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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 • 2
9 + DESCENT correction (including 6 min IFR) + 0 • 2
10 (2) Landing Weight at Destination = 5 8 • 4
11 - ALTERNATE Fuel - 1 • 1
12 = ALTERNATE Landing Weight = 5 7 • 3
13 - HOLDING - 1 • 2
14 = Weight at END OF HOLDING = 5 6 • 1
15 TRIP FUEL (1) - (2) 1 3 • 6 / / / / / / / / / / / / / / /
16 - "En Route" Reserve - 0 • 7
17 (3) ZERO FUEL WEIGHT = 5 5 • 4
18 - OPERATING WEIGHT EMPTY - 4 8 • 5
19 = Max Allowable Payload = 6 • 9
BLOCK FUEL CALCULATION
20 Required Fuel (1) - (3) ◂ 1 6 • 6
21 + Taxi + 0 • 2
22 = Block Fuel = 1 6 • 8
FLIGHT TIME CALCULATION (H. MIN)
23 Time from integrated Cruise Tables ◂ 5 • 0 1
24 + CLIMB Correction + 0 • 0 4
25 + DESCENT Correction (including 6 min IFR) + 0 • 0 9
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 42/42
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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALT-10 P 1/14
FCOM 19 AUG 10
OPTIMUM AND MAXIMUM ALTITUDES
DEFINITIONS
Applicable to: ALL
• Optimum altitude : The altitude at which the airplane covers the maximum distance per kilogram
(pound) of fuel (best specific range). It depends on the actual weight and deviation from ISA.
• Maximum altitude is defined as the lower of :
maximum altitude at maximum ‐ cruise thrust in level flight and
‐ maximum altitude at maximum climb thrust with 300 ft/min vertical speed.
Note: Definition of the maximum altitude in the FMGC is different (Refer to STLO-22_10_R-40-10
MCDU).
CRUISE LEVEL CHARTS
Applicable to:
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: The n = 1.3 g (1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR 4 000 FT STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 75/165 75/165 74/163 73/160 72/158 69/152
330/370 68/149 68/149 68/149 67/147 66/145 64/141
350/390 61/134 62/136 61/134 61/134 60/132 58/127
BLEED CORRECTIONS
ENGINE ANTI ICE TOTAL ANTI ICE
ISA Max Alt. : - 900 ft
Opt Alt. : No corr.
Max Alt. : -1 500 ft
Opt Alt. : No corr.
ISA +10 Max Alt. : - 900 ft
Opt Alt. : No corr.
Max Alt. : -1 600 ft
Opt Alt. : No corr.
ISA +15 Max Alt. : - 900 ft
Opt Alt. : No corr.
Max Alt. : -1 700 ft
Opt Alt. : No corr.
ISA +20 Max Alt. : -1 700 ft
Opt Alt. : -1 500 ft
Max Alt. : -2 900 ft
Opt Alt. : -2 900 ft
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALT-10 P 2/14
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
FLIGHT PLANNING
FLIGHT PREPARATION - ALTITUDE
A318/A319/A320/A321 FLEET PER-FPL-FLP-ALT-10 P 3/14
FCOM 19 AUG 10
CRUISE LEVEL CHARTS
Applicable to: MSN
These charts have been established for a center of gravity at 33 % MAC.
Maximum and optimum altitudes are given for different temperatures at long range speed and M .78.
Note: The n = 1.3 g (1.4 g) curve indicates the buffet margin.
OPTIMUM WEIGHT FOR 4 000 FT STEP CLIMB
WEIGHT (1 000 kg/1 000 lb)
STEP CLIMB FROM/TO ≤ ISA +10 ISA +15 ISA +20
LR M .78 LR M .78 LR M .78
310/350 82/180 82/180 80/176 80/176 77/169 76/167
330/370 74/163 75/165 73/160 73/160 69/152 69/152
　
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