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Ensure cross checking of vital controls before moving them: thrust lever, master switch etc.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.70 Page 4
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
POWER PLANT
CHAP03\70
ENGINE RELIGHT IN FLIGHT (END)
06 - COMPLETION STANDARDS
· Uses all available information to make a sound decision to attempt an engine relight in
flight.
· Applies correct engine relight procedure and respects all related limitations.
· Ensures correct task sharing and good crew communications.
07 - COMMON ERRORS
· Relight attempt made without checking engine parameters.
· Actions requiring crew confirmation not cross checked during relight (e.g. Eng Master "on"
or "off").
· No timing for light-up or engine draining.
· Procedure initiated at inappropriate time in relation to workload and without checklist.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.70 Page 5
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
POWER PLANT
CHAP03\70
ALL ENGINE FLAME OUT
01 - TRAINING OBJECTIVE
· To establish a safe flight path.
· To recognize the indications of a dual engine failure.
· To carry out correct procedure.
02 - SCHEDULE
Briefing duration : 20 minutes
03 - EQUIPMENT
DOC references :
· QRH 1.01 to 1.04 (Systems remaining)
· QRH 2.18 (Engine relight in flight)
· FCOM 1.70.80 (Ignition and starting)
· FCOM 3.02.70 (Engine Dual Failure)
04 - INSTRUCTOR’S ACTIONS
Briefing of the following key points.
MAIN
· Monitoring of flight path and parameters.
· Choice of optimum speed.
· ECAM actions (APU use, relight parameters...).
· Situational awareness.
· Relight monitoring and system recovery.
SECONDARY
· Aircraft status : systems, F/CTL law..
· Minimum RAT speed.
· Communications (ATC, transponder, cabin).
· Related consequences (Pressurization, forced landing, ditching...).
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.70 Page 6
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
POWER PLANT
CHAP03\70
ALL ENGINE FLAME OUT (END)
05 - TRAINEES’ ACTIONS
Following a dual engine failure the flight deck indications change drastically as generators
drop off line, the RAT is deployed and ECAM prioritizes checklists.
Control of the aircraft must be taken immediately by CM1, and a safe flight path established.
It is important at this stage to correctly identify the failure as it can be easily confused with all
engine generators fault. ECAM will prioritize checklists so to avoid confusion read ECAM
carefully to correctly identify the failure. It is vital to establish good crew communications and
to apply efficient task-sharing.
Establish communications with ATC, stating nature of emergency and intentions. Consider
use of transponder emergency code.
The ECAM actions can be commenced, with attention to optimum relight speed . If there is
no relight within 30 sec ECAM will order the engine master switches to be placed off for 30
sec and then on again. This is to permit ventilation of the combustion chamber. Start the
APU.
Maximum gliding range is achieved at green dot speed. Think ahead and plan the approach.
Depending on the airplane’s position, a forced landing or a ditching may be required if the
relight is unsuccessful. Find the relevant QRH page and review the procedure.
The list of affected systems is long and flight controls will be much degraded. If the relight
attempts are successful, consider the options of immediate landing versus continuing the
flight. If the engines failed simultaneously, was there a common cause ?
At all times, maintain correct speed and situational awareness.
06 - COMPLETION STANDARDS
· Establishes immediately a safe flight path.
· Makes correct analysis and carries out procedure.
· Ensures strict application of task-sharing and good crew communications.
· Makes appropriate decision according to outcome of relight attempt.
07 - COMMON ERRORS
· Incorrect speed choice and lack of monitoring.
· Confusion with ELEC EMER CONFIG.
· Lack of situational awareness.
· APU started too late.
· Engine relight not monitored (stopwatch/parameters).
· Lack of communication.
A319/A320/A321
FLIGHT CREW TRAINING MANUAL
1.03.70 Page 7
REV 21 MAY 98
ABNORMAL OPERATION BRIEFINGS
POWER PLANT
CHAP03\70
　
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