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ABN-70
7/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , MSN,
ENG DUAL FAILURE - NO FUEL REMAINING - SECURE CABIN AND
COCKPIT (Cont'd)
IF DITCHING ANTICIPATED
APPROACH
FOR
LDG............................................................................................................................US
E FLAP 3
Only slats extend, and slowly.
MIN APPR
SPEED.......................................................................................................................150
KT
VAPP...............................................................................................................................
.. DETERMINE
Vapp is the maximum between VREF + 25 kt/150 kt:
Weight (1 000 kg) 40 44 48 52 56 60 64 68 72 76
Vapp 150 150 150 150 150 151 155 159 163 167
�� At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for
ditching (CONF 3 ;
L/G UP)
L/G
lever..........................................................................................................................CHE
CK UP
AT 2 000 FT AGL
CABIN.............................................................................................................. NOTIFY
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 , , MSN,
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.
�� 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............................................................................................................................
　
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