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L2 Due to the loss of one elevator.
L1MANOEUVER WITH CARE
L2 To avoid high hydraulic demand on the remaining system.
Note: As a general rule, do not manually select a HYD ELEC PUMP ON, except temporarily, to
retract the spoilers if they remain out after a hydraulic failure.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...........................................................................................................................330/.82
SECONDARY FAILURES
*WHEEL
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A330/A340 FLEET PRO-ABN-29 P 98/164
FCOM 19 AUG 10
HYD G + B SYS LO PR (Cont'd)
*F/CTL
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A330/A340 FLEET PRO-ABN-29 P 99/164
FCOM 19 AUG 10
HYD G + B SYS LO PR (Cont'd)
L12
STATUS
SPD BRK ..................................................... DO NOT USE
MAX SPEED.......................................................... 330/0.82
MIN RAT SPEED (IF RAT EXTENDED).................. 140 KT
MANEUVER WITH CARE
MAX BRK PR........................................................1000 PSI
APPR PROC
If system lost by RSVR LO AIR PR:
AFFECTED ENG PUMP.................................................... ON
If system lost by RSVR OVHT:
IF GREEN OVHT OUT:
GREEN ENG 1 + 2 PUMP.......................................... ON
IF BLUE OVHT OUT:
BLUE ENG 1 PUMP.................................................... ON
If HYD not recovered:
BEFORE S/F EXTENSION and if ENG 1 S/D:
BLUE ELEC PUMP.................................................... OFF
Switch OFF the yellow electrical pump to avoid flight
control jerk, in case Engine 1 is additionally lost.
GPWS FLAP MODE (IF S < 2).........................................
....................................................................................OFF
S/F JAMMED PROC..............................................APPLY
FOR LDG (IF S < 2).........................................................
......................................................................USE FLAP 2
FOR LDG (IF S ≥ 2).........................................................
......................................................................USE FLAP 3
FOR L/G GRVTY EXTN:
MAX SPEED..........................................................200 KT
LDG GRVTY EXTN................................................DOWN
INOP SYS
F/CTL PROT
G + B HYD
ANTI SKID
L/G RETRACT
AP 1 + 2
SLATS
L ELEV
MOST SPLRS
REV 1 (PW/RR Eng)
L + R INR AIL
N/W STRG
AUTO BRK
NORM BRK
ALTN BRK
CAT 2
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A330/A340 FLEET PRO-ABN-29 P 100/164
FCOM 19 AUG 10
HYD G + B SYS LO PR (Cont'd)
WHEN L/G DOWNLOCKED:
L/G LEVER.............................................................DOWN
APPR SPD (IF S ≥ 1).......................................................
..................................................................... VLS + 10 KT
Approach speed must be increased, due to the loss of
one elevator.
LDG DIST PROC...................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
CONSIDER RAT MAN USE
See (1)
BRK B ACCU PR ONLY
See (2)
INCREASED FUEL CONSUMP
See (3)
FLAPS SLOW
See (4)
(1) “LC2ONSIDER RAT MAN USE” is not triggered in case of: A green reservoir overheat, or in the
case of a G + B hydraulic system low level.
(2) 7 full brake applications are available.
(3) Fuel consumption increases by approximately 16 %, due to the inner ailerons in the upfloat
position.
(4) Note: Following a blue hydraulic system failure, the parking brake may be inoperative due to
blue accumulator low pressure.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A330/A340 FLEET PRO-ABN-29 P 101/164
FCOM 19 AUG 10
HYD G + Y SYS LO PR
Applicable to:
LAND ASAP
CONSIDER RAT MAN USE
L2 "CONSIDER RAT MAN USE" is not triggered, in case of a green reservoir overheat.
Note: With RAT extended, the green system is recovered. This permits to recover the flap
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(3)
