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OFF THEN ON
Resetting FAC 1 also enables rudder trim recovery, even if no indication is available.
OPTIMUM
SPEED.........................................................................................................215
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
CREW OXY MASKS (Above FL
100)........................................................................................................ ON
CABIN AND
COCKPIT....................................................................................................................PR
EPARE
SIGNS.............................................................................................................................
.......................... ON
GALY &
CAB.................................................................................................................................
..........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 800
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.......................................................................................................................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
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
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