曝光台 注意防骗
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┃ ┃ ┃1.34.70 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-~ A318 ┃I NAVIGATIGPWS ┃SEQ 109 1 ┃I REV 25 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━━┻━━━━━┛
MODE 2 : EXCESSIVE TERRAIN CLOSURE RATE
I,J-
LIJ
'< I--
I,-I
<: ,~
2450
RA RATE OF CHANGE (FT/MINXlO00)
2A -- Flaps not in landing configuration and aircraft not on the glide slope beam.
Penetration of the boundary lights up the GPWS lights and sounds the repeated aural alert:
"TERRAIN".
After "TERRAIN" has sounded twice, the warning switches to "PULL UP", repeated
continually until the aircraft leaves the warning envelope.
After the aircraft leaves the boundary, the GPWS lights stay on and the voice message
"TERRAIN" persists. These alerts cease when the aircraft increases either the barometric
or inertial altitude by 300 feet. If it enters another alert region during this altitude-gain time,
then the whole process begins again with a new reference altitude for the 300 feet altitude
gain.
* Upper cut-off limit varies from 1650 feet to 2450 feet radio altitude, depending on
speed (between 220 knots to 310 knots). At certain airports, the upper boundary
may be lowered down to 1250 feet to reduce the warning sensitivity and minimize
the nuisance warnings.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃NAVIGATION ┃1.34.70 P 5 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 110 I ┃I REV 29 ┃
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AIRBUS A320 Flight Crew Operating Manual5(59)
