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is no residual cabin pressure.
At touchdown, any remaining cabin pressure is released at a cabin vertical speed of 500
feet/minute.
Takeoff (TO)
To avoid a pressure surge at rotation, the controller prepressurizes the aircraft at a rate of
500 feet/minute, until the AP reaches 0.1 psi.
At liftoff, the controller initiates the climb phase.
Climb (CL)
During climb, the cabin altitude varies according to a fixed preprogrammed law that takes
into account the aircraft's actual rate of climb.
Cruise (OR)
During cruise, the controller maintains cabin altitude at level-off value, or the landing field
elevation, whichever is higher.
Descent (DE)
During descent, the controller maintains a cabin rate of descent such that cabin pressure
reaches landing field pressure just before the landing.
The maximum descent rate is 750 feet/minute.
Abort (AB)
The abort mode prevents the cabin altitude from climbing, if the aircraft does not climb after
takeoff.
Cabin pressure is set back to the takeoff altitude + 0.1 psi.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                              ┃1.21.20     P 6       ┃
┃                                ┃                              ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃l      AIR CONDPRESSURIZATION ┃SEQ 001 1 ┃I REV 23  ┃
┃  aw aw ,, ~4W~ A319            ┃                              ┃          ┃          ┃
┃ Lii,~ A320                     ┃                              ┃          ┃          ┃
┃      A~7-~'iP" A321            ┃                              ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                              ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
PRESSURIZATION MODES SWITCHING
┏━━━━━━━━━━━━━━━━━━━━━━━━━┳━━┳━━┳━━┳━━┳━━┳━━┳━━┳━━┳━━┳━━┳━━┳━━┓
┃FROM                                              ┃GN  ┃TO  ┃GN  ┃CL  ┃AB  ┃TO  ┃CL  ┃CR  ┃CR  ┃DE  ┃DE  ┃AB  ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━╋━━╋━━╋━━╋━━╋━━╋━━╋━━╋━━╋━━╋━━╋━━╋━━┫
┃TO                                                ┃TO  ┃CL  ┃CL  ┃AB  ┃GN  ┃GN  ┃CR  ┃CL  ┃DE  ┃CL  ┃GN  ┃CL  ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual1(108)