曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
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
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→ 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)
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 (enter100 kg into table)
7 : Subtract value for step climb correction : 90 kg (enter 100 kg into table)
8 : Calculate corrected weight overhdccdrshmshnm→471//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→473//f
11 : Subtract alternate fuel, e.g. : 100 nm at FL 100
(Refer to PER-FPL-FLP-ALN-20 ALTERNATE PLANNING ISA(→0/82f
mchmfvdhfgssksdqmsd→473//- 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(→4×462- 60) = –13.5 kg
Bnqqdbsdcksdqmsdetdk→0/7/f
019Bkbtksdksdqmsdkmchmfvdhfgs→462//f
13 : Subtract holding fuel (Refer to PER-HOL-GEN GENERAL(→002/f
14 : Calculate weight at endnegnkchmf→451//f
049Bkbtksdsqhoetdk→025//f
059Rtasqbs“DmQntsd”qdrdqudrsmcqclntmshr4nesqhoetdk(→57/f
069Bkbtksdydqnetdkvdhfgs→444//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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(47)