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WHEN L/G DOWNLOCKED:
L/G LEVER.............................................................DOWN
APPR SPD (IF F ≥ 2)..............................................................
............................................................................. VLS+ 10 KT
Approach speed increases, due to the loss of one elevator.
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM. Landing distance increases due to the increase
in approach speed and the partial loss of ground spoilers.
ALTN LAW: PROT LOST
CONSIDER RAT MAN USE
See (1)
SLATS SLOW
CAT 1 ONLY
INCREASED FUEL CONSUMP
See (2)
(1) “LC2ONSIDER RAT MAN USE” is not triggered in case of green reservoir overheat or a green
hydraulic system low level.
(2) Fuel consumption increases by approximately 16 %, due to the inner ailerons in the upfloat
position.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
HYDRAULIC
A330/A340 FLEET PRO-ABN-29 P 128/164
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
extensions.
However, green pressure will be lost when the speed will drop below 140 kt.
At the time, the red warning "G + Y SYS LO PR" will be triggered again.
With RAT extended, the fuel consumption is approximately increased by 1 %.
L1MIN RAT SPD (NOT DISPLAYED IF G RSVR OVHT)............................................................140 KT
AFFECTED PUMPS......................................................................................................................OFF
USE RUD FOR TURN COORD
L2 Due to the loss of yaw dampers 1 + 2.
L1 SPD BRK.......................................................................................................................DO NOT USE
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
MAX SPEED...........................................................................................................................305/.82
SECONDARY FAILURES
*WHEEL
*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 129/164
FCOM 19 AUG 10
HYD G + Y SYS LO PR (Cont'd)
LAND ASAP
RAT...................................................................................................................................... MAN ON
L2 “RAT MAN ON” is only triggered, on the ECAM in case of G+ Y hydraulic system low level.
L1CONSIDER RAT MAN USE
L2 "CONSIDER RAT MAN USE" is not triggered, in case of a green reservoir overheat, or in case of a
green hydraulic system low level.
Note: With RAT extended, the green system is recovered. This permits to recover the flap
extensions.
However, green pressure will be lost when the speed will drop below 140 kt.
At the time, the red warning "G + Y SYS LO PR" will be triggered again.
With RAT extended, the fuel consumption is approximately increased by 1 %.
L1MIN RAT SPEED ..................................................................................................................... !40 KT
L2Note: The MIN RAT SPEED ...... 140 kt action line is displayed, if the CONSIDER RAT MAN
USE action line is displayed.
L1 AFFECTED PUMPS.................................................................................................OFF CAPT
SPD BRK.......................................................................................................................DO NOT USE
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
*F/CTL
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(13)