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effect on any of the MCDU ATSU DATALINK submenus.
On ground, or in flight:
‐ Pull the C/Bs in the following order:
L16, L15 on 121VU
‐ Wait 5 s , then:.
‐ Push the C/Bs in the following order:
L15, L16.
70 ENG IGN A+B FAULT FADEC and EIU Refer to FCOM/PRO-ABN-70-K ENG
1(2) IGN
FAULT (IGN A + B Fault) if applicable.
To be continued on next page
ABN-80
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A318/A319/A320/A321 FLEET
Continued from previous page
ENG 1(2) FADEC
A(B) FAULT
FADEC Refer to FCOM/PRO-ABN-70 ENG 1(2) FADEC
A(B) FAULT if applicable.
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
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Intentionally left blank
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ABN-80
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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 75.0 75.0 73.0 70.0 67.0 63.0 60.0 55.0
5 75.0 75.0 73.0 70.0 67.0 63.0 58.0 55.0
10 75.0 75.0 73.0 70.0 66.0 61.0 56.0 55.0
15 75.0 75.0 73.0 69.0 63.0 58.0 53.0 53.0
20 75.0 75.0 71.0 66.0 61.0 57.0 51.0 51.0
25 75.0 74.0 68.0 64.0 60.0 55.0 50.0 45.0
30 75.0 71.0 67.0 62.0 58.0 53.0 48.0
35 73.0 69.0 65.0 60.0 56.0 51.0
40 70.0 66.0 62.0 58.0
45 68.0 64.0 60.0
50 66.0 62.0
55 63.0
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.
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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
　
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