曝光臺 注意防騙
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┃ .-,,.8, ,, ~e~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃RECONFIGURATION CONTROL LAWS ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━━┻━━━━┻━━━━┛
The system applies an abnormal-attitude law in pitch and roll if the aircraft exceeds any of
these limits in flight.
- Pitch attitude > 50~ nose up or 30~ nose down
- Bank angle > 125~
- Angle of attack > 30~ or < - 10~ (- 15~ for A319 and A321)
- Speed > 440 knots or < 60 knots
- Mach > 0.91 or < 0.1
The law in pitch is the alternate law with no protection except load-factor protection and
without auto trim. In roll it is a full-authority direct law with a yaw mechanical.
When the aircraft has recovered from its abnormal attitude, the flight control laws in effect
are :
- in pitch : alternate law without protection with autotrim.
- in roll : full authority direct law with yaw alternate law.
There is no reversion to the direct law when the pilot extends the landing gear.
PITCH
Mechanical back-up permits the pilot to control the aircraft during a temporary complete
loss of electrical power.
He does this in pitch by applying trim manually to the THS.
The PFDs display "MAN PITCH TRIM ONLY" in red.
LATERAL
The pilot uses the rudder pedals as the mechanical back-up to control the aircraft laterally
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━┳━━━━━━━━━┓
┃I -~ A318 ┃ FLIGHT CONTROLS ┃1.27.40 P 1 ┃
┃ .-,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃CONTROLS AND INDICATORS ┃SEQ 001 ┃REV 35 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━┻━━━━┻━━━━┛
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本文鏈接地址：
AIRBUS A320 Flight Crew Operating Manual3(93)
