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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)
