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ENG DUAL FAILURE - NO FUEL REMAINING - SECURE CABIN AND
COCKPIT (Cont'd)
IF FORCED LANDING ANTICIPATED
APPROACH
FOR
LDG............................................................................................................................US
E FLAP 3
Only slats extend, and slowly.
MIN APPR
SPEED.......................................................................................................................160
KT
VAPP...............................................................................................................................
.. DETERMINE
Vapp is the maximum between VREF + 30 kt/160 kt.
Weight (1 000 kg) 52 56 60 64 68 72 76 80 84 86
Vapp 160 160 160 160 163 167 171 174 178 180
�� At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for
landing (CONF 3 ;
L/G DOWN)
�� When in CONF 3 and VAPP
GRAVITY GEAR EXTN handcrank................................................................PULL
AND TURN
Flight controls revert to direct law at landing gear extension. Wait for CONF 3 and
VAPP
before extending the landing gear to enable the aircraft to be trimmed for approach.
Disregard
″USE MAN PITCH TRIM″ on the PFD, because the stabilizer is frozen in the position
where it
was at, when the windmilling was insufficient to provide hydraulic power.
�� When L/G downlocked
L/G
lever..........................................................................................................................DO
WN
APPROACH SPEED.....................................................................................................
ADJUST
Adjust the speed to the determined Vapp. Nevertheless, to reach the landing
field/runway, the
approach speed may be adjusted up to 215 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
BRAKES ON ACCU ONLY
AFTER LANDING
�� When the aircraft has stopped :
PARKING
BRK............................................................................................................................
ON
ATC.................................................................................................................................
.... NOTIFY
�� If Evacuation required :
EVACUATION...............................................................................................................
INITIATE
ELT �� ....................................................................................................... CHECK
EMITTING
If not, switch on the transmitter
�� If Evacuation not required :
CABIN CREW and PASSENGERS
(PA).......................................................................NOTIFY
ABN-70
4/6
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...............................................................................................................................
　
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