A320机组操作手册FLIGHT CREW OPERATING MANUAL 6(46)

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9 + DESCENT correction (including 6 min IFR) + 0 • 2
10 (2) Landing Weight at Destination = 5 8 • 9
11 - ALTERNATE Fuel - 1 • 0
12 = ALTERNATE Landing Weight = 5 7 • 9
13 - HOLDING - 1 • 1
14 = Weight at END OF HOLDING = 5 6 • 8
15 TRIP FUEL (1) - (2) 1 3 • 1 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 0 • 7
17 (3) ZERO FUEL WEIGHT = 5 6 • 1
18 - OPERATING WEIGHT EMPTY - 3 9 • 2
19 = Max Allowable Payload = 1 6 • 9
BLOCK FUEL CALCULATION
20 Required Fuel (1) - (3) ◂ 1 5 • 9
21 + Taxi + 0 • 2
22 = Block Fuel = 1 6 • 1
FLIGHT TIME CALCULATION (H. MIN)
23 Time from integrated Cruise Tables ◂ 5 • 0 0
24 + CLIMB Correction + 0 • 0 4
25 + DESCENT Correction (including 6 min IFR) + 0 • 1 0
26 = Flight Time = 5 • 1 4
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 37/42
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􀀃3􀀃388􀀃ml􀀃→􀀃shld􀀃9􀀃5//􀀃lhm
C : Read from Refer to PER-FPL-FLP-ALT-10 CRUISE LEVEL CHARTS the value for the
noshltl􀀃􀁄hqbq􀁄es􀀃vdhfgs􀀃sn􀀃oqnbddc􀀃sn􀀃E􀀯􀀃28/􀀃→􀀃57􀀃///􀀃􀁎f
D : Enter integrated cruise table (M .78, FL 350) and read the values for a weight of
68 000 kg (begin of first step climb)
→􀀃chrs􀁄mbd􀀃9􀀃2􀀃700􀀃ml􀀃→􀀃shld􀀃9􀀃4/8􀀃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 38/42
FCOM 19 AUG 10
E : Calculate the values for the first cruise segment :
Fuel : 72 000 – 68 000 = 4 000 kg
Distance : 4 499 – 3 811 = 688 nm
Time : 600 – 509 = 91 min
Remaining distance : 2 248 – 688 = 1 560 nm
CRUISE TABLE FL390
F : Read from integrated cruise table (M .78, FL 390) the values for time and distance for
the weight of 68 000 kg (Refer to PER-FPL-FLP-ICR-20 INTEGRATED CRUISE - M.78
FL390)
→􀀃chrs􀁄mbd􀀃9􀀃3􀀃/58􀀃ml􀀃→􀀃shld􀀃9􀀃435􀀃lhm
G : Subtract remaining distance : 4 069 – 1 560 = 2 509 nm
H : Interpolate in integrated cruise table (M .78, FL 390) the weight and time values
corresponding to the distance of 2 509 nm
→􀀃vdhfgs􀀃9􀀃48􀀃62/􀀃􀁎f􀀃→􀀃shld􀀃9􀀃336 min
I : Calculate values for the second cruise segment :
Fuel : 68 000 – 59 730 = 8 270 kg
Distance : 4 069 – 2 509 = 1 560 nm
Time : 546 – 336 = 210 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 (59 730 kg).
K : Calculate total values :
Fuel : 72 000 – 59 730 = 12 270 kg
　
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