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AND TURN
Disregard ″USE MAN PITCH TRIM″ on the PFD : The stabilizer is frozen due to
insufficient
hydraulic power.
�� When L/G downlocked
L/G
lever..........................................................................................................................DO
WN
APPROACH SPEED.....................................................................................................
ADJUST
Adjust the speed to the above given Vapp. Nevertheless, to reach the landing
field/runway,
the approach speed may be adjusted up to 200 kt (max speed with slats extended).
GND
SPLR...............................................................................................................................
ARM
MAX BRK
PR..................................................................................................................... 1000 PSI
AT 2 000 FT AGL
CABIN................................................................................................................NOTIF
Y FOR LANDING
AT 500 FT AGL
BRACE FOR
IMPACT.................................................................................................................ORD
ER
AT TOUCHDOWN
ENG
MASTERS.......................................................................................................................
........ OFF
APU MASTER
SW............................................................................................................................OFF
BRAKES ON ACCU ONLY
AFTER LANDING
�� When the aircraft has stopped:
PARKING
BRK............................................................................................................................
ON
ATC.................................................................................................................................
.... NOTIFY
FIRE pushbutton (ENG and
APU)...........................................................................................PUSH
AGENTS (ENG and
APU)......................................................................................................DISCH
Engine Agent 2 is not available.
�� If Evacuation required:
EVACUATION...............................................................................................................
INITIATE
ELT �� ....................................................................................................... CHECK
EMITTING
If not, switch on the transmitter.
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA).......................................................................NOTIFY
To be continued on next page
ABN-70
4/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , ,
ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT
ATTEMPT (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.......................................................................................................................
　
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