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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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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(16)