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┃ENG 1(2) REVERSER FAULT ┃ ┃ ┃ ┃ ┃ ┃
┃loss of thrust reverser on one engine due to system ┃ ┃ ┃ ┃ ┃3,4,5 ┃
┃components or input faults ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━╋━━━━╋━━━━┫ ┃ ┣━━━━┫
┃ENG 1(2) REV ISOL FAULT ┃SC ┃CAUT ┃NIL ┃NIL ┃3to 7 ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━╋━━━━╋━━━━┫ ┃ ┣━━━━┫
┃ENG 1(2) REV SWITCH FAULT ┃ ┃ ┃ ┃ ┃3,4,5, ┃
┃failure of reverser permission switch ┃ ┃ ┃ ┃ ┃6,7,8 ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━┫
┃ENG 1(2) FUEL RETURN VALVE ┃ ┃ ┃ ┃ ┃ ┃
┃Failure of the fuel return valve in open or closed ┃NIL ┃NIL ┃ ┃ ┃3,4,5, ┃
┃ ┃ ┃ ┃ ┃ ┃ 7,8 ┃
┃position ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━┫
┃ ┃ ┃ ┃ ┃ ┃3,4,5, ┃
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AIRBUS A320 Flight Crew Operating Manual5(195)
