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┃ Lli,~ A320                     ┃              ┃SEQ 005 I ┃I REV 23  ┃
┃      A~7-~'M" A321             ┃ FUEL SYSTEM  ┃          ┃          ┃
┃  FLIGHT CREW OPERATING MANUAL  ┃              ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━┻━━━━━┻━━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃J  -~ A318                      ┃POWER PLANT ┃1.70.50     P 1       ┃
┃  .-,,.8, ,, ~L,~ A319          ┃            ┃                      ┃
┃                                ┃            ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃            ┃SEQ 005 J ┃J REV 23  ┃
┃      A~7-~'M" A321             ┃ OIL SYSTEM ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
The oil system lubricates the engine components.
It contains :
- the oil tank
- the lube and scavenge pump modules
- the fueVoil heat exchanger
- the filters, chip detectors, pressure relief and bypass valves
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃J  -~ A318                      ┃ POWER PLANT    ┃1.70.60     P 1       ┃
┃  .*,,.8, ,, ~L,~ A319          ┃                ┃                      ┃
┃                                ┃                ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃                ┃SEQ 005 J ┃J REV 23  ┃
┃      A~7-~'M" A321             ┃AIRBLEED SYSTEM ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━━┻━━━━━┛
The air bleed system supplies the aircraft with compressed air
It uses the air for :
- pneumatic system (refer to 1.36)
- cooling the engine compartment and the turbines.
REFER
  TO
 1.~
ROTOR ACTIVE CLEARANCE CONTROL (RACC) SYSTEM
The FADEC controls the RACC system through the HMU. The RACC system controls the
clearance between the rotor blades of the HP compressor and its stator case.
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(165)