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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 78
Vapp 150 150 150 150 150 155 159 163 167 171 173
�� 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
APU MASTER
SW............................................................................................................................OFF
AFTER DITCHING
ATC (VHF
1).............................................................................................................................
NOTIFY
FIRE pushbutton (ENG and
APU)................................................................................................. PUSH
AGENT (ENG and
APU)...............................................................................................................DISCH
Engine Agent 2 is not available.
EVACUATION................................................................................................................
...........INITIATE
ELT �� ....................................................................................................................
CHECK EMITTING
If not, switch on the transmitter.
ABN-70
5/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
ENG DUAL FAILURE - NO FUEL REMAINING - SECURE CABIN AND
COCKPIT
The flight crew should apply this paper procedure and then, if time permits, clear
ECAM warnings and
check the ECAM STATUS page.
THRUST
LEVERS..........................................................................................................................
........IDLE
FAC
1....................................................................................................................................
OFF THEN ON
Resetting FAC 1 also enables rudder trim recovery, even if no indication is available.
OPTIMUM
SPEED.........................................................................................................220
KT/GREEN DOT
Initially, fly 220 kt, because the PFD may not display the correct green dot speed.
Then fly the green dot
speed according to the following table:
GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)
Weight (1 000 kg) At or below FL 200 FL 300 FL 400
68 221 231 241
64 213 223 233
60 205 215 225
56 197 207 217
52 189 199 209
48 181 191 201
44 173 183 193
40 165 175 185
At green dot speed, the aircraft can fly up to approximately 2.5 nm per 1 000 ft (with
no wind). Average rate
of descent is approximately 1 600 ft/min .
LANDING
STRATEGY................................................................................................................DE
TERMINE
Determine whether a runway can be reached or the most appropriate place for a
forced landing/ditching.
EMER ELEC POWER (if EMER GEN not in
line)............................................................................ MAN ON
VHF1/HF1 ��
/ATC1.............................................................................................................................
USE
ATC.................................................................................................................................
...................NOTIFY
　
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