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┃ .*,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃ NORMAL LAW ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━┻━━━━┛
Flight control normal law covers
- three-axis control
- flight envelope protection
- alleviation of maneuver loads
GROUND MODE
Ground mode is active when the aircraft is on the ground. It is a direct relationship between
sidestick deflection and elevator deflection, without auto trim.
It automatically sets the trimmable horizontal stabilizer (THS) at 0~ (inside the green band).
A setting that the pilot enters manually to adjust for CG has priority for takeoff.
When the aircraft reaches 70 knots during the takeoff roll, the system reduces the
maximum up elevator deflection from 30~ to 20~, and the aircraft performs the rotation
maneuver in direct law.
As soon as the aircraft becomes airborne, the system blends in the flight mode.
The reverse process occurs after touchdown.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃ ┃ ┃1.27.20 P 2 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃I -~ A318 ┃I FLIGHNORMALRLAW ┃SEQ 100 1 ┃I REV 23 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
FLIGHT MODE
The normal-law flight mode is a load-factor-demand mode with automatic trim and
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(83)
