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time)...................................................................................OFF 30 S/ON
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ABN-70
2/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT
ATTEMPT (Cont'd)
�� When APU bleed is available or if engine restart is definitively considered
impossible:
OPTIMUM SPEED........................................................................................REFER
TO TABLE BELOW
GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)
Weight (1 000 kg) At or below FL 200 FL 300 FL 400
94 251 261 271
92 248 258 268
88 242 252 262
86 239 249 259
84 236 246 256
82 233 243 253
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 1 600 ft/min.
CABIN AND
COCKPIT.............................................................................................................PREP
ARE
CABIN
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 and 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
3/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET ,
ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT
ATTEMPT (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
Disregard ″USE MAN PITCH TRIM″ on the PFD : The stabilizer is frozen due to
insufficient
hydraulic power.
�� When L/G downlocked
L/G
lever..........................................................................................................................DO
WN
APPROACH SPEED.....................................................................................................
ADJUST
Adjust the speed to the above given 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
　
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