曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

A318/A319/A320/A321 FLEET PER-FPL-FLP-CAT P 17/42
FCOM 19 AUG 10
Note: Line 3 : temperature correction :
0.015 (kg/°C/NM) × ◂ISA (°C) × air distance (NM)
Line 6 : TO altitude correction :
0.5 (kg/1 000 kg/1 000 ft) × TOW (1 000 kg) × airport elevation (1 000 ft).
Line 10 : Check that landing weight at destination is lower than maximum landing
weight.
Line 17 : Check that the zero fuel weight is lower than maximum zero fuel weight.
Line 22 : Check that the block fuel value is lower than maximum tank capacity.
EXAMPLE
Applicable to: MSN,
DATA
‐ TO weight : 72 000 kg
‐ Ground distance to destination : 2 000 nm
‐ Wind : –50 kt (head wind)
‐ Selected initial FL : 350
‐ Mach number : M .78
‐ Temperature : ISA +10
DETERMINATION OF CRUISE FUEL AND TIME
A : Enter the chosen flight Mach number, flight level, ground distance to be covered and
forecast windspeed in the calculation table (See CALCULATION TABLE).
Calculate the air distance (Refer to PER-OPD-CON-AEO M.78)
here : M .78, 50 kt head wind, 2 000 nm ground distance
→􀀃􀁄hq􀀃chrs􀁄mbd􀀃9􀀃1􀀃137􀀃ml
CRUISE TABLE FL350
B : Read from integrated cruise table (M .78, FL 350) the values for time and distance for
a weight of 72 000 kg (Refer to PER-FPL-FLP-ICR-20 INTEGRATED CRUISE - M.78
FL350) :
→􀀃chrs􀁄mbd􀀃9􀀃5􀀃478􀀃ml􀀃→􀀃shld􀀃9􀀃768􀀃lhm
C : Read from Refer to PER-FPL-FLP-ALT-10 CRUISE LEVEL CHARTS the value for the
optimum aircraft weight to proceed􀀃sn􀀃E􀀯􀀃28/􀀃→􀀃51􀀃///􀀃􀁎f
D : Enter integrated cruise table (M .78, FL 350) and read the values for a weight of
62 000 kg (begin of first step climb)
→􀀃chrs􀁄mbd􀀃9􀀃3􀀃6/2􀀃ml􀀃→􀀃shld􀀃9􀀃517􀀃lhm
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 18/42
FCOM 19 AUG 10
E : Calculate the values for the first cruise segment :
Fuel : 72 000 – 62 000 = 10 000 kg
Distance : 6 589 – 4 703 = 1 886 nm
Time : 879 – 628 = 251 min
Remaining distance : 2 248 – 1 886 = 362 nm
CRUISE TABLE FL390
F : Read from integrated cruise table (M .78, FL 390) the values for time and distance for
the weight of 62 000 kg (Refer to PER-FPL-FLP-ICR-20 INTEGRATED CRUISE - M.78
FL390)
→􀀃chrs􀁄mbd􀀃9􀀃4􀀃/73􀀃ml􀀃→􀀃shld􀀃9􀀃571􀀃lhm
G : Subtract remaining distance : 5 084 – 362 = 4 722 nm
H : Interpolate in integrated cruise table (M .78, FL 390) the weight and time values
corresponding to the distance of 4 722 nm
→􀀃vdhfgs􀀃9􀀃5/􀀃1//􀀃􀁎f􀀃→􀀃shld􀀃9􀀃523 min
I : Calculate values for the second cruise segment :
Fuel : 62 000 – 60 200 = 1 800 kg
Distance : 5 084– 4 722 = 362 nm
Time : 682– 633 = 49 min
Crosscheck that remaining air distance equals zero.
J : Fill in the final table with weight overhead departure (72 000 kg) and weight overhead
destination (60 200 kg).
K : Calculate total values :
Fuel : 72 000 – 60 200 = 11 800 kg
Time : 251 + 49 = 300 min = 5 h
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 19/42
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 20/42
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
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機組操作手冊FLIGHT CREW OPERATING MANUAL 6(38)