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‐ Wait 5 s, then push the C/B.
34
ISIS malfunction ISIS On ground only:
With aircraft not moving:
‐ Pull C/B F12 on 49VU,
‐ Wait 5 s ,then push the C/B,
‐ Normal operation is expected after approximately 2 min.
Note: In the case of small aircraft motion during the C/B reset (refueling,
cargo loading conditions, etc.), the ATT red flag may appear on the ISIS. In
this case, press the RST P/B for 2 s wait 2 min additional to recover normal
operation.
46
ATSU Malfunction ATSU An ATSU reset should be attempted, if: key selection has
no
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.
ENG IGN A+B FAULT FADEC and EIU Refer to FCOM/PRO-ABN-70-K ENG 1(2)
IGN
70 ENG 1(2) FADEC FAULT (IGN A + B Fault) if applicable.
A(B) FAULT
FADEC Refer to FCOM/PRO-ABN-70 ENG 1(2) FADEC
A(B) FAULT if applicable.
ABN-80
32/32
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
1/32
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
　
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