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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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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual4(32)
