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Note: Maximum differential pressure and safety valve setting tolerance = ± 7 hPa
(0.1 PSI).
CABIN PRESSURE
Applicable to: ,
Maximum positive differential pressure.................................................................................... 9.25 PSI
Maximum negative differential pressure.......................................................................................-1 PSI
Safety relief valve setting.............................................................................................8.85 PSI /-1 PSI
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
PRESSURIZATION
A330/A340 FLEET LIM-21_20 P 2/2
FCOM 19 AUG 10
Note: Maximum differential pressure and safety valve setting tolerance = ± 7 hPa
(0.1 PSI).
LIMITATIONS
AUTO FLIGHT
Intentionally left blank
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET LIM-22-PLP-TOC P 1/2
FCOM 19 AUG 10
LIM-22-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
LIM-22-10 GENERAL
AUTO PILOT FUNCTION................................................................................................................................... 1/4
AUTOTHRUST FUNCTION................................................................................................................................ 1/4
FLIGHT MANAGEMENT FUNCTION...................................................................................................................2/4
USE OF NAV AND FINAL APP MODES FOR NON-PRECISION APPROACH..................................................3/4
LIM-22-20 AUTOMATIC APPROACH, LANDING AND ROLL OUT
CATEGORY II..................................................................................................................................................... 1/4
CATEGORY III FAIL PASSIVE...........................................................................................................................1/4
CATEGORY III FAIL OPERATIONAL.................................................................................................................. 1/4
ENGINE OUT......................................................................................................................................................1/4
MAXIMUM WIND CONDITIONS FOR CAT II/CAT III ATOMATIC APPROACH, OR AUTOMATIC LANDING AND
AUTOMATIC ROLL OUT....................................................................................................................................2/4
AUTOMATIC LANDING...................................................................................................................................... 2/4
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
PRELIMINARY PAGES - TABLE OF CONTENTS
Intentionally left blank
A330/A340 FLEET LIM-22-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
GENERAL
A330/A340 FLEET LIM-22-10 P 1/4
FCOM 19 AUG 10
AUTO PILOT FUNCTION
Applicable to: ,
Minimum height for use of the autopilot on takeoff with SRS mode..................................... 100 ft AGL
(An internal FMGS logic prevents the autopilot from engaging during the 5 s after liftoff).
Minimum height for use of the autopilot in :
Straight-in non precision approach....................................................................applicable MDA (MDH)
Circling approach................................................................. applicable MDA - 100 ft (or MDH - 100 ft)
ILS approach with CAT 1 displayed on FMA ...................................................................... 160 ft AGL
Go-around (AP or FD engagement) .................................................................................... 100 ft AGL
All other phases.................................................................................................................... 500 ft AGL
Use of the AP or FD in OPEN DES or DES mode is not permitted in approach, unless the FCU
altitude is set to, or above, MDA (MDH) or 500 ft, whichever is the highest.
AUTO PILOT FUNCTION
Applicable to: ,
Minimum weight for use of autoland.................................................................................... 123 000 kg
Minimum height for use of the autopilot on takeoff with SRS mode..................................... 100 ft AGL
(An internal FMGS logic prevents the autopilot from engaging during the 5 s after liftoff).
Minimum height for use of the autopilot in :
Straight-in non precision approach....................................................................applicable MDA (MDH)
　
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