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┃ aw aw ,, ~L,~ .4319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
BMC FAILURE
If one BMC fails, the adjacent BMC takes over the monitoring of the bleed system to issue
the following ECAM warnings if necessary :
- overpressure
- overtemperature
- wing leak.
Nevertheless, the associated FAULT light on the AIR COND panel is lost, and the associated
bleed valve does not close automatically.
ENG BLEED LEAK warning is lost for the associated engine, as is also the APU BLEED LEAK
warning if BMC1 has failed.
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃ PNEUMATIC ┃1.36.20 P 1 ┃
┃ .-,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃CONTROLS AND INDICATORS ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━┻━━━━┛
ENG 1 and ENG 2 BLEED pb sw
On
Bleed valve opens if :
- Upstream pressure is above 8 psi.
- APU BLEED pushbutton switch is off or
There is no onside wing or pylon
overtemperature has been detected.
APU bleed valve is closed.
eak, and no overpressure or
- The ENG FIRE pushbutton has not been popped out.
- The engine start valve is closed.
FAULT It : This amber light comes on, and an ECAM caution appears, if :
- There is an overpressure downstream of the bleed valve.
- There is a bleed air overheat.
- There is a wing or engine leak on the related side.
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual5(17)
