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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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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual4(101)