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associated ground spoilers are available only through reverse selection.
L12
STATUS
LDG DIST PROC................................................................APPLY
If reversers are not used, Refer to 99 Duref Cible QRH, or to the
Refer to 99 Duref Cible FCOM.
INOP SYS
SPD BRK
F/CTL SPD BRK FAULT
Applicable to: ,
MSN,,,,
L2 Loss of speedbrake surfaces, due to failure of the speedbrake lever transducer(s). In addition,
associated ground spoilers are available only through reverse selection.
L12
STATUS
LDG DIST PROC................................................................APPLY
If reversers are not used, Refer to 99 Duref Cible QRH, or to the
Refer to 99 Duref Cible FCOM.
INOP SYS
SPD BRK
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 122/146
FCOM 19 AUG 10
F/CTL SPD BRK 2(3+4) FAULT
Applicable to:
L2 Loss of speedbrake surfaces, due to failure of speedbrake lever transducer(s). In addition
associated ground spoilers are available only through reverse selection.
L1 If SPD BRK 3+4 affected:
SPD BRK................................................................................................................ DO NOT USE
L2 Do not use speedbrakes since it is not efficient to use only surfaces n° 2, and would active the
SPD BRK DISAGREE caution.
L12
STATUS
• If SPD BRK 3+4 affected:
SPD BRK................................................ DO NOT USE
LDG DIST PROC................................................................APPLY
If reversers are not used, Refer to 99 Duref Cible QRH, or to the
Refer to 99 Duref Cible FCOM.
INOP SYS
SPD BRK (affected)
F/CTL SPD BRK 2(3+4) FAULT
Applicable to: ,
L2 Loss of speedbrake surfaces, due to failure of speedbrake lever transducer(s). In addition
associated ground spoilers are available only through reverse selection.
L1 If SPD BRK 3+4 affected:
SPD BRK................................................................................................................ DO NOT USE
L2 Do not use speedbrakes since it is not efficient to use only surfaces n° 2, and would active the
SPD BRK DISAGREE caution.
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 123/146
FCOM 19 AUG 10
F/CTL SPD BRK 2(3+4) FAULT (Cont'd)
L12
STATUS
• If SPD BRK 3+4 affected:
SPD BRK................................................ DO NOT USE
LDG DIST PROC................................................................APPLY
If reversers are not used, Refer to 99 Duref Cible QRH, or to the
Refer to 99 Duref Cible FCOM.
INOP SYS
SPD BRK (affected)
F/CTL SPD BRK 2(3+4) FAULT
Applicable to: ,
MSN,,,,
L2 Loss of speedbrake surfaces, due to failure of speedbrake lever transducer(s). In addition
associated ground spoilers are available only through reverse selection.
L1 If SPD BRK 3+4 affected:
SPD BRK................................................................................................................ DO NOT USE
L2 Do not use speedbrakes since it is not efficient to use only surfaces n° 2, and would active the
SPD BRK DISAGREE caution.
L12
STATUS
• If SPD BRK 3+4 affected:
SPD BRK................................................ DO NOT USE
LDG DIST PROC................................................................APPLY
If reversers are not used, Refer to 99 Duref Cible QRH, or to the
Refer to 99 Duref Cible FCOM.
INOP SYS
SPD BRK (affected)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 124/146
FCOM 19 AUG 10
F/CTL LAF ACCU FAULT
Applicable to:
L2 Failure of one LAF accumulator.
LAF DEGRADED is displayed on the F/CTL page. Degraded LAF function is available with a
reduced aileron deflection rate and without associated spoilers.
Crew awareness.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 125/146
FCOM 19 AUG 10
F/CTL SIDESTICK PRIORITY
Applicable to: ALL
L2 A failure is detected in the sidestick priority logic circuit.
L1CHECK PRIORITY LOGIC
L2Check the integrity of flight control priority, as follows (not displayed on ECAM) :
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 9(107)
