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LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A318/A319/A320/A321 FLEET LIM-22-20 P 4/8
FCOM 19 AUG 10
Tailwind : 10 kt
Crosswind : 20 kt
Note: Wind limitation is based on the surface wind reported by the tower. If the wind displayed
on ND exceeds the above-noted autoland limitations, but the tower reports a surface
wind within the limitations, then the autopilot can remain engaged. If the tower reports a
surface wind beyond limitations, only CAT II automatic approach without autoland can be
performed provided wind conditions are within the limitations quoted on FCOM 3.01.22
page 3. Otherwise, only CAT I automatic approach without autoland can be performed.
MAXIMUM WIND CONDITIONS FOR CAT III AUTOMATIC APPROACH
OR AUTOMATIC LANDING AND AUTOMATIC ROLL OUT
Applicable to: ,
, MSN,,
Headwind : 30 kt
Tailwind : 10 kt
Crosswind : 20 kt
Note: Wind limitation is based on the surface wind reported by ATC. If the wind displayed on
the ND exceeds the above-noted autoland limitations, but the tower reports surface
wind within the limitations, then the autopilot can remain engaged. If the tower reports a
surface wind that exceeds the limitations, only CAT II automatic approach without autoland
can be performed provided wind conditions are within the limitations quoted on Refer to
LIM-22-20 CATEGORY II. Otherwise, only CAT I automatic approach without autoland can
be performed.
AUTOMATIC LANDING
Applicable to:
CAT II and CAT III autoland are approved in CONF 3 and CONF FULL.
Automatic landing is demonstrated :
With ‐ CAT II and CAT III ILS beam.
‐ With slope angle within (–2.5 °, –3.15 °) range.
‐ For airport altitude at or below 2 500 ft.
‐ At or below the maximum landing weight.
‐ At approach speed (VAPP) = VLS + wind correction.
Minimum wind correction 5 kt ; maximum windcorrection15 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A318/A319/A320/A321 FLEET LIM-22-20 P 5/8
FCOM 19 AUG 10
Automatic rollout performance has been approved on dry and wet runways, but performance on
snow-covered or icy runways has not been demonstrated.
AUTOMATIC LANDING
Applicable to:
CAT II and CAT III autoland are approved in CONF 3 and CONF FULL.
Automatic landing is demonstrated :
With ‐ CAT II and CAT III ILS beam.
‐ With slope angle within (–2.5 °, –3.15 °) range.
‐ For airport altitude at or below 2 500 ft.
‐ At or below the maximum landing weight.
‐ At approach speed (VAPP) = VLS + 5 kt + wind correction.
Automatic rollout performance has been approved on dry and wet runways, but performance on
snow-covered or icy runways has not been demonstrated.
AUTOMATIC LANDING
Applicable to:
CAT II and CAT III autoland are approved in CONF 3 and CONF FULL.
Automatic landing is demonstrated :
‐ With CAT II and CAT III ILS beam.
‐ With slope angle within (–2.5 °, –3.15 °) range.
‐ For airport altitude at or below 9 200 ft.
‐ At or below the maximum landing weight.
‐ At approach speed (VAPP) = VLS + wind correction.
Minimum wind correction 5 kt, maximum wind correction 15 kt.
Automatic rollout performance has been approved on dry and wet runways, but performance on
snow-covered or icy runways has not been demonstrated.
During automatic rollout with one engine inoperative, the flight crew can use the remaining thrust
reverser, provided that :
‐ Only IDLE reverse thrust is used
‐ The crosswind does not exceed 15 kt.
Note: Under crew responsability and in case of emergency, autoland can be performed up to 69 t
(152 117 lb).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A318/A319/A320/A321 FLEET LIM-22-20 P 6/8
FCOM 19 AUG 10
AUTOMATIC LANDING
Applicable to:
CAT II and CAT III autoland are approved in CONF 3 and CONF FULL.
Automatic landing is demonstrated :
‐ With CAT II and CAT III ILS beam.
‐ With slope angle within (–2.5 °, –3.15 °) range.
‐ For airport altitude at or below 9 200 ft.
‐ At or below the maximum landing weight.
‐ At approach speed (VAPP) = VLS + wind correction.
Minimum wind correction 5 kt, maximum wind correction 15 kt.
Automatic rollout performance has been approved on dry and wet runways, but performance on
snow-covered or icy runways has not been demonstrated.
Note: Under crew responsability and in case of emergency, autoland can be performed up to 69 t
　
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