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┃ENG 1(2) N1 or N2 or EGT OVER LIMIT ┃ ┃ ┃ ┃ ┃ ┃
┃N1 above 104 % ┃SINGLE ┃MASTER ┃ ┃ ┃ ┃
┃N2 above 105.0 % ┃CHIME ┃ CAUT ┃NIL ┃ ┃ ┃
┃ ┃ ┃ ┃ ┃ ┃4,8 ┃
┃EGT above 950~C ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
┃ENG 1(2) IGN A + B FAULT ┃ ┃ ┃ ┃ ┃3,4,5, ┃
┃Both ignition circuits are failed. ┃ ┃ ┃ ┃ ┃ 7,8 ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
┃ENG 1(2) CTL VALVE FAULT ┃ ┃ ┃ ┃ ┃ ┃
┃Burn stag valve failure or HPTC, or RAC system failure. ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┃ ┃
┃ENG 1(2) FUEL CTL FAULT ┃ ┃ ┃ ┃ ┃ ┃
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AIRBUS A320 Flight Crew Operating Manual5(190)
