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L1 SPD BRK.......................................................................................................................DO NOT USE
L2 Do not use speed brakes, because it is difficult to control the induced pitch moment with manual
pitch trim only.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 98/146
FCOM 19 AUG 10
F/CTL ELEV SERVO FAULT
Applicable to:
L2 The remaining servojack controls the elevator.
L1
L2Crew awareness
L1CAUTION Do not use speedbrakes above 350 kt/M 0.82 (VMO/MMO).
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
F/CTL ELEV SERVO FAULT
Applicable to: ,
L2 The remaining servojack controls the elevator.
L1
L2Crew awareness
L1CAUTION Do not use speedbrakes above 350 kt/M 0.82 (VMO/MMO).
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 99/146
FCOM 19 AUG 10
F/CTL ELEV SERVO FAULT
Applicable to: ,
MSN,,,,
L2 The remaining servojack controls the elevator.
L1
L2Crew awareness
L1CAUTION Do not use speedbrakes above 350 kt/M 0.82 (VMO/MMO).
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
F/CTL L (R) ELEV FAULT
Applicable to:
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
L2Note: If the L(R) elevator fails, the ELACs loose pitch control through the elevator. Therefore,
the SECs control pitch in alternate law. This is not the case, if the right elevator is lost, due
to the failure of B+Y hydraulic circuits. Pitch normal law remains active in ELAC.
L1MAX SPEED...........................................................................................................................320 KT
L2 Speed is limited, due to the loss of high-speed protection.
L1 SPD BRK.......................................................................................................................DO NOT USE
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 100/146
FCOM 19 AUG 10
F/CTL L (R) ELEV FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
SPD BRK.......................................................DO NOT USE
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL, so as not to degrade handling
qualities.
GPWS LDG FLAP 3................................................................. ON
Will be displayed, when flaps in CONF 3.
APPR SPD...............................................................VREF +10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
See (1)
CAT 1 ONLY
INOP SYS
F/CTL PROT
L (R) ELEV
ELAC PITCH
AP 1+2
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll.Refer to
00011770 **Not found**.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 101/146
FCOM 19 AUG 10
F/CTL L (R) ELEV FAULT
Applicable to:
,
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
L2Note: If the L(R) elevator fails, the ELACs loose pitch control through the elevator. Therefore,
the SECs control pitch in alternate law. This is not the case, if the right elevator is lost, due
to the failure of B+Y hydraulic circuits. Pitch normal law remains active in ELAC.
L1MAX SPEED...........................................................................................................................320 KT
L2 Speed is limited, due to the loss of high-speed protection.
L1 SPD BRK.......................................................................................................................DO NOT USE
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 102/146
FCOM 19 AUG 10
F/CTL L (R) ELEV FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
　
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