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LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2
CAT 2
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 86/142
FCOM 19 AUG 10
F/CTL STAB CTL FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 330/.82
• IF TRIM LOCKED > 8 UP:
MAX SPEED......................................................180 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
IF MAN TRIM NOT AVAIL:
PITCH AUTHORITY REDUCED
Start the flare slightly earlier. More stick deflection may be
needed to achieve the flare
GPWS FLAP MODE.........................................................OFF
FOR LDG............................................................ USE FLAP 2
Do not select CONF FULL or CONF 3 so as not to degrade
handling qualities.
APPR SPD..........................................................VLS + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2
CAT 2
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 87/142
FCOM 19 AUG 10
F/CTL STAB CTL FAULT
Applicable to:
MAN PITCH TRIM................................................................................................................... CHECK
L2 The force needed on the pitch trim wheel may be higher than usual (pre-takeoff manual setting).
L1 IF MAN TRIM AVAIL:
TRIM FOR NEUTRAL ELEV
L2 If man pitch trim is available, trim to maintain elevator at zero position (indications on F/CTL SD
page). To improve the longitudinal control of the aircraft, it is recommended to disconnect the
autothrust.
L1 IF TRIM LOCKED > 8 UP:
MAX SPEED...................................................................................................................... 180 KT
L2 If trim is locked above 8 ° up, pitch down authority may not be sufficient for speed above 180 kt.
Select configuration as appropriate - Fuel consumption is increased.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...........................................................................................................................330/.82
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 88/142
FCOM 19 AUG 10
F/CTL STAB CTL FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 330/.82
• IF TRIM LOCKED > 8 UP:
MAX SPEED......................................................180 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
IF MAN TRIM NOT AVAIL:
PITCH AUTHORITY REDUCED
Start the flare slightly earlier. More stick deflection may be
needed to achieve the flare
GPWS FLAP MODE.........................................................OFF
FOR LDG............................................................ USE FLAP 2
Do not select CONF FULL or CONF 3 so as not to degrade
handling qualities.
APPR SPD..........................................................VLS + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2
CAT 2
CONFIG PITCH TRIM NOT IN T.O RANGE
Applicable to: ALL
L2Crew awareness
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 89/142
FCOM 19 AUG 10
F/CTL SPLR FAULT
Applicable to: ,
L2 Loss of one or more spoilers.
Crew awareness
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
INCREASED FUEL CONSUMP
See (1)
INOP SYS
PART (HALF, MOST, ALL)
SPLRS
(1) AL2ppears when one or more spoilers remain partly (deflection greater than 6 °), or fully extended.
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(101)
