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CONTROL SURFACES
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┃ ┃1 ┃i ┃ ┃kl ┃ ┃ ┃
┃ ┃ ┃ ┃ ┃ ┃HORIZONTAL ┃ ┃
┃ ┃ ┃ ┃ ┃ ┃STABILIZER ┃ ┃
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The flight controls are electrically or mechanically controlled as follows
Pitch axis
Elevator
Stabilizer
Roll axis
Ailerons
Spoilers
Yaw axis
Rudder
Electrical
Electrical for normal or alternate control. Mechanical for manual trim
control
Electrica
Electrica
Mechanical, however control for yaw damping, turn coordination and
trim is electrical.
Speed brakes
Speed brakes = Electrica
Note : All surfaces are hydraulically actuated
CCM ALL
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┃I -~ A318 ┃FLIGHT CONTROLS ┃1.27.10 P 3 ┃
┃ .-,,.8, ,, ~e~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
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┃ A~7-~'M" A321 ┃ DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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COCKPIT CONTROLS
Each pilot has a sidestick controller with which to exercise manual control of pitch and
roll. These are on their respective lateral consoles.
The two sidestick controllers are not coupled mechanically, and they send separate sets
of signals to the flight control computers.
Two pairs of pedals, which are rigidly interconnected, give the pilot mechanical control
of the rudder.
The pilots control speed brakes with a lever on the center pedestal.
The pilots use mechanically interconnected handwheels on each side of the center
pedestal to control the trimmable horizontal stabilizer.
The pilots use a single switch on the center pedestal to set the rudder trim.
There is no manual switch for trimming the ailerons.
COMPUTERS
Seven flight control computers process pilot and autopilot inputs according to normal,
alternate, or direct flight control laws.
The computers are :
2 ELACs
(Elevator Aileron Computer)
For : Normal elevator and stabilizer control
Aileron control.
3 SECs
(Spoilers Elevator Computer)
For : Spoilers control.
Standby elevator and stabilizer control
2 FACs
(Flight Augmentation Computer)
For : Electrical rudder control.
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(73)
