曝光台 注意防骗
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SAD(Ehkkhm→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)
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(→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→476//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
0/9Bkbtksdkmchmfvdhfgsscdrshmshnm→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(→873f
mchmfvdhfgssksdqmsd→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
Bnqqdbsdcksdqmsdetdk→0//1f
019Bkbtksdksdqmsdkmchmfvdhfgs→47///f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(→0/87f
039Bkbtksdvdhfgssdmcnegnkchmf→451//kg
049Bkbtksdsqhoetdk→02///f
059Rtasqbs“DmQntsd”qdrdqudrsmcqclntmshr4nesqhoetdk(→54/f
069Bkbtksdydqnetdkvdhfgs→451//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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A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(39)