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action in case of an
abnormal start.
Engine light up must be achieved within 30 s after fuel flow increases.
�� 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 ENG SHUT DOWN procedure has
been applied, the
TCAS mode selector may have been set at the TA position.
Affected
SYS............................................................................................................................
RESTORE
�� If no relight :
ENG MASTER
(affected)....................................................................................................................OF
F
Wait 30 s before attempting a new start (to drain the engine).
IN FLIGHT ENGINE RELIGHT ENVELOPE
ABN-70
9/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , ,
ENG 1(2) STALL
�� On the ground :
THR LEVER (AFFECTED
ENGINE)................................................................................................. IDLE
ENG MASTER (AFFECTED
ENGINE).............................................................................................. OFF
�� In flight :
THR LEVER (AFFECTED
ENGINE)................................................................................................. IDLE
ENG PARAMETERS (AFFECTED
ENGINE)............................................................................... CHECK
�� IF ABNORMAL :
ENG MASTER (AFFECTED
ENGINE)........................................................................................OFF
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
�� Normal :
ENG A.ICE (AFFECTED
ENGINE)............................................................................................... ON
WING
A.ICE...............................................................................................................................
..ON
THR LEVER (AFFECTED ENGINE).................................................................
SLOWLY ADVANCE
�� If a stall recurs :
THR LEVER (AFFECTED
ENGINE).............................................................................REDUCE
�� If a stall does not recur :
Continue engine operation.
ENG TAILPIPE FIRE
CAUTION External fire agents can cause severe corrosive damage and should,
therefore, only be
considered after having applied following procedure :
MAN
START............................................................................................................................
................OFF
ENG MASTER
(affected)........................................................................................................................
OFF
AIR BLEED
PRESS.....................................................................................................................
ESTABLISH
BEACON.........................................................................................................................
........................... ON
ENG MODE
SEL...............................................................................................................................
CRANK
MAN
START............................................................................................................................
................. ON
�� When burning has stopped :
MAN
START............................................................................................................................
.........OFF
ENG MODE
SEL............................................................................................................................
NORM
ABN-70
10/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , ,
HIGH ENGINE VIBRATION
�� High N2 vibrations during engine start on ground :
Engine start should be aborted (if vibration indications are available), when the N2
vibration level
exceeds the 6.5-units advisory threshold. The subsequent start is to be initiated after
the engine has
completely spooled down. This procedure may be repeated a maximum of three times.
Report any N2
vibration advisory condition in the logbook.
　
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