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┃I -~ A318 ┃l AFLIGHTIGUIDANCE ┃SEQ 303 1 ┃I REV 34 ┃
┃ .,,,.8, ,, ~e~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
AP engagement is indicated by the lighting of the corresponding FCU pushbutton and by
the appearance of "API" (or 2) on the PFD's Flight Mode Annunciator.
AP DISENGAGEMENT
AP1 or 2 disengages when :
- The pilot presses the takeover pushbutton on the sidestick.
- The pilot presses the corresponding AP pushbutton on the FCU.
- The pilot pushes on the sidestick harder than a certain threshold or moves on the rudder
pedals above a threshold.
- The pilot moves the pitch trim wheel beyond a certain threshold.
- The other AP is engaged, except when Iocalizer/glideslope modes are armed or engaged,
or when the rollout or go-around mode is engaged.
- Both thrust levers are set above the MCT detent and the aircraft is on the ground.
- The aircraft reaches the MDA- 50 feet (MDH-50 feet), or 400 feet AGL if no MDA/MDH,
with APPR mode engaged and a non-lLS approach selected.
- One of the engagement conditions is lost.
Furthermore, in normal law with all protections available, the AP will disconnect if :
~ High speed protection is active ;
~ Angle-of-attack protection is active (~ prot + 1~ is reached) ;
~ Pitch attitude exceeds 25~ up, or 13~ down, or bank angle exceeds 45~ ;
~ A rudder pedal deflection is more than 10~ out of trim.
The standard way for the flight crew to disengage the AP is to press the takeover
pushbutton on the sidestick.
When the AP is OFF, the associated FCU pushbutton goes off, and "API" (or AP2)
disappears from the PFD's FMA.
CCM ALL
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┃I ~-~ A318 ┃ AUTO FLIGHT ┃1.22.30 P 9 ┃
┃ aw aw ,, ~e~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃FLIGHT GUIDANCE ┃SEQ 001 ┃REV 23 ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(24)
