SECTION 5
PS-POH-1-1-13
P
P
S
S
-
-
2
2
8
8
C
C
r
r
u
u
i
i
s
s
e
e
r
r
PERFORMANCE
Date: 2015-11-11
5-2
EASA approved Rev. No.: 1
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 600 kg and under ISA conditions.
The performance shown in this section is valid for aircraft equipped with
ROTAX 912 S2 / ULS2 engine with maximum power 73.5 kW and
WOODCOMP KLASSIC 170/3/R three composite blades ground adjustable
propeller with pitch setting 17.5 ±0.5°.
CAUTION
Airspeed values are valid for standard AVIATIK WA037383 pitot-static probe.