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NORM
– – – – –
DIRECT (4)
NORM
– – – – –
MECH (4)
SPOILER 4 or
5 or (4 and 5) NORM NORM NORM NORM
All SPOILERS ALTN REDUCED DIRECT ALTN
1 AIL SERVO
or 1 AILERON NORM NORM NORM NORM
1 ELEV SERVO NORM NORM NORM NORM
1 ELEVATOR ALTN REDUCED DIRECT ALTN
THS (jammed) (5)NORM NORM NORM NORM ALTN REDUCED DIRECT ALTN
HYD G or Y or B NORM NORM NORM NORM
HYD G + Y ALTN REDUCED DIRECT MECH
HYD G + B ALTN NO DIRECT ALTN
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 143/146
FCOM 19 AUG 10
ACTIVE CONTROL LAW (Cont'd)
ACTIVE LAW ▸ PITCH
SYS FAILED▸ LAW PROTEC ROLL YAW
HYD Y + B NORM NORM NORM NORM
on BATTERIES ALTN REDUCED DIRECT MECH
on EMER GEN ALTN REDUCED DIRECT
MECH
– – – – –
ALTN (3)
(1) In case of AOA disagree
(2) After the faulty IR is selected OFF
(3) After FAC 1 is reset
(4)When landing gear down (or CONF 2, if both LGCIUs faulty)
(5) Depending where the failure is, control law may revert to alternate law
ELEVATORS AND STABILIZER CONTROL AFTER FAILURE
Applicable to: ALL
LEFT ELEVATOR THS RIGHT ELEVATOR
BLUE GREEN GREEN AND YELLOW YELLOW BLUE
NORM OPERATION ELAC 2 ELAC 2 ELAC 2
SINGLE FAILURE
ELAC 2 ELAC 1 ELAC 1 ELAC 1
ELAC 1 ELAC 2 ELAC 2 ELAC 2
SEC 2 ELAC 2 ELAC 2 ELAC 2
SEC 1 ELAC 2 ELAC 2 ELAC 2
G ELAC 1 ELAC 1 ELAC 1
Y ELAC 1 ELAC 1 ELAC 1
B ELAC 2 ELAC 2 ELAC 2
DOUBLE FAILURE
ELAC
2
+ ELAC 1 SEC 2 SEC 2 SEC 2
+ SEC 2 ELAC 1 ELAC 1 ELAC 1
+ SEC 1 ELAC 1 ELAC 1 ELAC 1
+ G ELAC 1 ELAC 1 ELAC 1
+ Y ELAC 1 ELAC 1 ELAC 1
+ B SEC 2 SEC 2 SEC 2
ELAC
1
+ SEC 2 ELAC 2 ELAC 2 ELAC 2
+ SEC 1 ELAC 2 ELAC 2 ELAC 2
+ G SEC 1 SEC 2 SEC 2
+ Y SEC 2 SEC 2 SEC 1
+ B ELAC 2 ELAC 2 ELAC 2
SEC 2 + SEC 1 ELAC 2 ELAC 2 ELAC 2
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 144/146
FCOM 19 AUG 10
Continued from previous page
+ G ELAC 1 ELAC 1 ELAC 1
+ Y ELAC 1 ELAC 1 ELAC 1
+ B ELAC 2 ELAC 2 ELAC 2
SEC 1 + G ELAC 1 ELAC 1 ELAC 1
+ Y ELAC 1 ELAC 1 ELAC 1
+ B ELAC 2 ELAC 2 ELAC 2
G + Y ELAC 1 INOP ELAC 1
B + G Damped ELAC 2 ELAC 2
B + Y ELAC 2 ELAC 2 Damped
TRIPLE FAILURE
ELAC 2
ELAC
1
+ SEC 2 SEC 1 SEC 1 SEC 1
+ SEC 1 SEC 2 SEC 2 SEC 2
+ G SEC 1 SEC 2 SEC 2
+ Y SEC 2 SEC 2 SEC 1
+ B SEC 2 SEC 2 SEC 2
SEC 2 + SEC 1 ELAC 1 ELAC 1 ELAC 1
+ G ELAC 1 ELAC 1 ELAC 1
+ Y ELAC 1 ELAC 1 ELAC 1
+ B Centered Mechanical Centered
SEC 1 + G ELAC 1 ELAC 1 ELAC 1
+ Y ELAC 1 ELAC 1 ELAC 1
+ B SEC 2 SEC 2 SEC 2
G + Y ELAC 1 INOP ELAC 1
B + G Damped SEC 2 SEC 2
B + Y SEC 2 SEC 2 Damped
ELAC 1
SEC 2 + SEC 1 ELAC 2 ELAC 2 ELAC 2
+ G SEC 1 SEC 1 SEC 1
+ Y SEC 1 SEC 1 SEC 1
+ B ELAC 2 ELAC 2 ELAC 2
SEC 1 + G Damped SEC 2 SEC 2
+ Y SEC 2 SEC 2 Damped
+ B ELAC 2 ELAC 2 ELAC 2
G + Y SEC 1 INOP SEC 1
B + G Damped ELAC 2 ELAC 2
B + Y ELAC 2 ELAC 2 Damped
SEC 2
SEC 1 + G ELAC 1 ELAC 1 ELAC 1
+ Y ELAC 1 ELAC 1 ELAC 1
+ B ELAC 2 ELAC 2 ELAC 2
G + Y ELAC 1 INOP ELAC 1
B + G Damped ELAC 2 ELAC 2
B + Y ELAC 2 ELAC 2 Damped
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 145/146
FCOM 19 AUG 10
Continued from previous page
SEC 1
G + Y ELAC 1 INOP ELAC 1
B + G Damped ELAC 2 ELAC 2
B + Y ELAC 2 ELAC 2 Damped
SIDESTICK/RUDDER PEDALS STIFF
Applicable to: ALL
L2 Even if the autopilot is disengaged, the sidestick and/or the rudder pedals may be stiff. This may
affect either:
Both sidesticks (CAPT and F/O) at the same time, but ‐ not the rudder pedals, or
‐ One sidestick and the rudder pedals at the same time.
The piloting technique remains the same: The aircraft remains responsive.
However, the flight crew should keep in mind that they may need to use extra force on the
sidesticks and/or the rudder pedals.
The extra force required to move the controls out of the neutral position is moderate.
This extra force does not significantly affect the handling of the aircraft.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 9(113)
