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FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 18/22
FCOM 19 AUG 10
DATA
‐ TO weight : 200 000 kg
‐ Ground distance to destination 4 000 nm
‐ Wind : –40 kt (headwind)
‐ Selected first flight level : FL 330
‐ Long range speed
‐ Temperature : ISA +10 along the whole flight profile
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 19/22
FCOM 19 AUG 10
‐ Airport elevation : 1 500 ft
‐ Normal air conditioning
STEPS
1􀀃:􀀃Fill􀀃in􀀃Max􀀃TO􀀃weight􀀃→􀀃200􀀃000􀀃kg􀀃
2 : Enter the integrated cruise table corresponding to chosen FL with TO weight at brake
release point and calculate weight overhead destination (See CALCULATION TABLE)
Fill􀀃in􀀃→􀀃152􀀃750􀀃kg􀀃
3 : Apply temperature correction for given air distance
4 380 nm × 10 °C × 0.010 kg/°C/NM = 438 kg
4􀀃:􀀃Correction􀀃for􀀃air􀀃conditioning􀀃→􀀃here􀀃=􀀃0􀀃
5 : Subtract climb correction for chosen FL (Refer to PER-FPL-FLP-ICR-70 STEP CLIMB
CORRECTION)􀀃→􀀃2􀀃600􀀃kg􀀃
6 : Add TO altitude correction 0.9 × 200 × 1.5 = 270 kg
7 : Subtract value for step climb correction (Refer to PER-FPL-FLP-ICR-70 STEP CLIMB
CORRECTION) 2 × 160 = 320 kg
8􀀃:􀀃Calculate􀀃corrected􀀃weight􀀃overhead􀀃destination􀀃→􀀃149􀀃500􀀃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􀀃→􀀃149􀀃900􀀃kg􀀃
11 : Alternate fuel e.g. 250 nm at FL 270
(Refer to PER-FPL-FLP-ALN-30 ALTERNATE PLANNING - ISA)􀀃→􀀃4􀀃021􀀃kg􀀃
Landing weight at alternate 149 900 - 4 021 = 145 879 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-30 ALTERNATE PLANNING - ISA) (145.9 – 140) × 11 = 65 kg
Corrected alternate fuel 4 021 + 65 = 4 086 kg
12􀀃:􀀃Calculate􀀃alternate􀀃landing􀀃weight􀀃→􀀃145􀀃800􀀃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􀀃→􀀃143􀀃000􀀃kg􀀃
15􀀃:􀀃Calculate􀀃trip􀀃fuel􀀃→􀀃50􀀃100􀀃kg􀀃
16􀀃:􀀃Subtract􀀃“en􀀃route”􀀃reserve􀀃(standard􀀃amount􀀃is􀀃5􀀃%􀀃of􀀃trip􀀃fuel􀀃→􀀃2􀀃505􀀃kg)􀀃
17􀀃:􀀃Calculate􀀃zero􀀃fuel􀀃weight􀀃→􀀃140􀀃500􀀃kg􀀃
18-19: Subtract dry operating weight to obtain maximum allowable payload
20-22: Calculate block fuel
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A330/A340 FLEET PER-FPL-FLP-CAT P 20/22
FCOM 19 AUG 10
23-26: Calculate flight time
1􀀃(1)􀀃Max􀀃TO􀀃Weight􀀃at􀀃BRAKE􀀃RELEASE􀀃▹􀀃2􀀃0􀀃0􀀃•􀀃0􀀃
2􀀃WEIGHT􀀃Overhead􀀃Destination􀀃▹􀀃1􀀃5􀀃2􀀃•􀀃8􀀃
3 - Temperature Correction for CRUISE - 0 • 5
4 + Correction for Air Conditioning (+ for LO, - for HI) + 0 • 0
5 - CLIMB correction - 2 • 6
6 + TO Altitude correction + 0 • 2
7 - STEP CLIMB correction - 0 • 4
8 = Corrected Weight Overhead Destination = 1 4 9 • 5
9 + DESCENT correction (including 6 min IFR) + 0 • 4
10 (2) Landing Weight at Destination = 1 4 9 • 9
11 - ALTERNATE Fuel - 4 • 1
12 = ALTERNATE Landing Weight = 1 4 5 • 8
13 - HOLDING - 2 • 8
　
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