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STEPS
0􀀃9􀀃Ehkk􀀃hm􀀃L􀁄w􀀃SN􀀃vdhfgs􀀃→􀀃61􀀃///􀀃􀁎f
2 : Enter the integrated cruise table corresponding to the chosen FL with TO weight at
brake release point and calculate weight overhead destination. (See CALCULATION
S􀀤A􀀯D(􀀑􀀃Ehkk􀀃hm􀀃→􀀃5/ 100 kg
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􀀃0//􀀃􀁎f
6 : Add TO altitude correction 0.5 × 72 × 1.5 = 54 kg (enter 100 kg into table)
7 : Subtract value for step climb correction : 80 kg (enter 100 kg into table)
8 : Calculate corrected weight overheac􀀃cdrshm􀁄shnm􀀃→􀀃47􀀃5//􀀃􀁎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􀀃→􀀃47􀀃7//􀀃􀁎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(􀀃→􀀃802􀀃􀁎f
􀀯􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃􀁄ksdqm􀁄sd􀀃→􀀃47􀀃7//􀀃- 913 = 57 887 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-10 CORRECTION FOR DEVIATION FROM REFERENCE
WEIGHT(􀀃→􀀃5􀀃×􀀃􀀋46􀀑7􀀃- 50) = 46.8 kg
Bnqqdbsdc􀀃􀁄ksdqm􀁄sd􀀃etdk􀀃→􀀃85/􀀃􀁎f
01􀀃9􀀃B􀁄kbtk􀁄sd􀀃􀁄ksdqm􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃→􀀃46􀀃7//􀀃􀁎f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(􀀃→􀀃0􀀃/68􀀃􀁎f
14 : Calculatd􀀃vdhfgs􀀃􀁄s􀀃dmc􀀃ne􀀃gnkchmf􀀃→􀀃45􀀃6//􀀃􀁎f
04􀀃9􀀃B􀁄kbtk􀁄sd􀀃sqho􀀃etdk􀀃→􀀃02􀀃1//􀀃􀁎f
05􀀃9􀀃Rtasq􀁄bs􀀃“Dm􀀃Qntsd”􀀃qdrdqud􀀃􀀋rs􀁄mc􀁄qc􀀃􀁄lntms􀀃hr􀀃4􀀃􀀈􀀃ne􀀃sqho􀀃etdk(􀀃→􀀃55/􀀃􀁎f
06􀀃9􀀃B􀁄kbtk􀁄sd􀀃ydqn􀀃etdk􀀃vdhfgs􀀃→􀀃45􀀃///􀀃􀁎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 26/42
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 • 1
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 • 6
9 + DESCENT correction (including 6 min IFR) + 0 • 2
10 (2) Landing Weight at Destination = 5 8 • 8
11 - ALTERNATE Fuel - 1 • 0
12 = ALTERNATE Landing Weight = 5 7 • 8
13 - HOLDING - 1 • 1
14 = Weight at END OF HOLDING = 5 6 • 7
15 TRIP FUEL (1) - (2) 1 3 • 2 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 0 • 7
17 (3) ZERO FUEL WEIGHT = 5 6 • 0
　
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