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┃                                          ┃  AP/FD were previously off.                      ┃
┣━━━━━━━━━━━━━━━━━━━━━╋━━━━━━━━━━━━━━━━━━━━━━━━━┫
┃Roll FD bar (or FPV) flashes permanently  ┃Transmission of the LOC data is interrupted when  ┃
┃                                          ┃in LOC, LOC* or LAND modes above 15 ft RA.        ┃
┗━━━━━━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━━━━━━━━━━━┛
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━┓
┃I  ~-~ A318                     ┃  AUTO FLIGHT   ┃1.22.30     P 7   ┃
┃ aw aw ,, ~e~ A319              ┃                ┃                  ┃
┃ Lli,~ A320                     ┃                ┃                  ┃
┃                                ┃                ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃FLIGHT GUIDANCE ┃SEQ 001 ┃REV 25  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━┻━━━━┛
GENERAL
The AP
- stabilizes the aircraft around its center of gravity
- acquires and tracks a flight path
- flies the aircraft to an automatic landing or go-around
The AP commands the :
position of the flight control surfaces for pitch, roll, and yaw
nose wheel position.
AP ENGAGEMENT
R   The flight crew can engage AP1 or AP2 by pressing the corresponding pushbutton on the
R   FCU if the aircraft has been airborne for at least five seconds.
R   When one AP is engaged, the corresponding FCU pushbutton comes on and AP1 (or 2) is
R   displayed on the FMAs.
Note
One AP can be engaged on the ground if the engines are not running. It
disengages when one engine is started.
Two APs may be engaged at a time (API active, AP2 in standby), when the
Iocalizer/glide-slope or roll out or go-around mode is armed or engaged.
Only one AP can be engaged at a time in all other cases.
If one AP pushbutton is set to on with both FOs off, the AP engages in HOG V/S
or TRK FPA mode, depending upon which the pilot has selected on the FCU.
If one AP pushbutton is set to on with at/east one FO already on, the AP engages
in the current active FO modes.
AP engagement increases the break out force on the sidestick controllers and on
the rudder pedals.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.22.30     P 8       ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual2(23)