曝光臺 注意防騙
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┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃
┃ Lii,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃ INDICATIONS ON E/WD ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━┻━━━━┛
GENERAL
The FWC divides its functions according to these ten flight phases
To improve its operational efficacy, the computer inhibits some warnings and cautions for
certain flight phases. It does so to avoid alerting the pilots unnecessarily at times when
they have high workloads, such as during takeoff or landing. In these two phases, the DU
displays magenta memos : "T.O. INHIBIT" (flight phases 3, 4, and 5), and "LDG INHIBIT"
(flight phases 7 and 8).
Note ~ These flight phases are different from and independent of the ones that the FMGC
uses.
FLIGHT PHASE INHIBITION
Two cases are possible (for instance)
~ FAILURE APPEARANCE
┏━┳━┳━┳━┓
┃ ┃ ┃ ┃ ┃
┗━┻━┻━┻━┛
INHIBITED
PHASE
Effect on E/WD
~
~
FLIGHT PHASES INHIBITION
The failure occurs during phase 1. The
continues to display it as long as the fa
E/WD displays the warning immediately and
lure is present, even in phase 2.
The failure occurs during phase 2. The E/WD displays the warning only when the aircraft
has entered phase 3, where it is not inhibited. Then the warning remains displayed as
long as the failure is present.
EEM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.31.15 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I INDICATIINDICATIONSGONYE/WDS ┃SEQ 100 1 ┃I REV 33 ┃
┃ .-,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
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本文鏈接地址:
AIRBUS A320 Flight Crew Operating Manual4(27)