曝光臺 注意防騙
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(engine failure, landing gear extended) or when operating near closely
spaced runways, or
~ automatically, when the following messages are triggered :
- windshear (<~)
- stall
- GPWS messages
Consequently :
~ All RAs are inhibited and converted into TAs
~ the TA threshold is set to TAU _< 20 seconds, irrespective of the aircraft's
altitude.
~ No vertical speed advisories are indicated on the PFDs
~ "TA ONLY" is displayed on the NDs
If windshear, stall or GPWS messages are triggered, all the TCAS aural
messages are suppressed.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.34.80 P 6 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I NAVIGATITCAS ┃SEQ 150 1 ┃I REV 28 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━━┻━━━━━┛
ADVISORY INHIBITION
Some advisories are inhibited depending on the aircraft altitude :
- all intruders flying below 380 feet AGL when the own aircraft altitude is below 1700 feet
AGL.
- all RA below 1100 feet in climb and 900 feet in descent. In this case, the RAs are
converted into TAs.
- "Descend" type advisory below 1200 feet AGL at takeoff or 1000 feet AGL in approach.
- "Increase Descent" RA below 1450 feet.
- all TA aural messages below 500 feet AGL
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃NAVIGATION ┃1.34.80 P 7 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual4(115)
