A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 5(71)

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EXAMPLES....................................................................................................................................................... 2/26
FUEL TANKERING - FL290............................................................................................................................. 5/26
FUEL TANKERING - FL310............................................................................................................................. 9/26
FUEL TANKERING - FL330........................................................................................................................... 12/26
FUEL TANKERING - FL350........................................................................................................................... 16/26
FUEL TANKERING - FL370........................................................................................................................... 20/26
FUEL TANKERING - FL390........................................................................................................................... 23/26
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
PRELIMINARY PAGES - TABLE OF CONTENTS
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A330/A340 FLEET PER-FPL-PLP-TOC P 4/4
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
GENERAL - INTRODUCTION
A330/A340 FLEET PER-FPL-GEN-INT P 1/2
FCOM 19 AUG 10
INTRODUCTION
Applicable to:
Use this flight planning chapter when no precalculated flight plan is available.
It contains the following general graphs and tables :
‐ Climb ceilings at 300 ft/min for M .78, M .80, M .82, M .84
‐ Maximum and optimum cruise altitudes for M .80, M .82, M .84 and long range speed
‐ Optimum altitude on short stage
‐ Ground distance to air distance conversion for M .80, M .82, M .84 and long range speed.
The integrated range method includes the following tables :
‐ Integrated cruise tables for M .80, M .82, M .84 and long range speed at optimum FL
‐ Integrated cruise tables for long range speed for FL 100 up to FL 410
‐ Climb, step climb and descent correction tables
These tables allow the flight planning to be done segment by segment.
Refer to PER-FPL-FLP-CAT GENERAL contains calculation tables and a comprehensive example to
show how to use them.
The quick determination method is shown in Refer to PER-FPL-FLP-QFP-10 INTRODUCTION for
M .80, M .82, M .84 and long range speed.
INTRODUCTION
Applicable to: ,
Use this flight planning chapter when no precalculated flight plan is available.
It contains the following general graphs and tables :
‐ Maximum and optimum cruise altitudes for M .80, M .82, M .84 and long range speed
‐ Optimum altitude on short stage
‐ Ground distance to air distance conversion for M .80, M .82, M .84 and long range speed.
The integrated range method includes the following tables :
‐ Integrated cruise tables for M .80, M .82, M .84 and long range speed at optimum FL
‐ Integrated cruise tables for long range speed for FL 100 up to FL 410
‐ Climb, step climb and descent correction tables
These tables allow the flight planning to be done segment by segment.
Refer to PER-FPL-FLP-CAT GENERAL contains calculation tables and a comprehensive example to
show how to use them.
The quick determination method is shown in Refer to PER-FPL-FLP-QFP-10 INTRODUCTION for
M .80, M .82, M .84 and long range speed.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
GENERAL - INTRODUCTION
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A330/A340 FLEET PER-FPL-GEN-INT P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
GENERAL - MINIMUM RECOMMENDED FUEL REQUIREMENTS
A330/A340 FLEET PER-FPL-GEN-MFR P 1/4
FCOM 19 AUG 10
MINIMUM RECOMMENDED FUEL REQUIREMENTS
Applicable to:
The total fuel quantity required to fly a given sector is the sum of the following quantities :
TAXI FUEL
Quantity required for startup and taxi. Fuel calculation is based on a consumption of 25 kg/min or
55 lb/min
Average􀀃quantity􀀃(12􀀃min)􀀃→􀀃300􀀃kg􀀃or􀀃660􀀃lb􀀃
TRIP FUEL
Fuel required from departure to destination includes the following quantities :
‐ Takeoff and climb at selected speed.
‐ Cruise at selected speed.
‐ Descent from cruising level to 1 500 ft above destination airport.
‐ Approach and landing. Fuel calculation is based on a consumption of 55 kg/min or 120 lb/min.
Average􀀃quantity􀀃(6􀀃min􀀃IFR)􀀃→􀀃330􀀃kg􀀃or􀀃720􀀃lb􀀃
　
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