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PRESSURIZATION
A318/A319/A320/A321 FLEET LIM-21-21_20 P 2/2
FCOM 19 AUG 10
Note: Max ◂p and safety valve setting tolerance = ± 7 hPa (0.1 PSI)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
VENTILATION
A318/A319/A320/A321 FLEET LIM-21-21_30 P 1/2
FCOM 19 AUG 10
AVIONICS VENTILATION
Applicable to: ALL
During ground operations, limit the aircraft electric power supply with avionics ventilation system in
normal configuration as follows :
OAT = 49 °C no limitation
OAT = 55 °C time limit 2 h
OAT = 60 °C time limit 1 h
OAT = 64 °C time limit 1/2 h
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AIR CONDITIONING / PRESSURIZATION / VENTILATION
VENTILATION
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A318/A319/A320/A321 FLEET LIM-21-21_30 P 2/2
FCOM 19 AUG 10
LIMITATIONS
AUTO FLIGHT
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A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 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................................................................................................................................... 1/6
AUTOTHRUST FUNCTION................................................................................................................................ 2/6
FLIGHT MANAGEMENT FUNCTION...................................................................................................................3/6
TAKEOFF IN GPS PRIMARY.............................................................................................................................5/6
USE OF NAV AND FINAL APP MODES FOR NON-PRECISION APPROACH..................................................5/6
NON-PRECISION APPROACHES WITH ENGINE-OUT..................................................................................... 6/6
LIM-22-20 AUTOMATIC APPROACH, LANDING AND ROLL OUT
CATEGORY II..................................................................................................................................................... 1/8
CATEGORY III FAIL PASSIVE (SINGLE)............................................................................................................1/8
CATEGORY III FAIL OPERATIONAL (DUAL)..................................................................................................... 1/8
CATEGORY III FAIL OPERATIONAL.................................................................................................................. 2/8
CATEGORY III FAIL OPERATIONAL (DUAL)..................................................................................................... 3/8
ENGINE OUT......................................................................................................................................................3/8
MAXIMUM WIND CONDITIONS FOR CAT II OR CAT III AUTOMATIC APPROACH LANDING AND ROLL OUT.3/8
MAXIMUM WIND CONDITIONS FOR CAT III AUTOMATIC APPROACH OR AUTOMATIC LANDING AND
AUTOMATIC ROLL OUT....................................................................................................................................4/8
AUTOMATIC LANDING...................................................................................................................................... 4/8
AUTOMATIC LANDING IN CAT I OR BETTER WEATHER CONDITIONS.........................................................8/8
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
PRELIMINARY PAGES - TABLE OF CONTENTS
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A318/A319/A320/A321 FLEET LIM-22-PLP-TOC P 2/2
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
LIMITATIONS
AUTO FLIGHT
GENERAL
A318/A319/A320/A321 FLEET LIM-22-10 P 1/6
FCOM 19 AUG 10
AUTO PILOT FUNCTION
Applicable to:
Minimum height for use of 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
　
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