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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.........................................................................................................240
KT/GREEN DOT
Initially, fly 240 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
80 230 240 250
78 227 237 247
76 224 234 244
74 221 231 241
72 218 228 238
70 215 225 235
68 212 222 232
66 209 219 229
64 206 216 226
62 203 213 223
60 200 210 220
58 197 207 217
56 194 204 214
54 191 201 211
52 188 198 208
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 1 700 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
CREW OXY MASKS (Above FL
100)........................................................................................................ ON
CABIN AND
COCKPIT....................................................................................................................PR
EPARE
SIGNS.............................................................................................................................
.......................... ON
COMMERCIAL...............................................................................................................
.......................... OFF
USE RUDDER WITH CARE
�� WHEN BELOW FL 150
RAM
AIR..................................................................................................................................
...........ON
COMMON ACTIONS FOR THE APPROACH
APPROACH PREPARATION
Note: Final descent slope, when configured (CONF 3; L/G DOWN), will be
approximately 900
feet/NM (with no wind).
BARO..............................................................................................................................
.................SET
CREW MASKS/OXY SUPPLY (below FL
100)................................................................................ OFF
To be continued on next page
ABN-70
6/10
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 (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 160 160 160 160 163 167 170 174 178 179
�� 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.
　
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