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A330/A340 FLEET PER-CRZ-AEO-ALT-20 P 5/8
FCOM 19 AUG 10
GIVEN : Weight : 190 000 kg (419 000 lb)
Wind at FL 370 : 10 kt head
FIND : Minimum wind difference to descend to FL 330 : (26 - 3) = 23 kt
RESULTS : Descent to FL 330 may be considered provided the tail wind at this altitude is more
than (23 - 10) = 13 kt.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-20 P 6/8
FCOM 19 AUG 10
GIVEN : Weight : 195 000 kg (430 000 lb)
Wind at FL 350 : 15 kt head
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-20 P 7/8
FCOM 19 AUG 10
FIND : Minimum wind difference to descend to FL 310 : (51- 11) = 40 kt
RESULTS : Descent to FL 310 may be considered provided the tail wind at this altitude is more
than (40- 15) = 25 kt.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-20 P 8/8
FCOM 19 AUG 10
GIVEN : Weight : 190 000 kg (419 000 lb)
Wind at FL 350 : 10 kt head
FIND : Minimum wind difference to descend to FL 310 : (55 - 6) = 49 kt
RESULTS : Descent to FL 310 may be considered provided the tail wind at this altitude is more
than (49 - 10) = 39 kt.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-30 P 1/4
FCOM 19 AUG 10
OPTIMUM ALTITUDE ON SHORT STAGE
OPTIMUM ALTITUDE ON SHORT STAGE
Applicable to:
According to the air distance (from brake release point to landing), the cruise flight level is limited by
the distance required to perform climb and descent. The graph determines the optimum altitude.
It includes the following profiles :
‐ Takeoff
‐ Climb : 250 kt/300 kt/M .78
‐ Long range cruise (during at least 5 min)
‐ Descent : M .80/300 kt/250 kt
‐ Approach and landing
and it is established for
‐ ISA
‐ CG = 37 %
‐ Normal air conditioning
‐ Anti ice OFF
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-30 P 2/4
FCOM 19 AUG 10
OPTIMUM ALTITUDE ON SHORT STAGE
Applicable to: ,
According to the air distance (from brake release point to landing), the cruise flight level is limited by
the distance required to perform climb and descent. The graph determines the optimum altitude.
It includes the following profiles :
‐ Takeoff
‐ Climb : 250 kt/300 kt/M .80
‐ Long range cruise (during at least 5 min)
‐ Descent : M .80/300 kt/250 kt
‐ Approach and landing
and it is established for
‐ ISA
‐ CG = 37 %
‐ Normal air conditioning
‐ Anti ice OFF
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-30 P 3/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
Intentionally left blank
A330/A340 FLEET PER-CRZ-AEO-ALT-30 P 4/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - CRUISE TABLES
A330/A340 FLEET PER-CRZ-AEO-CRT-20 P 1/10
FCOM 19 AUG 10
CRUISE AT M.80
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - CRUISE TABLES
A330/A340 FLEET PER-CRZ-AEO-CRT-20 P 2/10
FCOM 19 AUG 10
CRUISE AT M.80 - ISA
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - CRUISE TABLES
A330/A340 FLEET PER-CRZ-AEO-CRT-20 P 3/10
FCOM 19 AUG 10
CRUISE AT M.80 - ISA
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - CRUISE TABLES
A330/A340 FLEET PER-CRZ-AEO-CRT-20 P 4/10
FCOM 19 AUG 10
CRUISE AT M.80 - ISA + 10
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - CRUISE TABLES
A330/A340 FLEET PER-CRZ-AEO-CRT-20 P 5/10
FCOM 19 AUG 10
CRUISE AT M.80 - ISA + 10
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - CRUISE TABLES
A330/A340 FLEET PER-CRZ-AEO-CRT-20 P 6/10
FCOM 19 AUG 10
CRUISE AT M.80 - ISA + 15
　
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