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AVOID ICING CONDITIONS
ASSOCIATED PROCEDURES
AIR ABNORM BLEED CONFIG
L12
STATUS
• If more than one BLEED LO TEMP:
AVOID ICING CONDITIONS
APPR PROC
IF ICE ACCRETION:
APPR SPD...........................................................VLS +10 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
INOP SYS
WING A. ICE
ENG 1(2)(3)(4) BLEED
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A330/A340 FLEET PRO-ABN-36 P 22/30
FCOM 19 AUG 10
AIR BLEED LO TEMP (Cont'd)
L12
STATUS
• If both BLEEDs LO TEMP:
AVOID ICING CONDITIONS
APPR PROC
IF ICE ACCRETION:
APPR SPD...........................................................VLS +10 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
INOP SYS
WING A. ICE
ENG 1(2) BLEED
AIR BLEED LO TEMP
Applicable to:
ON BLEED 1(2)
L2 In flight, engine bleed temperature is too low for correct wing deicing.
L1 ENG PWR.......................................................................................................................... INCREASE
L2 The thrust lever of the affected engine must be advanced with the autothrust OFF.
Low bleed temperature may be due to low outside air temperature. Therefore, increasing engine
thrust may increase bleed temperature and clear the ECAM caution.
L1 If one BLEED LO TEMP:
IF UNSUCCESSFUL:
ENG BLEED (AFFECTED).............................................................................................. OFF
If both BLEEDs LO TEMP:
WING ANTI ICE......................................................................................................................OFF
AVOID ICING CONDITIONS
ASSOCIATED PROCEDURES
AIR ABNORM BLEED CONFIG
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A330/A340 FLEET PRO-ABN-36 P 23/30
FCOM 19 AUG 10
AIR BLEED LO TEMP (Cont'd)
L12
STATUS
• If both BLEEDs LO TEMP:
AVOID ICING CONDITIONS
IF SEVERE ICE ACCRETION:
MIN SPD....................................................... VLS +10/G DOT
MANEUVER WITH CARE
APPR PROC
IF SEVERE ICE ACCRETION:
APPR SPD...........................................................VLS +10 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
INOP SYS
WING A. ICE
ENG 1(2) BLEED
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A330/A340 FLEET PRO-ABN-36 P 24/30
FCOM 19 AUG 10
AIR APU BLEED LEAK
Applicable to:
If the APU line leak is fed by an engine bleed:
APU LEAK FED BY ENG
APU BLEED (IF NOT AUTOMATICALLY CLOSED)....................................................................OFF
L2With the APU BLEED pb-sw ON, the FAULT light remains on.
With the APU BLEED pb-sw off, the FAULT light goes off when the overheat disappears.
L1 If the APU line leak is fed by an engine bleed and engine bleed valve autoclosure is
inoperative:
ENG 1 BLEED........................................................................................................................OFF
ENG 2 BLEED........................................................................................................................OFF
L12
ASSOCIATED PROCEDURES
AIR ABNORMAL BLEED CONFIG
L2 If the APU line leak is fed by an engine bleed.
STATUS
INOP SYS
ENG 1 BLEED
ENG 2 BLEED
APU BLEED
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A330/A340 FLEET PRO-ABN-36 P 25/30
FCOM 19 AUG 10
AIR APU BLEED LEAK
Applicable to: ,
If the APU line leak is fed by an engine bleed:
APU LEAK FED BY ENG
APU BLEED (IF NOT AUTOMATICALLY CLOSED)....................................................................OFF
L2With the APU BLEED pb-sw ON, the FAULT light remains on.
With the APU BLEED pb-sw off, the FAULT light goes off when the overheat disappears.
L1 If the APU line leak is fed by an engine bleed, and engine bleed valve autoclosure is
inoperative:
ENG 1 BLEED........................................................................................................................OFF
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 8(118)
