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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 surface
wind beyond the limitations, only a CAT I automatic approach without autoland can be
performed.
AUTOMATIC LANDING
Applicable to:
CAT II and CAT III autoland is approved in CONF 3 and CONF FULL.
Automatic landing has been demonstrated :
‐ On CAT II and CAT III ILS beam,
‐ With ILS slope angle inside a range of (–2.5 °, –3.15 °),
‐ For airfield elevation lower than 9 200 ft .
‐ For weights below maximum landing weight.
‐ at approach speed (VAPP) = VLS + wind correction
minimum wind correction = 5 kt
maximum wind correction = 15 kt
Automatic roll out performance has been approved on dry and wet runways, but performance on
snow covered or icy runway has not been demonstrated.
Automatic landing system performance has been demonstrated on CAT II and CAT III ILS beams.
However, automatic landing in CAT I, or better, weather conditions is possible on CAT I ground
installation or on CAT II/III ground installations when ILS-sensitive areas are not protected, if the
following precautions are taken :
The airline has checked that the ILS beam quality and the effect ‐ of the terrain profile before
the runway have no adverse effect on autopilot guidance. In particular the effect of terrain
discontinuities within 300 m before the runway threshold must be evaluated.
‐ The crew is aware that LOC or GS beam fluctuations, independent of the aircraft system, may
occur and the PF is prepared to immediately disconnect the autopilot and to take the appropriate
action should unsatisfactory guidance occur.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A330/A340 FLEET LIM-22-20 P 3/4
FCOM 19 AUG 10
‐ At least CAT 2 capability is displayed on the FMA and CAT II/III procedures are used.
‐ Visual references are obtained, at a DH appropriate for the CAT I approach being flown, or a
go-around is performed.
Note: Under crew responsibility and in case of emergency, autoland can be performed up to 270 t
(595 242 lb).
AUTOMATIC LANDING
Applicable to: ,
CAT II and CAT III autoland is approved in CONF 3 and CONF FULL.
Automatic landing has been demonstrated :
‐ On CAT II and CAT III ILS beam,
‐ With ILS slope angle inside a range of (–2.5 °, –3.15 °),
‐ For airfield elevation lower than 9 200 ft .
‐ For weights below maximum landing weight.
‐ at approach speed (VAPP) = VLS + wind correction
minimum wind correction = 5 kt
maximum wind correction = 15 kt
Automatic roll out performance has been approved on dry and wet runways, but performance on
snow covered or icy runway has not been demonstrated.
Automatic landing system performance has been demonstrated on CAT II and CAT III ILS beams.
However, automatic landing in CAT I, or better, weather conditions is possible on CAT I ground
installation or on CAT II/III ground installations when ILS-sensitive areas are not protected, if the
following precautions are taken :
‐ The airline has checked that the ILS beam quality and the effect of the terrain profile before
the runway have no adverse effect on autopilot guidance. In particular the effect of terrain
discontinuities within 300 m before the runway threshold must be evaluated.
‐ The crew is aware that LOC or GS beam fluctuations, independent of the aircraft system, may
occur and the PF is prepared to immediately disconnect the autopilot and to take the appropriate
action should unsatisfactory guidance occur.
‐ At least CAT 2 capability is displayed on the FMA and CAT II/III procedures are used.
Visual references are obtained, at a DH appropriate for the ‐ CAT I approach being flown, or a
go-around is performed.
Note: Under crew responsibility and in case of emergency, autoland can be performed up to 229 t
(504 853 lb).
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
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A330/A340 FLEET LIM-22-20 P 4/4
FCOM 19 AUG 10
LIMITATIONS
COMMUNICATIONS
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A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
COMMUNICATIONS
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET LIM-23-PLP-TOC P 1/2
FCOM 19 AUG 10
LIM-23-PLP PRELIMINARY PAGES
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VHF3 TUNING IN VOICE MODE FROM THE MCDU.........................................................................................1/2
　
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