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FINAL TAKE-OFF SEGMENT
As the speed trend arrow reaches Green Dot speed, pull for OPEN CLIMB, set THR MCT when
the LVR MCT message flashes on the FMA (triggered as the speed index reaches green dot)
and resume climb using MCT. If the thrust levers are already in the FLX/MCT detent, move
levers to CL and then back to MCT.
When an engine failure occurs after take-off, noise abatement procedures are no longer a
requirement. Additionally, the acceleration altitude provides a compromise between obstacle
clearance and engine thrust limiting time. It allows the aircraft to be configured to Flap 0 and
green dot speed, which provides the best climb gradient.
Once established on the final take-off flight path, continue the ECAM until the STATUS
is displayed. At this point, the AFTER T/O checklist should be completed, computer reset
considered and OEBs consulted (if applicable). STATUS should then be reviewed.
ONE ENGINE OUT FLIGHT PATH
The one engine out flight path will be flown according to the take-off briefing made at the gate:
• The EOSID (with attention to the decision point location)
• The SID
• Radar vector...
A330/A340 FLIGHT CREW TRAINING MANUAL
ABNORMAL OPERATIONS
OPERATING TECHNIQUES
A330/A340 FLEET AO-020 P 11/18
FCTM 17 JUN 09
Engine failure after V1
ENGINE FAILURE DURING INITIAL CLIMB
Applicable to: ALL
Proceed as above. If the failure occurs above V2 however, maintain the SRS commanded attitude. In
any event the minimum speed must be V2.
When an engine failure is detected, the FMGS produces predictions based on the engine-out
configuration and any pre-selected speeds entered in the MCDU are deleted.
ENGINE FAILURE DURING CRUISE
Applicable to: ALL
GENERAL
There are three strategies available for dealing with an engine failure in the cruise:
• The standard strategy
• The obstacle strategy
• The fixed speed strategy
A330/A340 FLIGHT CREW TRAINING MANUAL
ABNORMAL OPERATIONS
OPERATING TECHNIQUES
A330/A340 FLEET AO-020 P 12/18
FCTM 17 JUN 09
The fixed speed strategy refers to ETOPS (A330 only). It is discussed inRefer to FCOM/99 Duref
Cible FCOM and is discussed in a separate course.
Unless a specific procedure has been established before dispatch (considering ETOPS or
mountainous areas), the standard strategy is used.
Note: Pressing the EO CLR key on the MCDU restores the all engine operative predictions and
performance. Reverting to one engine-out performance again is not possible.
PROCEDURE
As soon as the engine failure is recognized, the PF will simultaneously:
• Set MCT on the remaining engine(s)
• Disconnect A/THR
Then, PF will
• Select the SPEED according to the strategy
• If appropriate, select a HDG to keep clear of the airway, preferably heading towards an
alternate. Consideration should be given to aircraft position relative to any relevant critical point
• Select the appropriate engine inoperative altitude in the FCU ALT window and pull for OPEN
DES
Then, PF will
• Require the ECAM actions
At high flight levels close to limiting weights, crew actions should not be delayed, as speed will
decay quickly requiring prompt crew response. The crew will avoid decelerating below green dot.
A330/A340 FLIGHT CREW TRAINING MANUAL
ABNORMAL OPERATIONS
OPERATING TECHNIQUES
A330/A340 FLEET AO-020 P 13/18
FCTM 17 JUN 09
Engine failure during cruise flow pattern
The A/THR is disconnected to avoid any engine thrust reduction when selecting speed according
to strategy or when pulling for OPEN DES to initiate the descent. With the A/THR disconnected,
the target speed is controlled by the elevator when in OPEN DES.
Carrying out the ECAM actions should not be hurried, as it is important to complete the drill
correctly. Generally, there will be sufficient time to cross check all actions.
STANDARD STRATEGY
Set speed target M 0.82/300 kt. The speed of M 0.82/300 kt is chosen to ensure the aircraft is
within the stabilised windmill engine relight in-flight envelope.
The REC MAX EO Cruise altitude, which equates to LRC with anti-icing off, is displayed on the
MCDU PROG page and should be set on the FCU. (Cruise altitude and speed are also available in
the QRH in case of double FM failure).
If V/S becomes less than 500 ft/min, select V/S - 500 ft/min and A/THR on. This is likely to occur
as level off altitude is approached.
Once established at level off altitude, long-range cruise performance with one engine out may be
extracted from QRH or Refer to FCOM/PER-CRZ-OEI-GEN-10 PROCEDURE.
A330/A340 FLIGHT CREW TRAINING MANUAL
　
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