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CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 17/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 18/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 19/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 20/32
FCOM 19 AUG 10
OPTIMUM MACH NUMBER
Applicable to: MSN,
Seven tables give the optimum Mach number versus cost index, altitude and wind as calculated by
the FMGC.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 21/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 22/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 23/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 24/32
FCOM 19 AUG 10
OPTIMUM MACH NUMBER
Applicable to:
Seven tables give the optimum Mach number versus cost index, altitude and wind as calculated by
the FMGC.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 25/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 26/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 27/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 28/32
FCOM 19 AUG 10
OPTIMUM MACH NUMBER
Applicable to: ,
, MSN
Seven tables give the optimum Mach number versus cost index, altitude and wind as calculated by
the FMGC.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 29/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 30/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 31/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ECON(CI)
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ECI-10 P 32/32
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ALL ENGINES OPERATIVE - ALTITUDE
A318/A319/A320/A321 FLEET PER-CRZ-AEO-ALT-10 P 1/16
FCOM 19 AUG 10
OPTIMUM AND MAXIMUM ALTITUDES
DEFINITIONS
Applicable to: ALL
• Optimum altitude : the altitude at which the airplane covers the maximum distance per kilogram
(pound) 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
STLO-22_20_R-50-10-20 PROG PAGES).
CRUISE LEVEL CHARTS
Applicable to:
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: 1. Optimum and maximum altitudes curves do not cover for M .78 the whole weight range
because above a given weight these Mach numbers cannot be maintained, whatever the
　
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