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14 = Weight at END OF HOLDING = 1 4 3 • 0
15 TRIP FUEL (1) - (2) 5 0 • 1 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 2 • 5
17 (3) ZERO FUEL WEIGHT = 1 4 0 • 5
18 - OPERATING WEIGHT EMPTY - 1 1 8 • 0
19 = Max Allowable Payload = 2 2 • 5
BLOCK FUEL CALCULATION
20􀀃Required􀀃Fuel􀀃(1)􀀃-􀀃(3)􀀃▹􀀃5􀀃9􀀃•􀀃5􀀃
21 + Taxi + 0 • 3
22 = Block Fuel = 5 9 • 8
FLIGHT TIME CALCULATION (H. MIN)
23􀀃Time􀀃from􀀃integrated􀀃Cruise􀀃Tables􀀃▹􀀃9􀀃•􀀃2􀀃2􀀃
24 + CLIMB Correction + 0 • 0 5
25 + DESCENT Correction (including 6 min IFR) + 0 • 1 1
26 = Flight Time = 9 • 3 8
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 21/22
FCOM 19 AUG 10
Note: Line 3 : temperature correction :
0.010 (kg/°C/NM) × ΔISA(°C) × air distance (NM) or
0.022 (lb/°C/NM) × ΔISA(°C) × air distance (NM)
Line 4 : in case of low air conditioning refer to cruise table correction box.
Line 6 : TO altitude correction :
0.9 (kg/1 000 kg/1 000 ft) × TOW (1 000 kg) × airport elevation (1 000 ft) or
0.9 (lb/1 000 lb/1 000 ft) × TOW (1 000 lb) × airport elevation (1 000 ft)
Line 10 : Check that landing weight at destination is lower than maximum landing
weight.
Line 17 : Check that the zero fuel weight is lower than maximum zero fuel weight.
Line 22 : Check that the block fuel value is lower than maximum tank capacity.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
Intentionally left blank
A330/A340 FLEET PER-FPL-FLP-CAT P 22/22
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A330/A340 FLEET PER-FPL-FLP-ALT-05 P 1/2
FCOM 19 AUG 10
GENERAL
CLIMB CEILING
Applicable to:
A minimum climb rate of 300 ft/minis usually used to define the climb ceiling. The following graphs
show for M .78, M .80, M .82, M .84 the flight levels that can be reached with a minimum rate of climb
of 300 ft/min.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A330/A340 FLEET PER-FPL-FLP-ALT-05 P 2/2
FCOM 19 AUG 10
BLEED CORRECTIONS
ENGINE ANTI ICE ON TOTAL ANTI ICE ON PACK FLOWHI AND/OR
CARGO COOL ON
≤ ISA +4 - 100 ft - 250 ft - 250 ft
ISA +20 -1 700 ft -2 700 ft - 400 ft
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A330/A340 FLEET PER-FPL-FLP-ALT-10 P 1/8
FCOM 19 AUG 10
OPTIMUM AND MAXIMUM ALTITUDES
DEFINITIONS
Applicable to:
DEFINITIONS
‐ 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 FCOM).
DEFINITIONS
Applicable to: ,
DEFINITIONS
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 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 FCOM).
CRUISE LEVEL CHARTS
Applicable to: ,
CRUISE LEVEL CHARTS
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 and
M .80, M .82 and M .84.
Note: 1. Optimum and maximum altitude curves do not cover for M .80, M .82 and M .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
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A330/A340 FLEET PER-FPL-FLP-ALT-10 P 2/8
　
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