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STEPS
09EhkkhmLwSNvdhfgs→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
SAD(Ehkkhm→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)
39Bnqqdbshnmenqknvhqbnmchshnmhmf→gdqd</
5 : Subtract climb correction for chosen FL (Refer to PER-FPL-FLP-ICR-40-A CLIMB
CORRECTION - M.78 and LONG RANGE SPEED(→00//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 overheaccdrshmshnm→475//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
0/9Bkbtksdkmchmfvdhfgsscdrshmshnm→477//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(→802f
mchmfvdhfgssksdqmsd→477//- 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(→5×467- 50) = 46.8 kg
Bnqqdbsdcksdqmsdetdk→85/f
019Bkbtksdksdqmsdkmchmfvdhfgs→467//f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(→0/68f
14 : Calculatdvdhfgssdmcnegnkchmf→456//f
049Bkbtksdsqhoetdk→021//f
059Rtasqbs“DmQntsd”qdrdqudrsmcqclntmshr4nesqhoetdk(→55/f
069Bkbtksdydqnetdkvdhfgs→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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A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(41)