曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

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┃                                ┃                            ┃1.36.10     P 10      ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  ~-~ A318                     ┃I          PNEUDESCRIPTION  ┃SEQ 001 1 ┃I REV 23  ┃
┃ aw aw ,, ~L,~ .4319            ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
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BMC FAILURE
If one BMC fails, the adjacent BMC takes over the monitoring of the bleed system to issue
the following ECAM warnings if necessary :
- overpressure
- overtemperature
- wing leak.
Nevertheless, the associated FAULT light on the AIR COND panel is lost, and the associated
bleed valve does not close automatically.
ENG BLEED LEAK warning is lost for the associated engine, as is also the APU BLEED LEAK
warning if BMC1 has failed.
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┃I  -~ A318                      ┃        PNEUMATIC       ┃1.36.20     P 1   ┃
┃  .-,,.8, ,, ~L,~ A319          ┃                        ┃                  ┃
┃ Lli,~ A320                     ┃                        ┃                  ┃
┃                                ┃                        ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃CONTROLS AND INDICATORS ┃SEQ 001 ┃REV 23  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                        ┃        ┃        ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(98)