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OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 9/22
FCOM 19 AUG 10
IMMEDIATE VMC LDG FOLLOWING ENG FAILURE ON TO
Applicable to: ALL
STRAIGHT-IN APPROACH WITH ONE ENGINE INOPERATIVE
Applicable to: ALL
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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 10/22
FCOM 19 AUG 10
CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE
Applicable to: ,
, MSN
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.................................................................................................................. USE 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 82 78 75 71 67 63 59
5 86 82 78 75 71 67 62
10 86 82 78 75 70 65 60
15 86 82 78 74 68 63
20 86 82 76 71 65 60
25 86 79 73 68 62
30 82 76 70 65 60
35 79 72 67 62
40 74 69 64 59
45 72 66 61
50 68 63
55 65
MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 KG)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 11/22
FCOM 19 AUG 10
CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE
Applicable to:
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.................................................................................................................. USE 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 77 76 69 63 58 53 48 45
5 77 76 69 63 58 53 48 45
10 77 76 69 63 58 53 48 45
15 77 76 69 63 58 53 48 45
20 77 76 69 63 58 53 48 45
25 77 75 69 63 58 53 48 45
30 77 72 68 63 58 53 48
35 74 70 66 63 56 51
40 71 67 63 59
45 69 65 61
50 67 63
55 64
MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 KG)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 12/22
FCOM 19 AUG 10
CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE
Applicable to:
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.................................................................................................................. USE FLAP 3
CONF 3 is preferred, to minimize a configuration change in short final.
GPWS LDG FLAP 3.................................................................................................................ON
　
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