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GENERAL
Applicable to: ,
The planner must correct the values for the fuel and the time obtained from the integrated cruise
tables with the numbers given in the following tables. The tables which are established for M .80,
M .82, M .84 and long range speed, take into account climbing from the brake release point at
250 kt/300 kt/M .80.
LONG RANGE SPEED
CORRECTION ON FUEL CONSUMPTION (1 000 kg)
FL 140 150 160 W1E7IG0 HT A1T8 0BRAK1E9 R0ELEA2S00E (1 00201 0kg) 220 230 240
time
correction
410 2.2 2.3 2.5 2.6 2.7 - - - - - - 4 min
390 2.1 2.3 2.4 2.5 2.7 2.8 2.8 - - - - 4 min
370 2.0 2.2 2.3 2.4 2.6 2.7 2.8 2.9 3.1 3.1 - 5 min
350 2.0 2.1 2.2 2.3 2.5 2.6 2.7 2.9 3.1 3.1 3.2 5 min
330 1.9 2.0 2.1 2.3 2.4 2.5 2.6 2.8 3.0 3.0 3.2 5 min
310 1.8 1.9 2.0 2.2 2.3 2.4 2.5 2.7 2.9 2.9 3.1 5 min
290 1.7 1.8 1.9 2.0 2.2 2.3 2.4 2.5 2.6 2.8 2.9 5 min
270 1.6 1.7 1.8 1.9 2.0 2.1 2.3 2.4 2.5 2.6 2.8 5 min
250 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3 2.5 2.6 4 min
200 1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 4 min
150 1.0 1.1 1.2 1.2 1.3 1.4 1.4 1.5 1.5 1.7 1.8 3 min
100 0.7 0.8 0.8 0.9 0.9 1.0 1.1 1.1 1.2 1.2 1.3 2 min
CLIMB TO OPTIMUM FL
CORRECTION ON FUEL CONSUMPTION (1 000 kg)
SPEED 140 150 160 WE1IG70HT AT1 8B0RAKE19 R0ELEA2S00E (1 020100 kg) 220 230 240
time
correction
LRC 2.2 2.3 2.5 2.6 2.7 2.7 2.8 2.9 3.0 3.0 3.1 5 min
M 80 2.2 2.4 2.5 2.6 2.7 2.7 2.8 2.9 3.0 3.1 3.2 5 min
M 82 2.2 2.3 2.5 2.6 2.7 2.8 2.8 2.9 3.0 3.0 3.1 5 min
M 84 2.1 2.3 2.4 2.4 2.5 2.6 2.6 2.7 2.8 2.8 2.8 5 min
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - INTEGRATED CRUISE
A330/A340 FLEET PER-FPL-FLP-ICR-70 P 1/2
FCOM 19 AUG 10
STEP CLIMB CORRECTION
STEP CLIMB CORRECTION
Applicable to:
When the flight includes one or more step climbs (2 000 ft below FL 290, 4 000 ft above), apply a
correction of 300 kg per step climb to the fuel consumption.
STEP CLIMB CORRECTION
Applicable to: ,
When the flight includes one or more step climbs (2 000 ft below FL 290, 4 000 ft above), apply a
correction of 160 kg per step climb to the fuel consumption.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - INTEGRATED CRUISE
Intentionally left blank
A330/A340 FLEET PER-FPL-FLP-ICR-70 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - INTEGRATED CRUISE
A330/A340 FLEET PER-FPL-FLP-ICR-80 P 1/2
FCOM 19 AUG 10
DESCENT CORRECTION
GENERAL
Applicable to:
Correct the fuel and time values determined in the integrated cruise tables as follows to take into
account the descent down to 1 500 ft followed by 6 min IFR approach and landing.
LONG RANGE CRUISE SPEED
CORRECTION ON FUEL CONSUMPTION (1 000 kg)
FL 150 WEIG1H60T OVERHEAD 1D7E0STINATION (11 08000 kg) 190 time correction
310and
above 0.3 0.4 0.4 0.5 0.6 11 min
290 0.3 0.4 0.4 0.5 0.6 11 min
250 0.3 0.3 0.4 0.4 0.5 10 min
200 0.2 0.2 0.3 0.3 0.4 9 min
150 0.1 0.1 0.2 0.2 0.2 8 min
100 0.0 0.0 0.0 0.0 0.0 8 min
DESCENT FROM OPTIMUM FL
CORRECTION ON FUEL CONSUMPTION (1 000 kg)
SPEED 150WEIG1H6T0 OVERHEAD 1D7E0STINATION (11 80000 kg) 190 time correction
LR 0.4 0.5 0.5 0.6 0.7 11 min
M 80 0.3 0.4 0.5 0.6 0.7 11 min
M 82 0.4 0.5 0.5 0.6 0.7 11 min
M 84 0.5 0.5 0.6 0.7 0.8 12 min
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - INTEGRATED CRUISE
Intentionally left blank
A330/A340 FLEET PER-FPL-FLP-ICR-80 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - QUICK DETERMINATION OF FLIGHT PLANNING
A330/A340 FLEET PER-FPL-FLP-QFP-10 P 1/2
FCOM 19 AUG 10
INTRODUCTION
INTRODUCTION
Applicable to:
The following flight planning tables allow the planner to determine trip fuel consumption and trip time
required to cover a given air distance.
These tables are established for :
‐ Takeoff
‐ Climb profile : 250 kt/300 kt/M .78
‐ Cruise Mach number : M .80/M .82/.M 84/LR
‐ Descent profile : Cruise Mach number/300 kt/250 kt
‐ Approach and landing : 330 kg - 6 min IFR
‐ ISA
‐ CG = 37 %
‐ Normal air conditioning
‐ Anti ice OFF
They are based upon a reference landing weight of 150 000 kg.
Note: 1. In the tables, the asterisk (*) means that a step climb of 4 000 ft must be flown to reach
the corresponding FL.
2. To obtain a flight plan at optimum cruise level, the highest flight level desired within the
　
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