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CTR TK R XFR............................................................................................................................OFF
STATUS
INOP SYS
CTR TK XFR
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A318/A319/A320/A321 FLEET PRO-ABN-28 P 21/42
FCOM 19 AUG 10
FUEL L (R) OUTER (INNER) TK HI TEMP
Applicable to:
L2 This caution may spuriously trigger due to interference from communication equipment.
Therefore, the flight crew should wait 2 min while the fuel temperature measurement is updated.
After 2 min, if the ECAM caution has not disappeared, the flight crew must apply the following
procedure:
L1GALLEY.......................................................................................................................................OFF
L2 Reducing electrical loads reduce heat emitted by IDG.
L1�� On the ground:
LIMITED TAXI TIME
�� If temp reaches 60° C in outer cell or 54° C in inner cell:
DELAY T.O.
ENG MASTER (AFFECTED SIDE)................................................................................. OFF
�� In flight:
ENG F. FLOW (AFFECTED SIDE).............................................................................INCREASE
L2 Disconnect autothrust. Adjust the thrust lever to increase fuel flow through the IDG oil heat
exchanger and decrease the temperature of the fuel returning to the outer cell.
L1�� IF TEMP ABV 65 DEG C in outer cell or 57 DEG C in inner cell:
APU.........................................................................................................................AS RQRD
L2 APU if available may be started and APU GEN used to allow IDG disconnection.
L1�� If opposite GEN avail:
IDG (AFFECTED SIDE).............................................................................................OFF
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A318/A319/A320/A321 FLEET PRO-ABN-28 P 22/42
FCOM 19 AUG 10
FUEL L (R) OUTER (INNER) TK HI TEMP
Applicable to: MSN
4566,
L2 This caution may spuriously trigger due to interference from communication equipment.
Therefore, the flight crew should wait 2 min while the fuel temperature measurement is updated.
After 2 min, if the ECAM caution has not disappeared, the flight crew must apply the following
procedure:
L1GEN (AFFECTED SIDE)...............................................................................................................OFF
�� On the ground:
DELAY T.O.
ENG MASTER (AFFECTED SIDE)........................................................................................OFF
�� In flight:
ENG F. FLOW (AFFECTED SIDE).............................................................................INCREASE
L2 Disconnect autothrust. Adjust the thrust lever to increase fuel flow through the IDG oil heat
exchanger and decrease the temperature of the fuel returning to the outer cell.
L1�� IF TEMP ABV 65 DEG C in outer cell or 57 DEG C in inner cell:
APU.........................................................................................................................AS RQRD
L2 APU if available may be started and APU GEN used to allow IDG disconnection.
L1�� If opposite GEN avail:
IDG (AFFECTED SIDE).............................................................................................OFF
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FUEL
A318/A319/A320/A321 FLEET PRO-ABN-28 P 23/42
FCOM 19 AUG 10
FUEL L (R) WING TK HI TEMP
Applicable to: MSN,
GEN (AFFECTED SIDE)...............................................................................................................OFF
�� On the ground:
DELAY T.O.
ENG MASTER (AFFECTED SIDE)........................................................................................OFF
�� In flight:
ENG. F. FLOW (AFFECTED SIDE)............................................................................ INCREASE
L2 Disconnect autothrust. Adjust the thrust lever to increase fuel flow through the IDG oil heat
exchanger and decrease the temperature of the fuel returning to the wing tank.
L1�� IF TEMP ABV 57 DEG C:
APU........................................................................................................................... S RQRD
L2 APU if available may be started and APU GEN used allow IDG disconnection.
L1�� If opposite GEN avail:
IDG (AFFECTED SIDE).............................................................................................OFF
A318/A319/A320/A321 FLIGHT CREW
　
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