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┃                            ┃   S/F ID~1~NDED~ ~ r~/ ~]IPBASE 6~  ~ < 16000 Ft                                       ┃                  ┃
┃                            ┃        NO T.0. PtlR                                                                  i ┃,=                ┃
┃                            ┃                                                                                        ┃        t         ┃
┃              I             ┃         @                  ~ ~"                                                        ┃1~,  i            ┃
┗━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┻━━━━━━━━━┛
   ~ Phase 2 : The F/CTL page replaces the WHEEL page for 20 seconds when either pilot
    moves his sidestick (more than 3~ in pitch or roll) or when the rudder pedal deflection
    is more than 22~.
   ~ The APU page appears when the APU MASTER switch is ON. It disappears when APU
    RPM has been above 95 % for 10 seconds, or when the APU MASTER switch is
    switched OFE
   ~ The ENGINE page appears at the beginning of start sequence or when a pilot selects
    "CRANK". It disappears 10 seconds after the end of the start sequence, when the ENG
    MODE sel is set to NORM.
For a description of the ENGINE and AIR indications that appear when the SD is displaying
the CRUISE page, see the relevant FCOM chapter.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                                ┃1.31.20     P 4       ┃
┃                                ┃                                ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃I INDICATININDICATIONS ONSSDMS  ┃SEQ 001 1 ┃I REV 24  ┃
┃ aw aw ,, ~L,~ A319             ┃                                ┃          ┃          ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual4(32)