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┃                                ┃                              ┃1.30.30     P 2       ┃
┃                                ┃                              ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃l    ICE AND ENGINERANTITICE  ┃SEQ 100 1 ┃I REV 26  ┃
┃ aw aw ,, ~% A319               ┃                              ┃          ┃          ┃
┃ Lli,~ A320                     ┃                              ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                              ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                              ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
OVERHEAD PANEL
┏━━━━━━━┳━━━┳━━━━━━━━━━━┳━━━━━━━┓
┃              ┃ANTI  ┃ICE                   ┃              ┃
┃              ┃      ┃                      ┃PROBE/WINDOk  ┃
┃              ┃      ┃                      ┃     HEAT     ┃
┃         WING ┃      ┃   ENG 1       ENG 2  ┃              ┃
┃              ┃      ┃     A      A         ┃              ┃
┗━━━━━━━┻━━━┻━━━━━━━━━━━┻━━━━━━━┛
O ENG 1 (2) pb sw
ON
Off
FAU LT
light comes on blue.
ECAM MEMO displays "ENG A. ICE".
Engine anti-ice valve opens if bleed air is available from the engine.
Continuous ignition is selected when the valve is opened and the ANTI
ICE ENG pushbutton switch is selected ON.
ON light goes out.
Engine anti-ice valve closes.
Amber light comes on, and caution message appears on ECAM, if the
position of the anti-icing valve disagrees with the ENG 1 (2) pushbutton
selection.
Note : The amber FAULT light comes on briefly as valve transits
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━━━┓
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(170)