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POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 82/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) N1/N2 OVERLIMIT
Applicable to:
�� Maximum pointer indications:
L2N1 between 104.2 % and 105.2 % or
N2 between 105 % and 105.8 %.
L1 THR LEVER (AFFECTED ENGINE)...................................................................... BELOW LIMIT
L2Normal operation may be resumed to next landing.
Report in maintenance logbook.
L1�� Maximum pointer indications:
L2N1 above 105.2 %or
N2 above 105.8 %
L1 THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
L2 If conditions do not permit engine shutdown, land as soon as possible using the minimum thrust
required to sustain safe flight.
L12
ASSOCIATED PROCEDURES
ENG 1(2)(3)(4) SHUT DOWN
Refer to PRO-ABN-70-A After ENG 1(2)(3)(4) SHUT DOWN
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 83/196
FCOM 19 AUG 10
ENG 1(2)(3)(4) EGT OVERLIMIT
Applicable to:
�� Maximum pointer indications:
L2 EGT above 915 °C (or 950 °C at takeoff power) and below 990 °C:
L1 THR LEVER (AFFECTED ENGINE)...................................................................... BELOW LIMIT
L2Normal operation may be resumed to next landing.
Report in maintenance logbook.
L1�� Maximum pointer indications:
L2 EGT above 990 °C:
L1 THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
L2 If conditions do not permit engine shutdown, land as soon as possible using the minimum thrust
required to sustain safe flight.
L1
ASSOCIATED PROCEDURES
ENG 1(2)(3)(4) SHUT DOWN
Refer to PRO-ABN-70-A After ENG 1(2)(3)(4) SHUT DOWN
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 84/196
FCOM 19 AUG 10
ENG 1(2) EGT OVERLIMIT
Applicable to: ,
�� Maximum pointer indications:
L2 EGT above 850 °C, or above 920 °C (or above 900 °C for more than 20 s), at takeoff power.
L1 THR LEVER (AFFECTED ENGINE)...................................................................... BELOW LIMIT
L2Normal operation may be resumed to next landing.
Report in maintenance logbook.
L1�� If THR LEVER at idle for more than 5 s:
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
L2 If conditions do not permit engine shut down land as soon as possible using the minimum thrust
required to sustain safe flight.
L1
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-B After ENG 1(2) SHUT DOWN
ENG 1(2) OVSPD PROT FAULT
Applicable to: ,
L2 A failure affects the overspeed protection system.
Maintenance action is due.
Crew awareness.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWERPLANT
A330/A340 FLEET PRO-ABN-70 P 85/196
FCOM 19 AUG 10
ENG TYPE DISAGREE
Applicable to: ALL
L2 The engine ratings seen by the FWC are not identical for all engines, or they are different from the
rating memorized by the FWC.
Crew awareness.
ENG 1(2)(3)(4) REV PRESSURIZED
Applicable to:
L2 The reverse thrust system is pressurized, without reverse deployment order.
L1�� If IDLE is not automatically selected by the FADEC:
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
�� If IDLE is automatically selected by the FADEC:
ENG (AFFECTED) AT IDLE
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
L2 Select thrust lever at idle, even if idle is automatically selected by the FADEC.
ENG 1(2) REV PRESSURIZED
Applicable to: ,
L2 Reverse thrust system is pressurized without reverse deployment order.
L1�� If IDLE automatically selected by FADEC:
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
L2 Select thrust lever at idle, even if idle is automatically selected by the FADEC.
ENG 1(2)(3)(4) REV INHIBITED
Applicable to:
L2 Reverse is inhibited by maintenance action.
Crew awareness.
To be continued on next page
　
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