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Time : 91 + 210 = 301 min = 5 h 01 min
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 39/42
FCOM 19 AUG 10
DATA
‐ TO weight : 72 000 kg
‐ Ground distance to destination : 2 000 nm
‐ Wind : –50 kt (headwind)
‐ Selected first flight level : FL 350
‐ M .78
‐ Temperature : ISA +10 along the whole flight profile
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 40/42
FCOM 19 AUG 10
‐ Airport elevation : 1 500 ft
‐ Normal air conditioning
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􀀃→ 59 730 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 (enter100 kg into table)
7 : Subtract value for step climb correction : 90 kg (enter 100 kg into table)
8 : Calculate corrected weight overhd􀁄c􀀃cdrshm􀁄shnm􀀃→􀀃47􀀃1//􀀃􀁎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􀀃3//􀀃􀁎f
11 : Subtract alternate fuel, e.g. : 100 nm at FL 100
(Refer to PER-FPL-FLP-ALN-20 ALTERNATE PLANNING ISA(􀀃→􀀃0􀀃/82􀀃􀁎f
􀀯􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃􀁄ksdqm􀁄sd􀀃→􀀃47􀀃3//􀀃- 1 093 = 57 307 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-10 CORRECTION FOR DEVIATION FROM REFERENCE
WEIGHT(􀀃→􀀃4􀀃×􀀃􀀋46􀀑2􀀃- 60) = –13.5 kg
Bnqqdbsdc􀀃􀁄ksdqm􀁄sd􀀃etdk􀀃→􀀃0􀀃/7/􀀃􀁎f
01􀀃9􀀃B􀁄kbtk􀁄sd􀀃􀁄ksdqm􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃→􀀃46􀀃2//􀀃􀁎f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(􀀃→􀀃0􀀃02/􀀃􀁎f
14 : Calculate weight at end􀀃ne􀀃gnkchmf􀀃→􀀃45􀀃1//􀀃􀁎f
04􀀃9􀀃B􀁄kbtk􀁄sd􀀃sqho􀀃etdk􀀃→􀀃02􀀃5//􀀃􀁎f
05􀀃9􀀃Rtasq􀁄bs􀀃“Dm􀀃Qntsd”􀀃qdrdqud􀀃􀀋rs􀁄mc􀁄qc􀀃􀁄lntms􀀃hr􀀃4􀀃􀀈􀀃ne􀀃sqho􀀃etdk(􀀃→􀀃57/􀀃􀁎f
06􀀃9􀀃B􀁄kbtk􀁄sd􀀃ydqn􀀃etdk􀀃vdhfgs􀀃→􀀃44􀀃4//􀀃􀁎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 41/42
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 ◂ 5 9 • 7
　
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