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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
�� N2 between 50 % and IDLE:
ENG MASTER (AFFECTED
ENGINE).............................................................................................. OFF
ASSOCIATED PROCEDURES
ENG 1(2) SHUT DOWN
�� N2 above IDLE (title and procedure not displayed on ECAM):
�� On ground :
ENG MASTER (AFFECTED
ENGINE)........................................................................................OFF
�� In flight :
THR LEVER (AFFECTED
ENGINE)...........................................................................................IDLE
ENG PARAMETERS (AFFECTED
ENGINE).........................................................................CHECK
�� 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
The ECAM’s VIB advisory (N1 ≥6 units, N2 ≥4.3 units) is mainly a guideline to
induce the crew to monitor
engine parameters more closely
VIB detection alone does not require engine shutdown.
Note: 1. High engine vibrations may be accompanied by cockpit and cabin smoke,
and/or the smell
of burning. This may be due only to compressor blade tip contact with associated
abradable
seals.
2. High N1 vibrations are generally accompanied by perceivable airframe vibrations.
High N2 vibrations can occur without perceivable airframe vibrations.
�� If no icing conditions :
ENG
PARAMETERS...............................................................................................................
　
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