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POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 48/194
FCOM 19 AUG 10
ENG RELIGHT
(IN FLIGHT)
Applicable to:
, , MSN
MAX ALTITUDE........................................................................................................................... See
ENG MASTER (affected).............................................................................................................. OFF
THR LEVER (affected)......................................................................................................Check IDLE
ENG MODE SEL............................................................................................................................IGN
X BLEED.................................................................................................................................. OPEN
If outside the windmilling start envelope, the FADEC will open the starter valve.
WING A. ICE (for starter assist)................................................................................................... OFF
ENG MASTER (affected)................................................................................................................ ON
Be aware that, unlike the procedure for auto start on ground, the crew must take appropriate action
in case of an abnormal start.
Engine light-up must be achieved within 30 s after the fuel flow increases.
Monitor N2. If uncertain about successful relight, move the thrust lever forward and check engine
response.
ENG PARAMETERS (N2, EGT)..............................................................................................CHECK
�� When idle is reached (AVAIL indication pulses in green):
ENG MODE SEL.................................................................................................................NORM
TCAS MODE SEL �� .............................................................................................check TA/RA
Check that the selector is at TA/RA since, if the Refer to PRO-ABN-70-I After ENG 1(2) SHUT
DOWNhas been applied, the TCAS mode selector may have been set to the TA position.
Affected SYS................................................................................................................ RESTORE
Restore affected systems, and set the X BLEED rotary selector to AUTO.
�� If no relight:
ENG MASTER (affected)........................................................................................................OFF
Wait 30 s before attempting a new start (to drain the engine).
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 49/194
FCOM 19 AUG 10
ENG RELIGHT (Cont'd)
(IN FLIGHT)
ENG 1(2) EGT EXCEEDED DURING AIR START
Applicable to: MSN
4566,,,
L2 EGT limit has been exceeded during ENG relight in flight (only displayed on ground).
Report in maintenance log.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
POWER PLANT
A318/A319/A320/A321 FLEET PRO-ABN-70 P 50/194
FCOM 19 AUG 10
ENG 1(2) FAIL
Applicable to: MSN
4566,,,
L2 An engine flame-out may be recognized by a rapid decrease in EGT, N2, FF and EPR.
Engine damage may be accompanied by:
‐ Loud noise,
‐ Significant increase in aircraft vibrations and/or buffeting,
‐ Repeated or uncontrollable engine stalls,
‐ Associated abnormal indications such as hydraulic fluid loss, or no N2 indication.
L1 LAND ASAP
�� Before takeoff or after landing:
THR LEVER (AFFECTED ENGINE)..................................................................................... IDLE
ENG MASTER (AFFECTED ENGINE)...................................................................................OFF
�� IF DAMAGE:
ENG FIRE P/B (AFFECTED ENGINE)......................................................................... PUSH
AGENT 1...................................................................................................................... DISCH
�� IF NO DAMAGE:
ENG (AFFECTED) RELIGHT...............................................................................CONSIDER
L2 If no damage, a new start sequence may be initiated.
L12
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
Refer to PRO-ABN-70-I After ENG 1(2) SHUT DOWN
If damage or if engine relight is unsuccessful.
L1�� In flight:
ENG MODE SEL..................................................................................................................... IGN
L2 Selection of continuous ignition confirms the immediate relight attempt made by the FADEC.
　
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