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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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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(148)