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┃L (R) WING LEAK                                     ┃        ┃        ┃        ┃  ENG     ┃          ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━┫        ┃        ┃        ┃          ┣━━━━━┫
┃temperature > 124~C detected by the loops           ┃        ┃        ┃        ┃ BLEED    ┃          ┃
┃ENG 1 (2) BLEED LEAK                                ┃        ┃        ┃        ┃FAULT It  ┃          ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━┫        ┃        ┃        ┃          ┃          ┃
┃temperature > 204~C detected by the loop and        ┃        ┃        ┃        ┃          ┃3,4,5,    ┃
┃engine 1 (2) running                                ┃        ┃        ┃        ┃          ┃ 7,8      ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━┫        ┃        ┃        ┃          ┃          ┃
┃ENG 1 (2) BLEED NOT CLSD                            ┃SINGLE  ┃MASTER  ┃        ┃          ┃          ┃
┃bleed valve not automatically closed during engine  ┃        ┃        ┃BLEED   ┃          ┃          ┃
┃start or with APU bleed selected                    ┃CHIME   ┃ CAUT   ┃        ┃          ┃          ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━┫        ┃        ┃        ┣━━━━━╋━━━━━┫
┃BLEED 1 (2) OFF                                     ┃        ┃        ┃        ┃ ENG      ┃1,3,4,5,  ┃
┃                                                    ┃        ┃        ┃        ┃BLEED     ┃7,8,9,    ┃
┃one engine bleed switched off with no fault         ┃        ┃        ┃        ┃OFF It    ┃   10     ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual5(22)