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┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
Leak detection loops detect any overheating near the hot air ducts in the fuselage, pylons,
and wings.
For the pylon and APU, the sensing elements are tied to form a single loop and for the wing,
a double loop~
When the two wing loops detect a leak, or when one loop detects the leak and the other
one is inoperative, they activate a wing leak signal.
BMC1 and BMC2 each contain identical control logic for the system.
- A wing leak signal causes :
~ the bleed valve on the related side to close automatically
~ the associated FAULT light on the AIR COND panel to come on
~ the x-bleed valve to close automatically (except during an engine start)
~ the APU bleed valve to close automatically (if it is open, and if the leak concerns the
left wing) (except during engine start)
- A pylon leak signal causes :
~ the bleed valve on the related side to close automatically
~ the FAULT light for the related engine on the AIR COND panel to come on
~ the x-bleed valve to close automatically (except during an engine start).
- An APU leak signal causes :
~ the APU bleed valve to close automatically (except during engine start).
~ the FAULT light the APU BLEED pushbutton switch on the AIR COND panel to come on
~ the x-bleed valve to close automatically (except during an engine start).
CCM ALL
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃ .*,,.8, ,, ~e~ A319 ┃PNEUMATIC ┃1.36.10 P 9 ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━┻━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.36.10 P 10 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I ~-~ A318 ┃I PNEUDESCRIPTION ┃SEQ 001 1 ┃I REV 23 ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual5(16)
