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PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A318/A319/A320/A321 FLEET PER-TOF-TOD-40-30 P 1/10
FCOM 19 AUG 10
HOW TO PROCEED
HOW TO PROCEED
Applicable to: ALL
1. Enter the first table with runway length, slope and wind data. Determine the corrected runway
length by applying the corrections due to slope and wind.
2. Select the configuration as a function of this corrected runway length.
3. Enter the table(s) corresponding to the configuration and airport pressure altitude.
As far as airport pressure altitude is concerned, two methods may be applied :
interpolate the takeoff performance by using the two tables enclosing ‐ the airport pressure
altitude,
‐ for a more conservative figure, use the table corresponding to the pressure altitude immediately
above the airport pressure altitude.
4. Enter the appropriate column of the table(s) with the corrected runway length.
Once again, two methods may be applied :
‐ interpolate the takeoff performance between the two columns enclosing the corrected runway
length,
‐ for a more conservative figure, use the column corresponding to the shorter corrected runway
length.
5. Determination of maximum takeoff weight.
Enter the table(s) and column(s) as explained above with the actual OAT and read maximum
takeoff weight, limitation codes, V1, VR and V2. If necessary interpolate weight and speeds.
6. Determination of flexible temperature.
The determination of flexible temperature is possible only when there is no obstacle on the flight
path. Enter the table(s) and column(s) with the actual takeoff weight and read the corresponding
temperature as flexible temperature.
7. In case of obstacles, use the graphs (Refer to PER-TOF-TOD-50 INTRODUCTION ) to determine
the corresponding weight penalty.
LIMITATION CODES
Applicable to: ALL
‐ 1 : first segment
‐ 2 : second segment
‐ 3 : runway
‐ 5 : tire speed
‐ 6 : brake energy
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A318/A319/A320/A321 FLEET PER-TOF-TOD-40-30 P 2/10
FCOM 19 AUG 10
‐ 7 : maximum computation weight
‐ 8 : final takeoff
‐ 9 : VMU
Note: 1. Limitation code 4 (obstacles) does not appear in quick reference tables.
2. VMC limitation appears with an asterisk (*) in the chart.
CORRECTIONS FOR WIND AND RUNWAY SLOPE
Applicable to:
Runway length (ft) 5 000 6 000 7 000 8 000 9 000 10 000 11 000 12 000
Effect
of wind
per knot of head
wind add (feet) 23 24 27 31 33 37 40 43
per percent
uphill slope
subtract (feet)
540 760 985 1 205 1 425 1 645 1 865 2 085
Effect of
runway slope per percent
downhill slope
add (feet)
60 82 108 133 157 185 209 233
CORRECTIONS FOR WIND AND RUNWAY SLOPE
Applicable to: MSN,
Runway length (m) 1 500 1 750 2 000 2 250 2 500 2 750 3 000 3 250 3 500
Effect
of wind
per knot of head
wind add (meters) 6.5 7 8 8.5 9.5 10 11 11.5 12.5
per percent
uphill slope
subtract (meters)
Effect of 160 215 270 325 380 435 490 545 600
runway
slope per percent
downhill slope
add (meters)
17 23 29 36 42 48 55 61 67
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A318/A319/A320/A321 FLEET PER-TOF-TOD-40-30 P 3/10
FCOM 19 AUG 10
CORRECTIONS FOR WIND AND RUNWAY SLOPE
Applicable to:
Runway length (m) 1 500 1 750 2 000 2 250 2 500 2 750 3 000 3 250 3 500
Effect
of wind
per knot of head
wind add (meters) 6.5 7 8 8.5 9.5 10 11 11.5 12.5
per percent
uphill slope
subtract (meters)
Effect of 160 215 270 325 380 435 490 545 600
runway
slope per percent
downhill slope
add (meters)
17 23 29 36 42 48 55 61 67
CORRECTIONS FOR WIND AND RUNWAY SLOPE
Applicable to: ,
, MSN,,
Runway length (m) 1 500 1 750 2 000 2 250 2 500 2 750 3 000 3 250 3 500
Effect
of wind
per knot of head
wind add (meters) 6 7.5 8 8.5 9.5 10 11 11.5 12.5
per percent
uphill slope
subtract (meters)
Effect of 100 150 200 280 375 475 600 725 820
runway
slope per percent
downhill slope
add (meters)
15 15 18 23 23 28 28 30 30
EXAMPLE
Applicable to:
Pressure altitude : 1 400 ft
Temperature : 30 °C
Runway length : 2 750 m
Wind : 10 kt head
Slope : 1 % up
Takeoff configuration: 1 + F
DETERMINATION OF CORRECTED RUNWAY LENGTH
(Refer to PER-TOF-TOD-40-30 CORRECTIONS FOR WIND AND RUNWAY SLOPE)
　
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