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┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
RESERVOIR PRESSURIZATION
Normally, HP bleed air from engine 1 pressurizes the hydraulic reservoirs automatically.
If the bleed air pressure is too low, the system takes bleed air pressure from the crossbleed
duct.
The systems maintain a high enough pressure to prevent their pumps from
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━┳━━━━━━━━━━━┓
┃I  -~ A318                      ┃HYDRAULIC   ┃1.29.10     P 5       ┃
┃  .*,,.8, ,, ~L,~ A319          ┃            ┃                      ┃
┃                                ┃            ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃            ┃SEQ 100 I ┃I REV 33  ┃
┃      A~7-~'M" A321             ┃DESCRIPTION ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━┻━━━━━┻━━━━━┛
INDICATIONS
LO LVL
             I-
=-          4-
\
\
     I
\1
 L
L
  /I          OVHT
Jl
   /
J
ENG I PUMP
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.29.10     P 6       ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃I           HYDDESCRIPTION  ┃SEQ 100 1 ┃I REV 23  ┃
┃ amain ,, ~L,~ A319             ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(151)