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┃A/THR in SPEED/MACH mode ┃If neither AP nor FD is engaged ┃
┃ ┣━━━━━━━━━━━━━━━━━━━━━━━┫
┃ ┃If AP/FD controls a vertical path ┃
┃ ┃V/S-FPA-ALT*- ALT CST*-ALT-ALT CRZ-G/S* ┃
┃ ┃-G/S-FINAL and DES (geometric path) ┃
┣━━━━━━━━━━━━━╋━━━━━━━━━━━━━━━━━━━━━━━┫
┃A/THR in RETARD mode ┃Automatic landing (AP engaged in LAND mode). ┃
┗━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━━━━━━━━┛
THRUST mode
In THRUST mode, autothrust commands a specific thrust level in conjunction with the
AP/FD pitch mode. This thrust level is limited by thrust lever position.
┏━━━━━━┳━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┓
┃FMA display ┃Meaning ┃
┣━━━━━━╋━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫
┃THR MCT ┃Single engine thrust in climb. The live engine is at maximum ┃
┃ ┃continuous thrust (thrust lever in MCT detent) ┃
┣━━━━━━╋━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫
┃THR CLB ┃Climb thrust two engine configuration (at least one thrust lever in ┃
┃ ┃the CL detent, the other one below CL) ┃
┣━━━━━━╋━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫
┃THR LVR ┃Undetermined thrust (neither CLB or MCT thrust) ┃
┣━━━━━━╋━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┫
┃THR IDLE ┃Minimum thrust (both engines at IDLE thrust) ┃
┗━━━━━━┻━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━━┛
Note : When the A/THR is armed for takeoff or go around, the FMA displays "MAN TOGA"
(or "MAN FLX") in white to remind the crew that the thrust levers have been
positioned properly.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I ~-~ A318 ┃ AUTO FLIGHT ┃1.22.30 P 65 ┃
┃ aw aw ,, ~e~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual2(75)
