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70.90      CONTROLS AND INDICATORS
          - PEDESTAL
          - OVERHEAD PANEL
          - MAINTENANCE PANEL
          - ECAM
          - WARNINGS AND CAUTIONS
          - MEMO DISPLAY
70.98   ELECTRICAL SUPPLY
.1
.4
.4
.5
13
15
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃J  -~ A318                      ┃POWER PLANT ┃1.70.10     P 1       ┃
┃  .-,,.8, ,, ~e~ A319           ┃            ┃                      ┃
┃                                ┃            ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃            ┃SEQ 120 I ┃J REV 28  ┃
┃      A~7-~'M" A321             ┃    ENGINE  ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
R   The CFM 56-5B engine is a high bypass ratio turbofan
Low-pressure (LP) compressor/turbine
The low-speed rotor (N1) consists of a front fan (single-stage) and a four-stage LP
compressor connected to a four-stage LP turbine.
High-pressure (HP) compressor/turbine
The high-speed rotor (N2) consists of a nine-stage HP compressor connected to a
single-stage HP turbine.
Combustion chamber
The annular combustion chamber is fitted with 40 fuel nozzles and 2 igniters
Accessory gearbox
The accessory gearbox, located at the bottom of the fan case, receives torque from
horizontal HP rotor drive shaft and drives gearbox mounted accessories.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃J  -~ A318                      ┃POWER PLANT ┃1.70.20     P 1       ┃
┃  .*,,.8, ,, ~L,~ A319          ┃            ┃                      ┃
┃                                ┃            ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃            ┃SEQ 005 J ┃J REV 23  ┃
┃      A~7-~'M" A321             ┃     FADEC  ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
Each powerplant has a FADEC (Full Authority Digital Engine Control) system.
FADEC, also called the Electronic Control Unit (ECU), is a digital control system that
performs complete engine management.
FADEC has two-channel redundancy, with one channel active and one in standby.
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(152)