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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 , , MSN,
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 , , MSN,
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.
High N1 or N2 vibrations in operation :
The ECAM’s VIB advisory (N1 > 5 units, N2 > 5 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
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK4(89)
