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24 + CLIMB Correction + •
25 + DESCENT Correction (including 6 min IFR) + •
26 = Flight Time = •
Note: Line 3 : temperature correction :
0.015 (kg/°C/NM) × ▵ISA (°C) × air distance (NM) or
0.033 (lb/°C/NM) × ▵ISA (°C) × air distance (NM)
Line 6 : TO altitude correction :
0.5 (kg/1 000 kg/1 000 ft) × TOW (1 000 kg) × airport elevation (1 000 ft) or
0.5 (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
A330/A340 FLEET PER-FPL-FLP-CAT P 7/22
FCOM 19 AUG 10
CALCULATION TABLE
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 8/22
FCOM 19 AUG 10
1􀀃(1)􀀃Max􀀃TO􀀃Weight􀀃at􀀃BRAKE􀀃RELEASE􀀃▹􀀃•􀀃
2􀀃WEIGHT􀀃Overhead􀀃Destination􀀃▹􀀃•􀀃
3 - Temperature Correction for CRUISE - •
4 + Correction for Air Conditioning (+ for LO, - for HI) + •
5 - CLIMB correction - •
6 + TO Altitude correction + •
7 - STEP CLIMB correction - •
8 = Corrected Weight Overhead Destination = •
9 + DESCENT correction (including 6 min IFR) + •
10 (2) Landing Weight at Destination = •
11 - ALTERNATE Fuel - •
12 = ALTERNATE Landing Weight = •
13 - HOLDING - •
14 = Weight at END OF HOLDING = •
15 TRIP FUEL (1) - (2) • / / / / / / / / / / / / / / /
16 - "En Route" Reserve - •
17 (3) ZERO FUEL WEIGHT = •
18 - OPERATING WEIGHT EMPTY - •
19 = Max Allowable Payload = •
BLOCK FUEL CALCULATION
20􀀃Required􀀃Fuel􀀃(1)􀀃-􀀃(3)􀀃▹􀀃•􀀃
21 + Taxi + •
22 = Block Fuel = •
FLIGHT TIME CALCULATION (H. MIN)
23􀀃Time􀀃from􀀃integrated􀀃Cruise􀀃Tables􀀃▹􀀃•􀀃
24 + CLIMB Correction + •
25 + DESCENT Correction (including 6 min IFR) + •
26 = Flight Time = •
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 9/22
FCOM 19 AUG 10
Note: Line 3 : temperature correction :
0.010 (kg/°C/NM) × ▵ISA (°C) × air distance (NM) or
0.022 (lb/°C/NM) × ▵ISA (°C) × air distance (NM)
Line 4 : in case of low air conditioning refer to cruise table correction box (Refer to
PER-FPL-FLP-ICR-10 GENERAL).
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.
EXAMPLE
Applicable to:
DATA
‐ TO weight : 240 000 kg
‐ Ground distance to destination : 5 000 nm
‐ Wind : –40 kt (head wind)
‐ Selected initial FL : 330
‐ Long range speed
‐ Temperature : ISA +10
DETERMINATION OF CRUISE FUEL AND TIME
A : Enter the chosen flight Mach number and flight level, ground distance to be covered and
forecast windspeed in the calculation table (See CALCULATION TABLE).
Calculate the air distance (Refer to PER-OPD-CON-AEO GENERAL)
here : long range speed, 40 kt head wind, 5 000 nm ground distance
→􀀃air􀀃distance􀀃:􀀃5􀀃485􀀃nm􀀃
CRUISE TABLE FL 330
B : Read from integrated cruise table (long range speed, FL 330) the values for time and
distance for a weight of 240 000 kg (Refer to PER-FPL-FLP-ICR-50 INTEGRATED
CRUISE - LR FL 330)
→􀀃distance􀀃:􀀃8􀀃718􀀃nm􀀃→􀀃time􀀃:􀀃1􀀃154􀀃min.􀀃
　
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