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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
78 241 251 261
76 237 247 257
72 229 239 249
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.
CABIN AND
COCKPIT.............................................................................................................PREP
ARE
CABIN
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
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.......................................................................................................................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
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 200 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
ER
AT TOUCHDOWN
ENG
MASTERS.......................................................................................................................
........ OFF
APU MASTER
SW............................................................................................................................OFF
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK4(27)
