Page 20 - Demo
P. 20

2.10/14b
REV 27
CHINA AIRLINES
A330
REV 27
PAGE 14b
AIR ENG 1+2 BLEED RESET (APU BLEED NOT AVAILABLE)
Apply this procedure when both engine bleed supply systems are failed and after the completion of the AIR ENG 1+2 BLEED FAULT ECAM procedure and if no APU Bleed is available to supply the aircraft.
MAX FL 100/MEA-MORA AVOID ICING CONDITIONS
If no message associated with AIR ENG 1+2 BLEED FAULT and
If no ENG BLEED lost due to ENG FIRE or Start Air
Valve failed open or APU leak fed by engine:
– PACK 1 ............................................................................ ON
– APPR SPD .................................................... VLS+10 KT
– PACK 2 ............................................................................ ON
– ENG 1 BLEED.................................................................. ON – ENG 2 BLEED ................................................................. ON ! IfnoENGBLEEDrecovered:
– ENG 1 BLEED...........................................................OFF
– ENG 2 BLEED...........................................................OFF If only LEFT LEAK message associated with AIR ENG
1+2 BLEED FAULT or
If only ENG 1 BLEED lost due to ENG 1 FIRE or Start Air Valve 1 failed open or APU leak fed by engine :
– PACK 2 .............................................................................. ON – ENG 2 BLEED ............................................................ON
! IfnoENGBLEEDrecovered:
– ENG 2 BLEED...........................................................OFF
If only RIGHT LEAK message associated with AIR ENG 1+ 2 BLEED FAULT or
If only ENG 2 BLEED lost due to ENG 2 FIRE or Start Air Valve 2 failed open:
– PACK 1 ............................................................................ ON – ENG 1 BLEED.................................................................. ON ! IfnoENGBLEEDrecovered:
– ENG 1 BLEED...........................................................OFF If both LEFT LEAK and RIGHT LEAK messages associated with AIR ENG 1+2 BLEED FAULT or
If both ENG BLEEDs are lost due to ENG FIRE or Start Air Valve failed open or APU leak fed by engine :
No ENG BLEED can be recovered.
Consider unsuccessful.
! If unsuccessful (no ENG BLEED recovered): ! WhenDIFFPR<1PSI
– RAM AIR ..........................................................ON ! If severe ice accretion :
– MIN SPD ..................................VLS + 10 / G DOT MANEUVER WITH CARE
! If severe ice accretion during approach:
– APPR SPD ....................................... VLS + 10 KT – LDG DIST PROC .......................................APPLY


































































































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