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STATUS
AVOID ICING CONDITIONS
• IF A/C ICING SEVERE:
MIN SPD.................................................ALPHA PROT
INOP SYS
WING A. ICE
AIR ENG 1(2) BLEED LO TEMP
(OPPOSITE BLEED NOT AVAILABLE)
Applicable to:
L2 In flight, engine bleed temperature is too low for correct wing de-icing.
L1 A/THR.......................................................................................................................................... OFF
THR LEVER (AFFECTED ENGINE)...................................................................................ADVANCE
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 UNSUCCESSFUL:
WING A. ICE.......................................................................................................................... OFF
AVOID ICING CONDITIONS
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A318/A319/A320/A321 FLEET PRO-ABN-36 P 48/54
FCOM 19 AUG 10
AIR ENG 1(2) BLEED LO TEMP (Cont'd)
(OPPOSITE BLEED NOT AVAILABLE)
STATUS
AVOID ICING CONDITIONS
• IF A/C ICING SEVERE:
MIN SPD.................................................ALPHA PROT
INOP SYS
WING A. ICE
L12
STATUS
AVOID ICING CONDITIONS
• IF SEVERE ICE ACCRETION:
MIN SPD...........................................VLS +10 / G DOT
MANEUVER WITH CARE
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
INOP SYS
WING A. ICE
AIR ENG 1(2) BLEED LO TEMP
(OPPOSITE BLEED NOT AVAILABLE)
Applicable to:
L2 In flight, engine bleed temperature is too low for correct wing de-icing.
L1 A/THR.......................................................................................................................................... OFF
THR LEVER (AFFECTED ENGINE)...................................................................................ADVANCE
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 UNSUCCESSFUL:
WING A. ICE.......................................................................................................................... OFF
AVOID ICING CONDITIONS
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A318/A319/A320/A321 FLEET PRO-ABN-36 P 49/54
FCOM 19 AUG 10
AIR ENG 1(2) BLEED LO TEMP (Cont'd)
(OPPOSITE BLEED NOT AVAILABLE)
STATUS
AVOID ICING CONDITIONS INOP SYS
WING A. ICE
L12
STATUS
AVOID ICING CONDITIONS
• IF SEVERE ICE ACCRETION:
MIN SPD...........................................VLS +10 / G DOT
MANEUVER WITH CARE
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
INOP SYS
WING A. ICE
AIR ENG 1(2) BLEED LO TEMP
(OPPOSITE BLEED NOT AVAILABLE)
Applicable to: , , MSN,,,,
L2 In flight, engine bleed temperature is too low for correct wing de-icing.
L1 A/THR.......................................................................................................................................... OFF
THR LEVER (AFFECTED ENGINE)...................................................................................ADVANCE
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 UNSUCCESSFUL:
WING A. ICE.......................................................................................................................... OFF
AVOID ICING CONDITIONS
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
PNEUMATIC
A318/A319/A320/A321 FLEET PRO-ABN-36 P 50/54
FCOM 19 AUG 10
AIR ENG 1(2) BLEED LO TEMP (Cont'd)
(OPPOSITE BLEED NOT AVAILABLE)
L12
STATUS
AVOID ICING CONDITIONS
• IF SEVERE ICE ACCRETION:
MIN SPD...........................................VLS +10 / G DOT
　
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