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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
EMERGENCY EVACUATION
AIRCRAFT/PARKING
BRK..............................................................................................................STOP/ON
ATC (VHF
1).....................................................................................................................................
NOTIFY
CABIN CREW
(PA)............................................................................................................................
ALERT
ΔP (only if MAN CAB PR has been
used)...............................................................................CHECK ZERO
If not zero, MODE selector on MAN, V/S CTL FULL UP.
ENG MASTERS
(ALL)............................................................................................................................O
FF
FIRE Pushbuttons (ALL : ENG and
APU)............................................................................................. PUSH
AGENTS (ENG and
APU)...............................................................................................................AS RQRD
�� If Evacuation required:
EVACUATION................................................................................................................
............ INITIATE
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA)..................................................................................... NOTIFY
ABN-80
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , ,
CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE
LANDING
WEIGHT.........................................................................................................................
...CHECK
�� if the aircraft weight is above the maximum weight for circling in CONF 3 (given
in the table
below):
The aircraft cannot maintain flight level with CONF 3 and the landing gear down.
FOR
LDG............................................................................................................................US
E FLAP 3
CONF 3 is preferred, to minimize a configuration change in short final.
GPWS LDG FLAP
3............................................................................................................................ ON
Delay gear extension.
Note: If the approach is flown at less than ‐ 750 ft RA, the “L/G NOT DOWN”
warning will be
triggered. The pilot can cancel the aural warning by pressing the EMER CANC pb,
located
on the ECAM control panel.
A ”TOO LOW GEAR” ‐ warning is to be expected, if the landing gear is not
downlocked at
500 ft RA.
OAT AIRPORT ELEVATION (feet)
(°C) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000
0 86.0 82.0 78.0 75.0 71.0 67.0 63.0 59.0
5 86.0 82.0 78.0 75.0 71.0 67.0 63.0 59.0
10 86.0 82.0 78.0 75.0 70.0 65.0 60.0
15 86.0 82.0 78.0 74.0 68.0 63.0
20 86.0 82.0 76.0 71.0 65.0 60.0
25 86.0 79.0 73.0 68.0 62.0
30 82.0 76.0 70.0 65.0 60.0
35 79.0 72.0 67.0 62.0
40 .740 69.0 64.0 59.0
45 72.0 66.0 61.0
50 68.0 63.0
55 65.0
MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 KG)
STRAIGHT-IN-APPROACH WITH ONE ENGINE INOPERATIVE
For performance reasons, do not extend flaps full until established on a final descent
to landing.
If a level off is expected during the final approach, perform the approach and landing
in CONF 3.
ABN-80
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AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , , , , , , ,
, , , , , , , , , , ,
BOMB ON BOARD
IF POSSIBLE, LAND AND EVACUATE THE AIRCRAFT IMMEDIATELY.
If it is not possible to land and evacuate the aircraft within 30 min, apply the
following procedures :
COCKPIT PROCEDURES
BACKGROUND
To avoid the activation of an altitude-sensitive bomb, the cabin altitude should not
exceed the value at
which the bomb has been discovered.
To reduce the effects of the explosion, the aircraft should fly as long as possible with
approximately
1 PSI differential pressure, to help the blast go outwards. 1 PSI differential pressure
corresponds to a
2 500 ft difference between the aircraft and the cabin altitude.
These conditions are achieved by using the manual pressure control.
PROCEDURE
The following procedure assumes that it is initiated during climb or cruise :
　
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