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.... NOTIFY
FIRE pushbutton (ENG and
APU)...........................................................................................PUSH
AGENTS (ENG and
APU)......................................................................................................DISCH
Engine Agent 2 is not available.
�� If Evacuation required:
EVACUATION...............................................................................................................
INITIATE
ELT �� ....................................................................................................... CHECK
EMITTING
If not, switch on the transmitter.
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA).......................................................................NOTIFY
To be continued on next page
ABN-70
4/10
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 DITCHING 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
ditching (CONF 3 ;
L/G UP)
L/G
lever..........................................................................................................................CHE
CK UP
AT 2 000 FT AGL
CABIN.............................................................................................................. NOTIFY
FOR DITCHING
DITCHING
pushbutton......................................................................................................................
ON
In case of strong crosswind, ditch face to the wind.
In the absence of strong crosswind, prefer ditching parallel to the swell. Touchdown
with
approximately 11 ° of pitch and minimum aircraft vertical speed.
AT 500 FT AGL
BRACE FOR
IMPACT.................................................................................................................ORD
ER
AT TOUCHDOWN
ENG
MASTERS.......................................................................................................................
........ OFF
APU MASTER
SW............................................................................................................................OFF
AFTER DITCHING
ATC (VHF
1).............................................................................................................................
NOTIFY
FIRE pushbutton (ENG and
APU)................................................................................................. PUSH
AGENT (ENG and
APU)...............................................................................................................DISCH
Engine Agent 2 is not available.
EVACUATION................................................................................................................
...........INITIATE
ELT �� ....................................................................................................................
CHECK EMITTING
If not, switch on the transmitter.
ABN-70
5/10
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
The flight crew should apply this paper procedure when required by the ECAM ENG
DUAL FAILURE
procedure. If time permits, clear ECAM alerts, and check the ECAM STATUS page.
OPTIMUM
SPEED.........................................................................................................240
KT/GREEN DOT
Initially, fly 240 kt, because the PFD may not display the correct green dot speed.
Then fly the green dot
speed according to the following table:
GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS)
Weight (1 000 kg) At or below FL 200 FL 300 FL 400
80 230 240 250
78 227 237 247
76 224 234 244
74 221 231 241
72 218 228 238
　
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