW).
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                                ┃1.27.30     P 4       ┃
┃                                ┃                                ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃I RECONFIGURATIONOCONTROL LAWS  ┃SEQ 001 1 ┃I REV 23  ┃
┃  .,,,.8, ,, ~L,~ A319          ┃                                ┃          ┃          ┃
┃ Lli,~ A320                     ┃                                ┃          ┃          ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(90)