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7 : Subtract value for step climb correction (Refer to PER-FPL-FLP-ICR-60 GENERAL) 2 ×
300 = 600 kg
8􀀃:􀀃Calculate􀀃corrected􀀃weight􀀃overhead􀀃destination􀀃→􀀃163􀀃600􀀃kg􀀃
9 : Enter weight overhead destination and find descent correction (including 6 min IFR)
(Refer to PER-FPL-FLP-ICR-80 GENERAL)􀀃→􀀃400􀀃kg􀀃
10􀀃:􀀃Calculate􀀃landing􀀃weight􀀃at􀀃destination􀀃→􀀃164􀀃000􀀃kg􀀃
11 : Subtract alternate fuel e.g. 150 nm at FL 120
(Refer to PER-FPL-FLP-ALN-30 ALTERNATE PLANNING - ISA)􀀃→􀀃3􀀃514􀀃kg􀀃
Landing weight at alternate 164 000 - 3 514 = 160 486 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-30 ALTERNATE PLANNING - ISA) (160.5 – 150) × 8 = 84 kg
Corrected alternate fuel 3 514 + 84 = 3 598 kg
12􀀃:􀀃Calculate􀀃alternate􀀃landing􀀃weight􀀃→􀀃160􀀃400􀀃kg􀀃
13 : Subtract holding fuel : (Refer to PER-FPL-GEN-MFR MINIMUM RECOMMENDED
FUEL REQUIREMENTS)􀀃→􀀃2􀀃800􀀃kg􀀃
14􀀃:􀀃Calculate􀀃weight􀀃at􀀃end􀀃of􀀃holding􀀃→􀀃157􀀃600􀀃kg􀀃
15􀀃:􀀃Calculate􀀃trip􀀃fuel􀀃→􀀃76􀀃000􀀃kg􀀃
16􀀃:􀀃Subtract􀀃“en􀀃route”􀀃reserve􀀃(standard􀀃amount􀀃is􀀃5􀀃%􀀃of􀀃trip􀀃fuel􀀃→􀀃3􀀃800􀀃kg)􀀃
17􀀃:􀀃Calculate􀀃zero􀀃fuel􀀃weight􀀃→􀀃153􀀃800􀀃kg􀀃
18-19: Subtract dry operating weight to obtain maximum allowable payload
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 14/22
FCOM 19 AUG 10
20-22: Calculate block fuel
23-26: Calculate flight time
1􀀃(1)􀀃Max􀀃TO􀀃Weight􀀃at􀀃BRAKE􀀃RELEASE􀀃▹􀀃2􀀃4􀀃0􀀃•􀀃0􀀃
2􀀃WEIGHT􀀃Overhead􀀃Destination􀀃▹􀀃1􀀃6􀀃8􀀃•􀀃4􀀃
3 - Temperature Correction for CRUISE - 0 • 9
4 + Correction for Air Conditioning + 0 • 0
5 - CLIMB correction - 3 • 4
6 + TO Altitude correction + 0 • 1
7 - STEP CLIMB correction - 0 • 6
8 = Corrected Weight Overhead Destination = 1 6 3 • 6
9 + DESCENT correction (including 6 min IFR) + 0 • 4
10 (2) Landing Weight at Destination = 1 6 4 • 0
11 - ALTERNATE Fuel - 3 • 6
12 = ALTERNATE Landing Weight = 1 6 0 • 4
13 - HOLDING - 2 • 8
14 = Weight at END OF HOLDING = 1 5 7 • 6
15 TRIP FUEL (1) - (2) 7 6 • 0 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 3 • 8
17 (3) ZERO FUEL WEIGHT = 1 5 3 • 8
18 - OPERATING WEIGHT EMPTY - 1 2 7 • 0
19 = Max Allowable Payload = 2 6 • 8
BLOCK FUEL CALCULATION
20􀀃Required􀀃Fuel􀀃(1)􀀃-􀀃(3)􀀃▹􀀃8􀀃6􀀃•􀀃2􀀃
21 + Taxi + 0 • 3
22 = Block Fuel = 8 6 • 5
FLIGHT TIME CALCULATION (H. MIN)
23􀀃Time􀀃from􀀃integrated􀀃Cruise􀀃Tables􀀃▹􀀃1􀀃1􀀃•􀀃4􀀃4􀀃
24 + CLIMB Correction + 0 • 0 6
25 + DESCENT Correction (including 6 min IFR) + 0 • 1 1
26 = Flight Time = 1 2 • 0 1
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 15/22
FCOM 19 AUG 10
Note: Line 3 : temperature correction :
0.015 (kg/°C/NM) × ΔISA(°C) × air distance (NM) or
0.033 (lb/°C/NM) × ΔISA(°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
　
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