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flight, and if
possible, shut down the engine after landing, for taxiing.
ABN-70
1/10
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
As long as none of the engines recover, the flight crew should apply this paper
procedure and then, if time
permits, clear ECAM alerts and check the ECAM. STATUS page.
LAND ASAP
ENG MODE
SEL..................................................................................................................................
... IGN
THRUST
LEVERS..........................................................................................................................
........IDLE
OPTIMUM RELIGHT
SPD................................................................................................................... 280 KT
Note: In the case of an ″ENG DUAL FAILURE″ during high power operations (i.e.
climb, cruise), it is
mandatory to fly at or above the optimum relight speed in order to prevent engine
core lock.
In the case of a speed indication failure (volcanic ash), Pitch attitude for optimum
relight speed is:
WEIGHT Pitch (°)
At or below 50 000 kg/110 000 lb -2.5
60 000 kg/132 000 lb -1.5
70 000 kg/154 000 lb -0.5
At 280 kt, the aircraft can fly up to about 2.2 nm per 1 000 ft (with no wind).
LANDING
STRATEGY................................................................................................................DE
TERMINE
Determine whether a runway can be reached, or the most appropriate place for a
forced landing/ditching.
EMER ELEC
PWR............................................................................................................................
MAN ON
VHF1/HF1 ��
/ATC1.............................................................................................................................
USE
ATC.................................................................................................................................
...................NOTIFY
FAC
1....................................................................................................................................
OFF THEN ON
Resetting FAC 1 also enables rudder trim recovery, even if no indication is available.
�� IF NO RELIGHT AFTER 30 SEC:
ENG
MASTERS..................................................................................................................
OFF 30 S/ON
Unassisted start attempts can be repeated until successful, or until APU bleed is
available.
�� IF UNSUCCESSFUL:
CREW OXY MASKS (Above FL
100)..................................................................................................ON
�� WHEN BELOW FL 250
APU (IF
AVAIL).......................................................................................................................
START
�� WHEN BELOW FL 200
WING ANTI
ICE...........................................................................................................................OFF
APU
BLEED............................................................................................................................
.....ON
ENG MASTERS (one at a
time)...................................................................................OFF 30 S/ON
To be continued on next page
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.............................................................................................................................
　
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