曝光台 注意防骗
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milliseconds,
The FAULT light goes out when the pilot selects OFF, or at the end of the ELAC
power-up test if its results are satisfactory.
(~ SEC 1(2)(3) pb sw
Controls the spoiler and elevator (SEC) computers 1(2)(3).
ON SEC 1(2)(3) performs the following functions :
- normal roll (by controlling the spoilers)
- speed brakes and ground spoilers (SEC 1 and SEC 3 only)
- alternate pitch (SEC 1 and SEC 2 only)
- direct pitch (SEC 1 and SEC 2 only)
- direct roll
- abnormal attitude.
OFF The corresponding computer is not active. Switching it OFF and then on resets
the computer.
FAULT Lights up in amber, along with a "CAUTION" advisory on the ECAM, when a
failure is detected.
The FAULT light goes out when the pilot selects OFE
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━┓
┃J -~ A318 ┃ FLIGHT CONTROLS ┃1.27.40 P 7 ┃
┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃CONTROLS AND INDICATORS ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━┻━━━━┛
(~ FAC 1(2) pb sw
Controls the flight augmentation computer (FAC) 1(2).
ON Both FACs perform the following functions :
- Normal roll (coordinating turns and damping dutch roll)
- Budder trim
- Budder travel limit
OFF
FAU LT
- Alternate yaw
The corresponding computer is not active. Switching it OFF and then ON resets
the computer.
Lights up in amber, along with a caution on ECAM, when a failure is detected.
The FAULT light goes out when the pilot selects OFE
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.27.40 P 8 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(98)
