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┃I ~-~ A318 ┃ AUTO FLIGHT ┃1.22.30 P 61 ┃
┃ aw aw ,, ~e~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃FLIGHT GUIDANCE ┃SEQ 001 ┃REV 28 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━┻━━━━┛
A/THR ACTIVATION
The A/-rHR is active when it controls thrust or speed. The position of the thrust lever
determines the maximum thrust that the A/-I-HR system can command (except in m-floor
condition).
The A/-I-HR being armed, is
8
when the pilot sets both
operative)
activated ~
thrust levers between the CL and IDLE detents (two engines
when the pilot sets one thrust lever between the MCT and IDLE detents (one engine
inoperative).
The A/-rHR being disconnected, is activated when the pilot pushes the FCU pushbutton
while the thrust levers are within the active range, including IDLE position.
Note : When the pilot sets both thrust levers to IDLE position, the A/THR disconnects but,
if the pilot pushes the A/THR pushbutton of the FCU, he will simultaneously arm and
activate the autothrust. Due to the thrust levers position, IDLE thrust will be
maintained.
- when ALPHA FLOOR is activated, regardless of the initial status of A/-I-HR and the
position of the thrust levers.
When A/1-HR is active ~
The A/-rHfi pushbutton on the FCU lights
The FMA displays A/-I-HR mode in green
fifth column.
I
A/THR mode
, green
?
Z
up.
n the first column and A/-FHR in white in the
A/THR active status
white
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.22.30 P 62 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃l AFLIGHTIGUIDANCE ┃SEQ 200 1 ┃I REV 31 ┃
┃ .,,,.8, ,, ~% A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(70)
