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and stabilizer.
INOP SYS
F/CTL PROT
STABILIZER
B + Y HYD
AP 1 + 2
MOST SPLRS
ALTN BRK
N/W STRG
CARGO DOORS (if Y LO LVL)
REVERSES (PW/RR Eng.)
L/G DOORS
CAT 2
Note: Following a
blue hyd. sys.
failure, the parking
brake may be
inop. 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 148/164
FCOM 19 AUG 10
HYD B + Y SYS LO PR (Cont'd)
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
ALTN LAW: PROT LOST
SLATS/FLAPS SLOW
HYD B + Y SYS LO PR
Applicable to:
LAND ASAP
AFFECTED PUMPS......................................................................................................................OFF
MANEUVER 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 IF TRIM LOCKED > 8 UP:
MAX SPEED...................................................................................................................... 180 KT
L2 Select the configuration, as appropriate. Fuel consumption is increased.
180 kt is the limit speed. Recommended speed is 160 kt.
Use manual thrust.
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...........................................................................................................................330/.82
SECONDARY FAILURES
*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 149/164
FCOM 19 AUG 10
HYD B + Y SYS LO PR (Cont'd)
L12
STATUS
MAX SPEED.......................................................... 330/0.82
• IF TRIM LOCKED > 8 UP:
MAX SPEED......................................................180 KT
MANEUVER WITH CARE
APPR PROC
If system lost by RSVR LO AIR PR:
AFFECTED ENG PUMP.................................................... ON
If system lost by RSVR OVHT:
IF BLUE OVHT OUT:
BLUE ENG 1 PUMP.................................................... ON
IF YELLOW OVHT OUT:
YELLOW ENG 2 PUMP...............................................ON
IF HYD NOT RECOVERED:
PITCH AUTHORITY...............................................REDUCED
Start the flare earlier. More stick deflection may be needed to
achieve the flare.
GPWS FLAP MODE.........................................................OFF
FOR LDG............................................................ USE FLAP 2
Due to loss of the stabilizer, do not select CONF FULL or 3,
so as not to degrade handling qualities.
FOR L/G GRVTY EXTN:
MAX SPEED..........................................................200 KT
LDG GRVTY EXTN................................................DOWN
WHEN L/G DOWNLOCKED:
L/G LEVER.............................................................DOWN
APPR SPD..........................................................VLS + 10 KT
Approach speed is increased, due to partial loss of spoilers
and stabilizer.
INOP SYS
F/CTL PROT
STABILIZER
B + Y HYD
AP 1 + 2
MOST SPLRS
ALTN BRK
N/W STRG
CARGO DOORS (if Y LO LVL)
REVERSES (PW/RR Eng.)
L/G DOORS
CAT 2
Note: Following a
blue hyd. sys.
failure, the parking
brake may be
inop. 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 150/164
FCOM 19 AUG 10
HYD B + Y SYS LO PR (Cont'd)
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
ALTN LAW: PROT LOST
SLATS/FLAPS SLOW
HYD G (B) (Y) ELEC PUMP FAULT
Applicable to:
L2 In case of an electrical pump overheat, or if an electrical pump fails while in use:
L1 AFFECTED ELEC PUMP..............................................................................................................OFF
L12
STATUS
INOP SYS
G ELEC PUMP (B)(Y)
Note: In case of an
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(20)
