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�� If both slat channels fail:
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...................................................................................................................... 320 KT
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 36/146
FCOM 19 AUG 10
F/CTL SLATS AND FLAPS FAULT IN CONF 0 (Cont'd)
L12
STATUS
• If both slat channels fail:
MAX SPEED......................................................320 KT
ALTN LAW: PROT LOST
APPR PROC
FOR LDG...................................................................USE FLAP 1
With FLAPS lever set at 1, AP/FD GO AROUND mode is
available.
GPWS FLAP MODE................................................................OFF
APPR SPD...............................................................VREF +60 KT
Approach with A/THR in selected mode is recommended.
�� If both slat channels fail:
WHEN L/G DN: DIRECT LAW
�� AT 300 FT AGL:
TARGET SPD......................................................... VREF +50
Reduce speed between 500 ft and 300 ft to reach VREF
+50 kt at runway threshold and disconnect A/THR, as the
target speed may be below VLS.
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
• ____________Only in case of FLAPS FAULT:
ENG 1 APPR IDLE ONLY
ENG 2 APPR IDLE ONLY
INOP SYS
F/CTL PROT (1)
SLATS
FLAPS
AP 1+2 (2)
A/THR (2)
Moreover, both FDs are lost (2)
CAT 2 (2)
(1) (If both slat channels fail.)
(2) (If both slat or flap channels fail.)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 37/146
FCOM 19 AUG 10
F/CTL SLAT SYS 1(2) FAULT
Applicable to:
L2Crew awareness
STATUS
SLATS SLOW
F/CTL SLAT SYS 1(2) FAULT
Applicable to: ,
L2Crew awareness
STATUS
SLATS SLOW
F/CTL SLAT SYS 1(2) FAULT
Applicable to: ,
MSN,,,,
L2Crew awareness
STATUS
SLATS SLOW
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 38/146
FCOM 19 AUG 10
F/CTL FLAP SYS 1(2) FAULT
Applicable to:
�� If FLAP sys 1 fault:
GPWS FLAP MODE...............................................................................................................OFF
STATUS
ENG 1(2) APPR IDLE ONLY
FLAPS SLOW
F/CTL FLAP SYS 1(2) FAULT
Applicable to: ,
�� If FLAP sys 1 fault:
GPWS FLAP MODE...............................................................................................................OFF
STATUS
ENG 1(2) APPR IDLE ONLY
FLAPS SLOW
F/CTL FLAP SYS 1(2) FAULT
Applicable to: ,
MSN,,,,
�� If FLAP sys 1 fault:
GPWS FLAP MODE...............................................................................................................OFF
STATUS
ENG 1(2) APPR IDLE ONLY
FLAPS SLOW
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 39/146
FCOM 19 AUG 10
F/CTL SLAT (FLAP) TIP BRK FAULT
Applicable to: ALL
L2 Failure of one slat or flap wingtip brake.
Crew awareness
F/CTL L(R) SIDESTICK FAULT
Applicable to: ALL
L2Crew awareness
F/CTL FLAP ATTACH SENSOR
Applicable to: ALL
L2Failure of flap attachment failure detection sensor.
Crew awareness
CONFIG SLATS (FLAPS) NOT IN T.O CONFIG
Applicable to: ALL
L2Crew 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 40/146
FCOM 19 AUG 10
F/CTL ELAC 1(2) FAULT
(ONE COMPUTER FAILED)
Applicable to:
CAUTION Do not reset ELAC, if uncommanded maneuvers occurred during the flight.
ELAC (AFFECTED).....................................................................................................OFF THEN ON
Note: 1. In some sidestick transducer failure cases, ELAC 1(2) FAULT is triggered without the
proc, and FAULT It on associated pb does not come on.
2. ELAC FAULT may be triggered during engine start, due to the electrical transient. To
　
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