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┃pushed in phases 1, 2, 9 and 10. ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
┃ENG 1(2) REVERSE UNLOCKED ┃ ┃ ┃ ┃ ┃ ┃
┃One or more reverser doors not locked in stowed ┃ ┃ ┃ ┃ ┃8 ┃
┃position in flight, or on ground with no deploy order. ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
┃ENG 1(2) BEY PRESSURIZED ┃ ┃ ┃ ┃ ┃ ┃
┃Reverser system is pressurized, while rev doors are ┃ ┃ ┃ ┃ ┃4,5,8 ┃
┃stowed and locked with no deploy order. ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
┃ENG 1(2) COMPRESSOR VANE ┃ ┃ ┃ ┃ ┃ ┃
┃Variable bleed valve sys or variable stator vane sys ┃ ┃ ┃ ┃ ┃4,5,7,8 ┃
┃fault. ┃ ┃ ┃ ┃ ┃ ┃
┣━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫ ┃ ┃ ┃ ┣━━━━━┫
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AIRBUS A320 Flight Crew Operating Manual5(189)
