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not follow the FD bars to maintain the commanded descent, the aircraft decelerates (pitch
too high and autothrust in IDLE).
Both FDs disengage when VLS-2 (or VLS-17 if speedbrakes extended) is reached.
The A/-rHB if active, reverts to SPEED mode, and increases the thrust to recover the speed
target.
REACHING
 VLS-2
   OR
(VLS-17)
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━━━┓
┃I  -~ A318                      ┃  AUTO FLIGHT   ┃1.22.30     P 43      ┃
┃  .-,,.8, ,, ~% A319            ┃                ┃                      ┃
┃                                ┃                ┣━━━━━┳━━━━━┫
┃ Lli,~ A320                     ┃                ┃SEQ 200 I ┃I REV 28  ┃
┃      A~7-~'M" A321             ┃FLIGHT GUIDANCE ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━━┻━━━━━┛
AUTOMATIC SPEED PROTECTION IN VERTICAL SPEED MODE
During climb
If the selected target V/S or FPA is too high (relative to the thrust condition and speed), the
FMGS maintains the target V/S or FPA but the aircraft decelerates and the indicated
airspeed decreases. When reaching VLS (or VLS-5 if the speed target is VLS), the selected
V/S or FPA target is temporarily abandonned to maintain VLS but V/S mode remains
engaged.
The FMGS automatically decreases the vertical speed to maintain VLS
The target V/S does not change but is no longer followed.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.22.30     P 44      ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
┃I  -~ A318                      ┃l          AFLIGHTIGUIDANCE ┃SEQ 200 1 ┃I REV 28  ┃
┃  .,,,.8, ,, ~e~ A319           ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual2(55)