5.1 Introduction
Section 5 provides data for airspeed calibration, stall speeds, take-off
performance and additional information.
The presented data has been computed from actual flight tests with the
aircraft and engine in good conditions and using average piloting
techniques.
If not stated otherwise, the performance stated in this section is valid for
maximum take-off weight and under ISA conditions.
The performance shown in this section is valid for aircraft fitted with given
engine ROTAX 912 ULS 98.6 hp with WOODCOMP Klassic 170/3/R or
EFFie 170/3/RF propeller.
