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┃ ┃ ┣━━━━━┳━━━━━┫
┃ aw aw ,, ~L,~ A319 ┃I NAVIGATIGPWS ┃SEQ 103 1 ┃I REV 35 ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━━┻━━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃I -~ A318 ┃NAVIGATION ┃1.34.70 P 3 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lli,~ A320 ┃ ┃SEQ 100 I ┃I REV 26 ┃
┃ A~7-~'M" A321 ┃ GPWS ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
MODE 1: EXCESSIVE RATE OF DESCENT
SINK RATE (FT/RIN X IO00)(ZNERTIAL VERTZCAL SPEED)
Mode 1 has two boundaries. Penetration of the first boundary generates the illumination of
the GPWS light and a repeated aural alert "SINK RATE". Penetration of the second boundary
generates a repetitive "PULL UP".
The upper cut-off limit is 2450 feet radio altitude.
The lower cut-off limit is 10 feet radio altitude.
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.34.70 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-~ A318 ┃I NAVIGATIGPWS ┃SEQ 109 1 ┃I REV 25 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃ ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual4(101)
