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6 : Add TO altitude correction 0.5 × 66 × 1.5 = 49.5 kg (enter 100 kg into table)
7 : Subtract value for step climb correction : 50 kg (enter 100 kg into table)
8 : Calculate corrected weight ovdqgd􀁄c􀀃cdrshm􀁄shnm􀀃→􀀃42􀀃6//􀀃􀁎f
9 : Enter weight overhead destination and find descent correction
(including 6 min IFR) (Refer to PER-FPL-FLP-ICR-60 DESCENT CORRECTION(􀀃→
200 kg
0/􀀃9􀀃B􀁄kbtk􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃cdrshm􀁄shnm􀀃→􀀃42􀀃8//􀀃􀁎f
11 : Subtract alternate fuel, e.g. : 100 nm at FL 100
(Refer to PER-FPL-FLP-ALN-10 CORRECTION FOR DEVIATION FROM REFERENCE
WEIGHT(􀀃→􀀃830􀀃􀁎f
􀀯􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃􀁄ksdqm􀁄sd􀀃→􀀃42􀀃8//􀀃- 941 = 52 959 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-10 CORRECTION FOR DEVIATION FROM REFERENCE
WEIGHT(􀀃→􀀃3􀀃×􀀃􀀋41􀀑8􀀃- 50) = 11.6 kg
Bnqqdbsdc􀀃􀁄ksdqm􀁄sd􀀃etdk􀀃→􀀃842􀀃􀁎f
01􀀃9􀀃B􀁄kbtk􀁄sd􀀃􀁄ksdqm􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃→􀀃41􀀃8//􀀃􀁎f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(􀀃→􀀃0􀀃/61􀀃􀁎f
14 : Calbtk􀁄sd􀀃vdhfgs􀀃􀁄s􀀃dmc􀀃ne􀀃gnkchmf􀀃→􀀃40􀀃7//􀀃􀁎f
04􀀃9􀀃B􀁄kbtk􀁄sd􀀃sqho􀀃etdk􀀃→􀀃01􀀃0//􀀃􀁎f
05􀀃9􀀃Rtasq􀁄bs􀀃“Dm􀀃Qntsd”􀀃qdrdqud􀀃􀀋rs􀁄mc􀁄qc􀀃􀁄lntms􀀃hr􀀃4􀀃􀀈􀀃ne􀀃sqho􀀃etdk(􀀃→􀀃5//􀀃􀁎f
06􀀃9􀀃B􀁄kbtk􀁄sd􀀃ydqn􀀃etdk􀀃vdhfgs􀀃→􀀃40􀀃1//􀀃􀁎f
18-19: Subtract dry operating weight to obtain maximum allowable payload.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A318/A319/A320/A321 FLEET PER-FPL-FLP-CAT P 11/42
FCOM 19 AUG 10
20-22: Calculate ramp fuel (Refer to PER-FPL-GEN-MFR MINIMUM RECOMMENDED FUEL
REQUIREMENTS for taxi fuel).
23-26: Calculate flight time :
(See CALCULATION TABLE,
Refer to PER-FPL-FLP-ICR-40-A CLIMB CORRECTION - M.78 and LONG RANGE
SPEED,
Refer to PER-FPL-FLP-ICR-60 DESCENT CORRECTION).
1 (1) Max TO Weight at BRAKE RELEASE ◂ ◂ 6 6 • 0
2 WEIGHT Overhead Destination ◂ 5 5 • 1
3 - Temperature Correction for CRUISE - 0 • 4
4 + Correction for Low Air Conditioning + 0 • 0
5 - CLIMB correction - 1 • 0
6 + TO Altitude correction + 0 • 1
7 - STEP CLIMB correction - 0 • 1
8 = Corrected Weight Overhead Destination = 5 3 • 7
9 + DESCENT correction (including 6 min IFR) + 0 • 2
10 (2) Landing Weight at Destination = 5 3 • 9
11 - ALTERNATE Fuel - 1 • 0
12 = ALTERNATE Landing Weight = 5 2 • 9
13 - HOLDING - 1 • 1
14 = Weight at END OF HOLDING = 5 1 • 8
15 TRIP FUEL (1) - (2) 1 2 • 1 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 0 • 6
17 (3) ZERO FUEL WEIGHT = 5 1 • 2
18 - OPERATING WEIGHT EMPTY - 3 9 • 2
19 = Max Allowable Payload = 1 2 • 0
BLOCK FUEL CALCULATION
20 Required Fuel (1) - (3) ◂ 1 4 • 7
21 + Taxi + 0 • 2
22 = Block Fuel = 1 4 • 9
FLIGHT TIME CALCULATION (H. MIN)
23 Time from integrated Cruise Tables ◂ 5 • 0 0
24 + CLIMB Correction + 0 • 0 4
25 + DESCENT Correction (including 6 min IFR) + 0 • 1 0
26 = Flight Time = 5 • 1 4
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - CALCULATION TABLES
A318/A319/A320/A321 FLEET PER-FPL-FLP-CAT P 12/42
FCOM 19 AUG 10
Note: Line 3 : temperature correction :
0.015 (kg/°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).
　
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