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(geodesic standard used by GPS, FMS) is not negligible, an incorrect NAV guidance may occur
after takeoff.
When departing from these airports, GPS must be deselected for takeoff from these airports, until
a safe altitude is reached.
USE OF NAV AND FINAL APP MODES FOR NON-PRECISION APPROACH
Applicable to: ALL
NAV, or NAV and FINAL APP mode may be used for VOR, VOR/DME, NDB, NDB/DME or RNAV
(including GPS) approach, but not for ILS, LOC, LOC-BC, LDA, SDF, or MLS final approach.
For instrument procedures not coded in the WGS 84 coordinate system, the GPS must be
deselected, unless the shift between the local coordinate system and the WGS 84 is found
acceptable for the intended operation.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
GENERAL
A330/A340 FLEET LIM-22-10 P 4/4
FCOM 19 AUG 10
Note: 1. The assesment of this shift can be done :
in flight, monitoring the navaid raw data ‐ in non RNAV procedures,
‐ on ground performing a GPS survey of the procedure waypoint.
2. RNAV (GPS) and RNP RNAV approach procedures require WGS 84 coordinates and
GPS.
FINAL APP mode guidance capability with GPS PRIMARY has been demonstrated down to
MDH/DH (barometric) 250 ft .
VOR, VOR/DME, NDB or NDB/DME approach procedures may be performed, in NAV, or NAV and
FINAL APP mode, provided AP or FD is used, and :
‐ GPS PRIMARY is available. In this case, the reference navaid may be unserviceable, or the
airborne radio equipment may be inoperative, or not installed, provided operational approval is
obtained.
‐ Without GPS PRIMARY :
• The reference navaid and the corresponding airborne equipment is serviceable, tuned, and
monitored during the approach, or
• The radio navaid coverage supports the RNP value, specified for the approach procedure, and
an operational approval is obtained.
For GPS approach, GPS PRIMARY must be available.
RNAV approach without GPS PRIMARY may be performed only if the radio navaid coverage
supports the RNP value and HIGH accuracy is displayed on the MCDU with the specified RNP, and
operational approval is obtained.
NAV mode may be used in the terminal area, provided :
‐ GPS PRIMARY is available, or
‐ HIGH accuracy is displayed, and the appropriate RNP is checked or entered on the MCDU, or
‐ Navaid raw data is monitored.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A330/A340 FLEET LIM-22-20 P 1/4
FCOM 19 AUG 10
CATEGORY II
Applicable to: ALL
Minimum decision height...................................................................................................... 100 ft AGL
At least one autopilot must be engaged in APPR mode and CAT 2, CAT 3 SINGLE or CAT 3 DUAL
must be displayed on the FMA.
CATEGORY III FAIL PASSIVE
Applicable to: ALL
Minimum decision height.................................................................................................................50 ft
At least one autopilot must be engaged in APPR mode and CAT 3 SINGLE or CAT 3 DUAL must be
displayed on the FMA.
A/THR must be used in selected or managed speed.
CATEGORY III FAIL OPERATIONAL
Applicable to: ALL
A/THR must be used in selected or managed speed.
Alert height.................................................................................................................................. 200 ft
‐ CAT III with DH :
2 autopilots must be engaged in APPR mode and CAT 3 DUAL must be displayed on the FMA
‐ CAT III without DH :
2 autopilots must be engaged in APPR mode and CAT 3 DUAL must be displayed on the FMA
Minimum Runway Visual Range................................................................................................ 75 m
ENGINE OUT
Applicable to:
CAT II and CAT III autoland are only approved in Configuration 3 if engine out procedures are
completed before reaching 1 000 ft in approach. CAT III fail passive autoland is approved in single
inner engine out, CAT III fail operational autoland in single outer engine out.
ENGINE OUT
Applicable to: ,
CAT II and CAT III autoland are only approved in Configuration 3 if engine out procedures are
completed before reaching 1 000 ft in approach.
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
AUTOMATIC APPROACH, LANDING AND ROLL OUT
A330/A340 FLEET LIM-22-20 P 2/4
FCOM 19 AUG 10
MAXIMUM WIND CONDITIONS FOR CAT II/CAT III ATOMATIC
APPROACH, OR AUTOMATIC LANDING AND AUTOMATIC ROLL OUT
Applicable to: ALL
Headwind : 35 kt
Tailwind :10 kt
Crosswind : 20 kt
Note: Wind limitation is based on the surface wind reported by the tower. If the wind displayed on
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 5(33)
