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┃I -~ A318 ┃I CONTROLSCANDCINDICATORS ┃SEQ 100 1 ┃ REV 25 ┃
┃ .,,,.8, ,, ~% A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
EMER ELEC PWR
EMER GEN TEST RAT RAN ON
GEN 1 LINE
(~ MAN ON pb (guarded)
~
AUTO
When the following conditions are met :
~ AC BUS 1 is not electrically supplied.
~ AC BUS 2 is not electrically supplied.
~ Aircraft speed is greater than 100 knots
- The RAT extends.
A
U
-- The blue hydraulic system drives the emergency generator.
-As soon as the emergency generator electrical parameters are within
tolerance the emergency generator is connected to the aircraft network.
Pressed : This selects manual RAT extension.
FAULT It
Emergency generator coupling occurs 3 seconds after the RAT is supplying
the emergency generator.
This light comes on red if the emergency generator is not supplying power when AC
BUS 1 and AC BUS 2 are not powered.
EMER GEN TEST pb (guarded)
Pressed and held :
~ If AC NORMAL BUSES are supplied :
- The EMER GEN is driven hydraulically if the blue electric pump is running.
The AC ESS BUS and the DC ESS BUS are connected to the emergency generator,
(The DC ESS SHED and AC ESS SHED buses are not powered.)
- ECAM displays the ELEC page automatically (only on the ground).
~ If only the batteries supply the aircraft :
- The static inverter powers the AC ESS BUS.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃ ELECTRICAL ┃1.24.20 P 7 ┃
┃ .*,,.8, ,, ~% A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(18)
