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FOR DITCHING
DITCHING
pushbutton......................................................................................................................
ON
In case of strong crosswind, ditch face to the wind.
In the absence of strong crosswind, prefer ditching parallel to the swell. Touchdown
with
approximately 11 ° of pitch and minimum aircraft vertical speed.
AT 500 FT AGL
BRACE FOR
IMPACT.................................................................................................................ORD
ER
AT TOUCHDOWN
ENG
MASTERS.......................................................................................................................
........ OFF
AFTER DITCHING
ATC (VHF
1).............................................................................................................................
NOTIFY
EVACUATION................................................................................................................
...........INITIATE
ELT �� ....................................................................................................................
CHECK EMITTING
If not, switch on the transmitter
ABN-70
8/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , ,
ENG RELIGHT
(IN FLIGHT)
MAX
ALTITUDE......................................................................................................................
....... See below
ENG MASTER
(affected)........................................................................................................................
OFF
THR LEVER
(affected).........................................................................................................................
..IDLE
ENG MODE
SEL..................................................................................................................................
... IGN
XB
LEED ............................................................................................................................
..................OPEN
WING A. ICE (for starter
assist)...............................................................................................................OFF
ENG MASTER
(affected).........................................................................................................................
.ON
Be aware that, contrary to an autostart on ground, the crew must take appropriate
action in case of an
abnormal start.
Engine light up must be achieved within 30 s after fuel flow increases.
ENG PARAMETERS (N2,
EGT)......................................................................................................... CHECK
If the START FAULT ENG STALL warning is triggered, although engine parameters
are normal, disregard
the warning.
�� When idle is reached :
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
�� 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
　
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