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S􀀤A􀀯D(􀀑􀀃Ehkk􀀃hm􀀃→􀀃5/􀀃1//􀀃􀁎f
3 : Apply temperature correction for given air distance :
2 248 nm × 10 °C × 0.015/°C/NM = 337 kg (enter 400 kg into table)
3􀀃9􀀃Bnqqdbshnm􀀃enq􀀃knv􀀃􀁄hq􀀃bnmchshnmhmf􀀃→􀀃gdqd􀀃<􀀃/
5 : Subtract climb correction for chosen FL (Refer to PER-FPL-FLP-ICR-40-A CLIMB
CORRECTION - M.78 and LONG RANGE SPEED(􀀃→􀀃0􀀃/4/􀀃􀁎f
6 : Add TO altitude correction 0.5 × 72 × 1.5 = 54 kg (enter100 kg into table)
7 : Subtract value for step climb correction : 50 kg (enter 100 kg into table)
8 : Calculate corrected weight overhead destinatiom􀀃→􀀃47􀀃6//􀀃􀁎f
9 : Enter weight overhead destination and find descent correction
(including 6 min IFR) (Refer to PER-FPL-FLP-ICR-60 DESCENT CORRECTION(􀀃→
300 kg
0/􀀃9􀀃B􀁄kbtk􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃cdrshm􀁄shnm􀀃→􀀃48􀀃///􀀃􀁎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(􀀃→􀀃873􀀃􀁎f
􀀯􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃􀁄ksdqm􀁄sd􀀃→􀀃48􀀃///􀀃- 984 = 58 016 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-20 ALTERNATE PLANNING ISA(􀀃→􀀃5􀀃×􀀃􀀋47􀀑/􀀃- 55) = 18 kg
Bnqqdbsdc􀀃􀁄ksdqm􀁄sd􀀃etdk􀀃→􀀃0􀀃//1􀀃􀁎f
01􀀃9􀀃B􀁄kbtk􀁄sd􀀃􀁄ksdqm􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃→􀀃47􀀃///􀀃􀁎f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(􀀃→􀀃0􀀃/87􀀃􀁎f
03􀀃9􀀃B􀁄kbtk􀁄sd􀀃vdhfgs􀀃􀁄s􀀃dmc􀀃ne􀀃gnkchmf􀀃→􀀃45􀀃1//􀀃kg
04􀀃9􀀃B􀁄kbtk􀁄sd􀀃sqho􀀃etdk􀀃→􀀃02􀀃///􀀃􀁎f
05􀀃9􀀃Rtasq􀁄bs􀀃“Dm􀀃Qntsd”􀀃qdrdqud􀀃􀀋rs􀁄mc􀁄qc􀀃􀁄lntms􀀃hr􀀃4􀀃􀀈􀀃ne􀀃sqho􀀃etdk(􀀃→􀀃54/􀀃􀁎f
06􀀃9􀀃B􀁄kbtk􀁄sd􀀃ydqn􀀃etdk􀀃vdhfgs􀀃→􀀃45􀀃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 21/42
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 ◂ ◂ 7 2 • 0
2 WEIGHT Overhead Destination ◂ 6 0 • 2
3 - Temperature Correction for CRUISE - 0 • 4
4 + Correction for Low Air Conditioning + 0 • 0
5 - CLIMB correction - 1 • 1
6 + TO Altitude correction + 0 • 1
7 - STEP CLIMB correction - 0 • 1
8 = Corrected Weight Overhead Destination = 5 8 • 7
9 + DESCENT correction (including 6 min IFR) + 0 • 3
10 (2) Landing Weight at Destination = 5 9 • 0
11 - ALTERNATE Fuel - 1 • 0
12 = ALTERNATE Landing Weight = 5 8 • 0
13 - HOLDING - 1 • 1
14 = Weight at END OF HOLDING = 5 6 • 9
15 TRIP FUEL (1) - (2) 1 3 • 0 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 0 • 7
17 (3) ZERO FUEL WEIGHT = 5 6 • 2
18 - OPERATING WEIGHT EMPTY - 4 1 • 3
19 = Max Allowable Payload = 1 4 • 9
BLOCK FUEL CALCULATION
20 Required Fuel (1) - (3) ◂ 1 5 • 8
21 + Taxi + 0 • 2
22 = Block Fuel = 1 6 • 0
FLIGHT TIME CALCULATION (H. MIN)
23 Time from integrated Cruise Tables ◂ 5 • 0 0
　
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