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‐ Pull C/B K10 on 121VU.
‐ 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
31/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN 4566
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
32/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
Intentionally left blank
A318/A319/A320/A321 FLEET MSN 4566
ABN-80
1/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET MSN 4617
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 76 74 71 68 64 61 58 54
5 76 74 71 68 64 61 56 52
10 76 74 71 68 64 59 54
15 76 74 71 67 61 57 52
20 76 74 69 64 59 54
25 76 71 66 61 56
30 73 68 63 58 53
35 69 64 60 55
40 65 61 57 52
45 61 57 53
50 57 54
55 54
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
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK9(81)
