曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

(152 117 lb).
AUTOMATIC LANDING
Applicable to: MSN,
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 5 750 ft.
‐ At or below the maximum landing weight.
‐ At approach speed (VAPP) = VLS + wind correction.
Minimum wind correction 5 kt ; maximum windcorrection15 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.
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 7/8
FCOM 19 AUG 10
AUTOMATIC LANDING
Applicable to: ,
, MSN
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.
Automatic landing is not allowed below-1 000 ft pressure altitude.
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.
AUTOMATIC LANDING
Applicable to: MSN,
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.
‐ At or below the maximum landing weight.
‐ For airport altitude at or below 6 500 ft
‐ 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.
AUTOMATIC LANDING
Applicable to:
CAT II and CAT III autoland are approved in CONF 3 and CONF FULL.
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 8/8
FCOM 19 AUG 10
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.
Automatic landing is not allowed below-1 000 ft pressure altitude.
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 IN CAT I OR BETTER WEATHER CONDITIONS
Applicable to: ALL
The automatic landing system’s performance has been demonstrated on runways equipped with
CAT II or CAT III ILS/MLS approaches. However, automatic landing in CAT I or better weather
conditions is possible on CAT I ground installations or on CAT II/III ground installations when
ILS/MLS sensitive areas are not protected, if the following precautions are taken :
The airline has checked that the ILS/MLS beam quality, ‐ and the effect of terrain profile before
the runway have no adverse effect on AP/FD guidance. In particular, the effect of terrain
discontinuities within 300 m before runway threshold must be evaluated.
‐ The crew is aware that LOC or GS beam fluctuations, independent of the aircraft systems, may
occur and the PF is prepared to immediately disconnect the AP and take appropriate action,
should unsatisfactory guidance occur.
‐ At least CAT2 capability is displayed on the FMA, and CAT II/III procedures are used.
‐ Visual references are obtained at an altitude appropriate to the performed CAT I approach,
otherwise go–around is initiated.
LIMITATIONS
ELECTRICAL
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