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This line is replaced by “FOR LDG: USE FLAP 3” when
CONF 3 is selected, as a reminder
�� 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 + 2 + 4
L + R INR AIL
N/W STRG
NORM BRK
AUTO BRK
ALTN BRK
YAW DAMPER 1
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 82/164
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.
Landing distance increases due to the increase in
approach speed, loss of antiskid, and partial loss of
ground spoilers.
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.
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 83/164
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 84/164
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
　
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