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If ENG 2 BLEED is lost first :
PACK
2................................................................................................................................OFF
ENGINE 1
BLEED...................................................................................................................ON
If engine bleed recovery was not successful, or if one pack is inoperative :
X BLEED.....................................................................................................................
CHECK OPEN
DESCENT TO
FL200/MEA.............................................................................................. CONTINUE
Descend rapidly to FL 200, to recover the bleed supply from the APU
APU.................................................................................................................................
.......START
Start the APU during the descent.
AT, OR BELOW, FL200 :
WING
A.ICE...........................................................................................................................O
FF
APU BLEED must not be used for wing anti-ice.
APU
BLEED..........................................................................................................................
ON
To be continued on next page
ABN-36
2/2
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
AIR DUAL BLEED FAULT (Cont'd)
MAX FL200
AVOID ICING CONDITIONS
ABN-36
1/4
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , ,
AIR DUAL BLEED FAULT
ENG 1 BLEED failure :
This procedure is to be applied if ENG 1 BLEED was lost due to a :
‐ LEAK on side 1, or
‐ ENG 1 FIRE, or
‐ Start Air Valve 1 failed open.
DESCENT TO
FL100/MEA.........................................................................................................INITIA
TE
Descend rapidly to FL 100/MEA, to prevent excessive cabin altitude.
AVOID ICING CONDITIONS
ENG 2 BLEED failure :
This procedure is to be applied if ENG 2 BLEED was lost due to a :
‐ LEAK on side 2, or
‐ ENG 2 FIRE, or
Start ‐ Air Valve 2 failed open.
X BLEED.......................................................................................................................
CHECK CLOSED
DESCENT TO
FL200/MEA.........................................................................................................INITIA
TE
Descend rapidly to FL 200, to recover the bleed supply from the APU.
APU.................................................................................................................................
............. START
Start the APU during the descent.
AT, OR BELOW, FL200 :
WING
A.ICE...............................................................................................................................
OFF
APU BLEED must not be used for wing anti-ice.
APU
BLEED............................................................................................................................
.....ON
MAX FL200
AVOID ICING CONDITIONS
In all other cases :
DESCENT........................................................................................................................
.......... INITIATE
Descend rapidly to FL 200, so that the bleed supply may be supplied by the APU, if
the bleed system
recovery is not successful.
If both packs are available :
If both packs are operative, it can be suspected that the second bleed system failed due
to
excessive demand. Recovery of the second failed engine bleed may be attempted.
If ENG 1 BLEED is lost first :
PACK
1................................................................................................................................OFF
ENGINE 2
BLEED...................................................................................................................ON
If ENG 2 BLEED is lost first :
PACK
2................................................................................................................................OFF
ENGINE 1
BLEED...................................................................................................................ON
If engine bleed recovery was not successful, or if one pack is inoperative :
X BLEED.....................................................................................................................
CHECK OPEN
DESCENT TO
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空客320快速檢查單QRH QUICK REFERENCE HAND BOOK4(16)
