Revision: -
Date of issue: 2011-09-01
SC-POH-1-1-17
SECTION 5
PERFORMANCE
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5. PERFORMANCE
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 takeoff weight
1,320 lb
and under ISA conditions.
The performance shown in this section is valid for aircraft equipped with
ROTAX 912 ULS
engine with maximum power
98.6 hp
and
WOODCOMP
KLASSIC 170/3/R
three composite blades ground adjustable propeller with
pitch setting
17.5°
.
CAUTION
Airspeed values are valid for standard
AVIATIK
WA037383 pitot-static probe
.
