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ABN-70
1/10
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , MSN,
ENG DUAL FAILURE - FUEL REMAINING - ENGINE RELIGHT
ATTEMPT
As long as none of the engines recover, the flight crew must apply this paper
procedure when required by
the ENG DUAL FAILURE procedure. If time permits, clear ECAM alerts, and check
the ECAM STATUS
page.
LAND ASAP
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.
VHF1/HF1 ��
/ATC1.............................................................................................................................
USE
ATC.................................................................................................................................
...................NOTIFY
�� 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 , , MSN,
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
78 236 246 256
76 232 242 252
72 224 234 244
68 216 226 236
64 208 218 228
60 200 210 220
56 192 202 212
52 184 194 204
48 176 186 196
44 168 178 188
40 160 170 180
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 ; L/G DOWN) will be
approximately 800
feet/NM (with no wind).
BARO..............................................................................................................................
　
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