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FLIGHT WITH GEAR DOWN - PERFORMANCE
A330/A340 FLEET PRO-SPO-25-40 P 16/22
FCOM 19 AUG 10
EN ROUTE NET FLIGHT PATH
Applicable to: ,
EN ROUTE NET FLIGHT PATH - L/G DOWN - ONE ENGINE OUT
MAX. CONTINUOUS THRUST ISA Required gradient : 1.1 %
NORMAL AIR CONDITIONING Minimum engine
ANTI-ICING OFF CG = 14 %
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A330/A340 FLEET PRO-SPO-25-40 P 17/22
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A330/A340 FLEET PRO-SPO-25-40 P 18/22
FCOM 19 AUG 10
GROSS CEILINGS AT LONG RANGE AND GREEN DOT SPEEDS - ONE ENGINE OUT
Applicable to:
BLEED CORRECTIONS
ISA ≥ ISA + 10
LONG RANGE ETNOGTIANLE A ANNTTI II CICEE O ONN –– 1310000 –– 45550000
GREEN DOT ETNOGTIANLE A ANNTTI II CICEE O ONN –– 140000 –– 23130000
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A330/A340 FLEET PRO-SPO-25-40 P 19/22
FCOM 19 AUG 10
GROSS CEILINGS AT LONG RANGE AND GREEN DOT SPEEDS - ONE ENGINE OUT
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A330/A340 FLEET PRO-SPO-25-40 P 20/22
FCOM 19 AUG 10
BLEED CORRECTIONS
ISA ≥ ISA + 10
LONG RANGE ETNOGTIANLE A ANNTTI II CICEE O ONN –– 110000 –– 2800000
GREEN DOT ETNOGTIANLE A ANNTTI II CICEE O ONN –– 110000 –– 1400000
EN ROUTE NET AND GROSS FLIGHT PATH - L/G DOWN - TWO ENGINES OUT
Applicable to:
EN ROUTE NET AND GROSS FLIGHT PATH - L/G DOWN - TWO ENGINES OUT
MAX. CONTINUOUS THRUST ISA
NORMAL AIR CONDITIONING Minimum engine
ANTI-ICING OFF CG = 17 %
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
A330/A340 FLEET PRO-SPO-25-40 P 21/22
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PERFORMANCE
Intentionally left blank
A330/A340 FLEET PRO-SPO-25-40 P 22/22
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
HIGH ALTITUDE OPERATION
A330/A340 FLEET PRO-SPO-30 P 1/2
FCOM 19 AUG 10
OPERATION ABOVE 8 000 FEET
Applicable to: ALL
The STANDARD OPERATING PROCEDURES (PRO NOR SOP) and ABNORMAL and
EMERGENCY PROCEDURES (PRO ABN) remain applicable for operation at high altitude airfields.
SYSTEM OPERATION
‐ PRESS
In case the aircraft takes off from an airfield higher than 8 000 ft the cabin altitude remains at
takeoff altitude until the cruise conditions are fulfilled (i.e. aircraft altitude 5 000 ft above takeoff
altitude and aircraft climb rate lower than 50 SLFPM for more than 32 s). After level off the cabin
altitude is controlled to the scheduled cruise cabin altitude. On the ECAM PRESS or CRUISE
page it can be observed that the cabin altitude starts changing 32 s after level off.
Note: After a takeoff with packs off the Cabin Pressure Controller (CLB mode) will control the
cabin altitude to takeoff altitude + 250 ft.
‐ HYD
If on ground the «RSVR LO AIR PR» ECAM caution is triggered, switch OFF the associated
hydraulic pumps (engines and electrical) before engine start to allow reservoir pressurization
before hydraulic pump operation.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
HIGH ALTITUDE OPERATION
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A330/A340 FLEET PRO-SPO-30 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT OVER MOUNTAINOUS AREA
A330/A340 FLEET PRO-SPO-35 P 1/2
FCOM 19 AUG 10
INTRODUCTION
Applicable to: ALL
Two failures must be taken into consideration for en route obstacle clearance over mountainous
area :
‐ Engine failure that forces a descent to a lower cruise level
‐ Depressurization which, due to the passenger oxygen system, requires a descent to 10 000 ft
before supplementary oxygen is exhausted.
ENGINE FAILURE
Applicable to: ALL
If the standard strategy does not allow the aircraft to clear obstacles, the pilot must use a drift down
procedure. If an engine failure occurs at any point on the route, the net flight path must clear the
obstacles on the drift down part by 2 000 ft and on the climb part by 1 000 ft.
　
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