Pilot Operating Handbook
Cavalon
SECTION 6
WEIGHT AND BALANCE
AutoGyro_POH_Cavalon 915iS
Revision 1.0 – Issue Date 08.MAY.2019
5-1
SECTION 5 - PERFORMANCE
The following data were determined by flight testing and demonstrated with average piloting
skills, with engine and aircraft in good condition, as well as clean main rotor and propeller.
The parameters apply to standard conditions (15 °C at sea level and standard pressure)
and a gross mass of 500 kg.
Note that operation at 560kg MTOW, a higher airfield elevation, increased temperature and
low air pressure will have a negative effect on performance.
5.1
Demonstrated Operating Temperature
Satisfactory engine cooling has been demonstrated at outside air temperatures up to 40 °C.
5.2
Airspeed Correction
Example
: Indicated airspeed of 140 km/h represents a calibrated airspeed (corrected for
installation error) of 138 km/h.
