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┃      A~7-~'M" A321             ┃CONTROLS AND INDICATORS ┃SEQ 001 ┃REV 23  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                        ┃        ┃        ┃
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┃                                ┃                              ┃1.27.40     P 6       ┃
┃                                ┃                              ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃I     CONTROLSTANDNINDICATORS ┃SEQ 100 1 ┃I REV 24  ┃
┃  .,,,.8, ,, ~L,~ A319          ┃                              ┃          ┃          ┃
┃ Lli,~ A320                     ┃                              ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                              ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                              ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
O ELAC 1(2) pb sw
Controls the elevator and aileron control (ELAC) computer 1(2).
ON     ELAC 1(2) performs the following functions :
          - normal pitch and roll
          - alternate pitch
          - direct pitch and roll
          - abnormal attitude
          - aileron droop
          - acquisition of autopilot orders.
OFF    The corresponding computer is not active. Switching it OFF and then ON resets
          the computer.
FAULT  Lights up in amber, along with a "CAUTION" advisory on ECAM :
          - when a failure is detected
          - during ELAC power-up test (eight seconds).
Note : ELAC power-up test occurs when electrical power is turned on or after
       the occurrence of an electrical transient lasting longer than 25
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(97)