Pilot Operating Handbook
Cavalon
SECTION 6
WEIGHT AND BALANCE
AutoGyro_POH_Cavalon 915iS
Revision 1.0 – Issue Date 08.MAY.2019
5-7
5.8
Sink Rate and Glide Ratio
The sink rate depending on airspeed with the engine in idle is plotted in the following
diagram:
In case of an engine failure, expect a glide ratio of 1:3 which corresponds to a vertical
distance of 900 m or 0.5 nautical miles for each 1000 ft.
5.9
Additional Performance Data
5.9.1
Fuel Flow
The following fuel flow figures are provided as estimates and do not constitute certified
performance. Exact fuel flow will vary with environmental conditions, cleanliness of propeller
and rotor, piloting technique (minimum side slip), and power setting. A fuel flow meter is
installed in the aircraft to enable accurate data for the operator.
For additional procedures about proper power setting consult SECTION 9 for supplemental
data concerning the variable pitch propeller, if installed.
Fuel flow at 125 km/h (78mph, 68KIAS) IAS ........................................... 15 ltr/h
Fuel flow at 140 km/h (87mph, 75KIAS) IAS ........................................... 18 ltr/h
5.9.2
Service Ceiling
See SECTION 2 LIMITATIONS