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automatic APU shutdown occurs, which happens in case of :
Fire (on ground only) Reverse flow
Air inlet flap not open Low oil pressure
Overspeed High oil temperature
No acceleration DC power loss. (BAT OFF when aircraft on
Slow start batteries only)
EGT overtemperature ECB failure
No flame loss of overspeed protection
Underspeed
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.49.20 P 2 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I CONTROLS AND INDICATORS ┃SEQ 100 1 ┃I REV 28 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
START pb sw
ON
AVAIL It
Blue ON light comes on.
- When the flap is completely open, the APU starter is energized.
- 1.5 seconds after the starter is energized, the ignition is turned ON.
- When N = 55 %. The APU starter is de-energized. The ignition is turned
off.
- 2 seconds after N reached 95 %, or when N is above 99.5 % :
The ON light on the START pushbutton goes out.
The APU may now supply bleed air and electrical power to the aircraft
systems.
- 10 seconds later, the APU page disappears from the ECAM display.
This green light comes on when N is above 99.5 % or 2 seconds after N
reaches 95 %.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃ APU ┃1.49.20 P 3 ┃
┃ .-,,.8, ,, ~L,~ A319 ┃ ┃ ┃
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual5(53)
