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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.
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.
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 FEET AGL
CABIN................................................................................................................NOTIF
Y FOR LANDING
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