II
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Pilot Operating Handbook
5. PERFORMANCE
The presented data has been computed from actual flight tests with the
aircraft and engine in good cond1t1or.s 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 seciion is valid for aircraft fitted with given
ROTAX 912 ULS
98.6 [hpj (73.5
[kV'l}j engine and
WOODCOMP KLASSIC
17013/R
propeller.
CAUTION
Airspeeds values are valid for standard AV/A T/K WA037383 pitot-static probe.
Date of Issue: 04/2009
Revision: 3.0
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