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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 35/42
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􀀃→􀀃5/􀀃011􀀃􀁎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􀀃///􀀃􀁎f
6 : Add TO altitude correction 0.5 × 72 × 1.5 = 54 kg (enter100 kg into table)
7 : Subtract value for step climb correction : 60 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(􀀃→
200 kg
0/􀀃9􀀃B􀁄kbtk􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃cdrshm􀁄shnm􀀃→􀀃47􀀃8//􀀃􀁎f
11 : Subtract alternate fuel, e.g. : 100 nm at FL 100
(Refer to PER-FPL-FLP-ALN-20 ALTERNATE PLANNING ISA(􀀃→􀀃802􀀃􀁎f
􀀯􀁄mchmf􀀃vdhfgs􀀃􀁄s􀀃􀁄ksdqm􀁄sd􀀃→􀀃47􀀃8//􀀃- 913 = 57 987 kg
Correction due to deviation from reference landing weight at alternate (Refer to
PER-FPL-FLP-ALN-20 ALTERNATE PLANNING ISA) →􀀃5􀀃×􀀃􀀋47􀀑/􀀃- 50) = 48 kg
Bnqqdbsdc􀀃􀁄ksdqm􀁄sd􀀃etdk􀀃→􀀃850􀀃􀁎f
01􀀃9􀀃B􀁄kbtk􀁄sd􀀃􀁄ksdqm􀁄sd􀀃k􀁄mchmf􀀃vdhfgs􀀃→􀀃46􀀃8//􀀃􀁎f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(􀀃→􀀃0􀀃/82􀀃􀁎f
03􀀃9􀀃B􀁄kbtk􀁄sd􀀃vdhfgs􀀃􀁄s􀀃dmc􀀃ne􀀃gnkchmf􀀃→􀀃45􀀃7//􀀃􀁎f
15 : Calculate trip fuek􀀃→􀀃02􀀃0//􀀃􀁎f
05􀀃9􀀃Rtasq􀁄bs􀀃“Dm􀀃Qntsd”􀀃qdrdqud􀀃􀀋rs􀁄mc􀁄qc􀀃􀁄lntms􀀃hr􀀃4􀀃􀀈􀀃ne􀀃sqho􀀃etdk(􀀃→􀀃544􀀃􀁎f
06􀀃9􀀃B􀁄kbtk􀁄sd􀀃ydqn􀀃etdk􀀃vdhfgs􀀃→􀀃45􀀃0//􀀃􀁎f
18-19: Subtract dry operating weight to obtain maximum allowable payload.
20-22: Calculate ramp fuel (Refer to PER-FPL-GEN-MFR MINIMUM RECOMMENDED FUEL
REQUIREMENTS for taxi fuel).
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 36/42
FCOM 19 AUG 10
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 • 0
6 + TO Altitude correction + 0 • 1
7 - STEP CLIMB correction - 0 • 1
8 = Corrected Weight Overhead Destination = 5 8 • 7
　
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