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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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AIRBUS A320 Flight Crew Operating Manual5(22)
