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temperature and corrected runway length. TREF and TMAX are given at the top of each table. For
pressure altitudes above 2 000 ft, use a specific RTOW chart.
Note: 1. Quick reference tables are established at V1 min (minimum V1 in the V1 range) with air
conditioning OFF and anti ice OFF
2. Do not use quick reference tables in case of tailwind.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
Intentionally left blank
A330/A340 FLEET PER-TOF-TOD-40-20 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A330/A340 FLEET PER-TOF-TOD-40-30 P 1/26
FCOM 19 AUG 10
HOW TO PROCEED
GENERAL
Applicable to:
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 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.
GENERAL
Applicable to: ,
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.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
TAKEOFF DATA - QUICK REFERENCE TABLES
A330/A340 FLEET PER-TOF-TOD-40-30 P 2/26
FCOM 19 AUG 10
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
‐ 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.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TAKEOFF
　
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