### Calculation Base Assumptions

**Important: There is no guarantee of correctness for the calculated data.** There are too much environmental influences to get a precice mathematical result.

Calculations are based on Fuji FA 200 Manual, which contains values based on **Prop 7656, and 15° flaps on an asphalt runway**.

The original diagram shown in the manual has been interpolated to provide calculations. Therefore a linear relation between Take-off-weight, density altitude and necessary takeoff- / ground rolling distances is assumed. This may not be precice especially for high altitudes or temperatures.