5-3
VELIS Electro
Pilot's Operating Handbook
POH-128-00-40-001
PAGE REV. 0
PAGE
SECTION 5
PERFORMANCE DATA
APPROVED
5.1 INTRODUCTION
The performance tables and diagrams on the following pages show the per-
formance of the airplane. The data presented in these tables and diagrams
has been derived from test–flights using an airplane, motor and batteries
in good operating condition, and was corrected to standard atmospheric
conditions 15˚ C and 1013.25 mb at sea level.
The performance tables do not take into account the expertise of the pilot
or the maintenance condition of the airplane. The performance illustrated in
the tables can be achieved if the indicated normal procedures are followed
and the airplane is maintained properly.
The energy consumption during cruise is based on propeller RPM and pow-
er settings. Some undefined variables such as the batteries state of health,
contamination of the aircrafts surface, or turbulence could influence flight
distance and flight duration. For this reason, it is of utmost importance that
all available data is used when calculating the range and endurance.
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