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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 70 69 68 67 65 64 62 57
5 70 69 68 67 65 64 60 55
10 70 69 68 67 65 61 57 52
15 70 69 68 66 63 59 54 50
20 70 69 66 64 61 56 52 48
25 70 67 64 62 58 54 50 46
30 67 65 63 60 56 51 47
35 65 62 60 57 53 49
40 62 60 58 54
45 59 57 55
50 56 54
55 53
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 16/22
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 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)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 17/22
FCOM 19 AUG 10
LANDING WITH SLATS OR FLAPS JAMMED
Applicable to:
LANDING CONF.....................................................................................................................CONF 3
�� Repeat the following until landing configuration is reached:
SPEED SEL.......................................................................................................VFE NEXT - 5KT
Decelerate towards VFE NEXT - 5 kt but not below VLS. In case of turbulence, to avoid VFE
exceedance, the pilot may decide to decelerate to a lower speed, but not below VLS.
Note: The autopilot may be used down to 500 ft AGL. As it ‐ is not tuned for abnormal
configurations, its behavior can be less than optimum and must be monitored.
‐ Approach with selected speed is recommended.
‐ A/THR is recommended, except in the case of a G+B SYS LO PR warning.
‐ OVERSPEED warning and VLS, displayed on the PFD, are computed according to
the actual flaps/slats position.
‐ VFE and VFE NEXT are displayed on the PFD according to the FLAPS lever
position. If not displayed, use the placard speeds.
‐ If VLS is greater than VFE NEXT (overweight landing case), the FLAPS lever
can be set in the required next position, while the speed is reduced to follow VLS
reduction as surfaces extend. The VFE warning threshold should not be triggered.
In this case, disconnect the A/THR. A/THR can be re-engaged when the landing
configuration is established.
As speed reduces through VFE NEXT:
FLAPS LEVER................................................................................................ONE STEP DOWN
　
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