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�� 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...............................................................................................................
......CHECK
Check engine parameters and especially EGT ; crosscheck with the other engine.
Report in the
maintenance log.
�� If rapid increase above the advisory :
THRUST LEVER (affected
engine)......................................................................................RETARD
Flight conditions permitting, reduce N1 to maintain the vibration level below the
advisory threshold.
Note: If the VIB indication does not decrease following thrust reduction, this may
indicate other
engine problems. Apply the adequate procedure.
�� If icing conditions :
An increase in N1 vibrations in icing conditions, with or without engine anti-ice, may
be due to fan
blades and/or spinner icing.
A/THR.............................................................................................................................
.................. OFF
ENGINE
ANTI-ICE........................................................................................................................
CHECK
If ENG ANTI-ICE is off, switch it ON at idle fan speed, one engine after the other at
an approximate
　
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