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OVHT IS DISPLAYED IN AMBER
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                                ┃1.31.25     P 4       ┃
┃                                ┃                                ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃I INDICATING/ECAMRSEQUENCETEMS  ┃SEQ 001 1 ┃I REV 24  ┃
┃ ~ ~ ,, ~L,~ A319               ┃                                ┃          ┃          ┃
┃ L~I,~ A320                     ┃                                ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                                ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                                ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
3 - THE FLIGHT CREW FOLLOWS THE INSTRUCTION DISPLAYED ON THE E/WD
The crew switches off the blue ELEC pump, depressurizing the blue hydraulic circuit
COCKPIT INDICATIONS
A single chime sounds.
Both MASTER CAUTION lights stay on.
A FAULT/OFF light on the overhead panel comes on.
The second part of the message on the E/WD changes to "B SYS LO PR".
The system diagram on the SD shows an amber zero for the pressure in the blue system,
along with the amber "OVHT".
The right side of the memo area indicates a secondary failure in the flight control
system.
The CLR pushbutton on the ECAM control panel stays lighted.
- LEFT PART
  ~ INDEPENDENT FAILURE AND
      PRIMARY FAILURE
- RIGHT PART
  .SECONDARY FAILURE
- THE SYNOPTIC OF THE
SYSTEM PAGE IS CHANGED
ACCORDING TO THE NEW SYSTEM
CONFIGURATION
OVHT  AND  THE  PRESSURE
ARE DISPLAYED IN AMBER
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃I  -~ A318                      ┃INDICATING/RECORDING SYSTEMS  ┃1.31.25     P 5       ┃
┃  .-,,.8, ,, ~L,~ A319          ┃                              ┃                      ┃
┃                                ┃                              ┣━━━━━┳━━━━━┫
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual4(38)