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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 74 72 69 67 64 62 59 55
5 74 72 69 67 64 62 58 53
10 74 72 69 67 64 59 55 50
15 74 72 69 66 61 57 52 48
20 74 72 68 63 59 54 50 46
25 74 70 66 61 56 52 48 43
30 72 68 63 58 54 49 45
35 71 66 61 56 52 48
40 68 63 59 54
45 66 61 56
50 63 58
55 61
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 13/22
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 75 75 73 70 67 63 60 55
5 75 75 73 70 67 63 58 55
10 75 75 73 70 66 61 56 55
15 75 75 73 69 63 58 53 53
20 75 75 71 66 61 57 51 51
25 75 74 68 64 60 55 50 45
30 75 71 67 62 58 53 48
35 73 69 65 60 56 51
40 70 66 62 58
45 68 64 60
50 66 62
55 63
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 14/22
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 65 64 63 62 62 62 60 57
5 65 64 63 62 62 62 59 55
10 65 64 63 62 61 60 57 52
15 65 64 63 61 59 58 55 50
20 65 64 62 59 57 55 52 48
25 65 62 60 58 55 53 50 46
30 63 60 58 56 53 50 47
35 60 58 56 53 50 48
40 59 56 54 51
45 56 54 51
50 53 51
55 50
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 15/22
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
　
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