曝光台 注意防骗
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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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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual1(108)
