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┃ ┣━━━━━━╋━━━━╋━━━━╋━━━━╋━━━━━╋━━━┫
┃ ┃LP VALVE ┃ ┃DC BAT ┃ ┃ ┃HOTI ┃
┣━━━━━━━┻━━━━━━╋━━━━╋━━━━╋━━━━╋━━━━━╋━━━┫
┃REFUEL VALVES ┃ ┃DC2 ┃ ┃ ┃(1) ┃
┗━━━━━━━━━━━━━━┻━━━━┻━━━━┻━━━━┻━━━━━┻━━━┛
(1)
(2)
(3)
HOT BUS supplies power during refueling on battery
This occurs if DC BUS 1 is lost.
In smoke configuration (GEN 1 LINE pushbutton OFF), inner tank pumps 1 are
supplied directly by IDG (instead of AC 1) and pump relays by DC ESS (instead of
DC 1).
┏━━━━━━━━━━━━━━━━┳━━━━━┳━━━━━━━━━┓
┃ ~-Z A318 ┃HYDRAULIC ┃1.29.00 P 1 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃CONTENTS ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━┻━━━━┻━━━━┛
29.00 CONTENTS
29.10 DESCRIPTION
-GENERAL.. .
- GENERATION.
- DISTRIBUTION
29.20 CONTROLS AND INDICATORS
- OVERHEAD PANEL
- MAINTENANCE PANEL
-ECAM HYD PAGE
- WARNINGS AND CAUTIONS
- MEMO DISPLAY
29.30 ELECTRICAL SUPPLY
1
1
6
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃HYDRAULIC ┃1.29.10 P 1 ┃
┃ -,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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航空翻译 www.aviation.cn
本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(148)
