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NET CEILING AT GREEN DOT SPEED..............................................................................................................2/2
PER-CRZ-TEI-CRT CRUISE TABLES
PER-CRZ-TEI-CRT-10 STANDARD STRATEGY
LONG RANGE CRUISE - ISA............................................................................................................................2/6
LONG RANGE CRUISE - ISA + 10..................................................................................................................... 3/6
LONG RANGE CRUISE - ISA + 15..................................................................................................................... 4/6
LONG RANGE CRUISE - ISA + 20..................................................................................................................... 5/6
PER-CRZ-TEI-ICQ IN CRUISE QUICK CHECK
FUEL AND TIME FROM LEVEL OFF TO END OF DESCENT AT 1500 FT.......................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - GENERAL
A330/A340 FLEET PER-CRZ-AEO-GEN P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
Cruise tables are established :
• for ISA, ISA +10, ISA +15 and ISA +20
• with normal air conditioning and anti ice OFF
• from FL 290 to FL 410 at M .80, M .82 and M .84
• from FL 100 to FL 410 at long range speed
• with a 30 % center of gravity below 25 000 ft and a 37 % center of gravity at higher altitudes.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - GENERAL
Intentionally left blank
A330/A340 FLEET PER-CRZ-AEO-GEN P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON (CI)
A330/A340 FLEET PER-CRZ-AEO-ECI-10 P 1/4
FCOM 19 AUG 10
OPTIMUM MACH NUMBER
OPTIMUM MACH NUMBER
Applicable to:
Six tables give the optimum Mach number versus cost index, altitude and wind as calculated by the
FMGC.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON (CI)
A330/A340 FLEET PER-CRZ-AEO-ECI-10 P 2/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON (CI)
A330/A340 FLEET PER-CRZ-AEO-ECI-10 P 3/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON (CI)
Intentionally left blank
A330/A340 FLEET PER-CRZ-AEO-ECI-10 P 4/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-10 P 1/8
FCOM 19 AUG 10
OPTIMUM AND MAXIMUM ALTITUDES
DEFINITIONS
Applicable to:
Optimum altitude : the altitude at which the airplane covers ‐ the maximum distance per kilogram of
fuel (best specific range). It depends on the actual weight and the deviation from ISA.
‐ Maximum altitude : Maximum altitude which can be flown in level flight without acceleration at
maximum cruise thrust.
Note: Definition of the maximum altitude in the FMGC is different (Refer to DSC-22_20-50-10-20
PROG PAGES).
DEFINITIONS
Applicable to: ,
• Optimum altitude : the altitude at which the airplane covers the maximum distance per kilogram of
fuel (best specific range). It depends on the actual weight and the deviation from ISA.
• Maximum altitude is defined as the lower of :
‐ Maximum altitude at maximum cruise thrust in level flight and
‐ Maximum altitude at maximum climb thrust with 300 ft/min vertical speed.
Note: Definition of the maximum altitude in the FMGC is different (Refer to DSC-22_20-50-10-20
PROG PAGES).
CRUISE LEVEL CHARTS
Applicable to:
These charts have been established for a center of gravity at 37 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed, M 0.82,
M 0.83 and M 0.84
Note: 1. Optimum and maximum altitudes curves do not cover for M 0.82, M 0.83 and M 0.84
the whole weight range because above a given weight these Mach numbers cannot be
maintained, whatever the altitude.
2. The n =1.3 g (n = 1.4 g) curve indicates the buffet margin.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A330/A340 FLEET PER-CRZ-AEO-ALT-10 P 2/8
FCOM 19 AUG 10
OPTIMUM WEIGHT FOR 4 000 FT STEP CLIMB
WEIGHT (1 000 kg)
ISA ISA +10 ISA +20
STEP
CLIMB
FROM/TO LRM .80 M.82 M.84 LR M .80 M.82 M .84 LRM .80 M.82 M.84
　
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