Neither the software nor the documentation may
be used for real aviation and training purposes.
05<01
5.0
PERFORMANCE
5.1.
INTRODUCTION
page
DA20-100 ‘Katana’ 4X Manual
PERFORMANCE
The performance tables and diagrams on the following pages have been
prepared to illustrate the performance you may expect from your airplane
as well as to assist you in precise flight planning. The data presented in
these tables and diagrams has been derived from test-flights using an
airplane and engine in good operating condition, and was corrected to
standard atmospheric conditions (15° C (59° F) and 1013.25 mbar (29.92
in. Hg) 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 procedures are followed and the
airplane is in good maintenance condition. Note that the flight duration data
does not include a fuel reserve. The fuel consumption during cruise is
based on propeller RPM and manifold pressure settings. Some undefined
variables such as the operating condition of the engine, contamination of
the aircrafts surface, or turbulence could have influences on flight distance
and flight duration. For this reason, it is of utmost importance that all
available data is used when calculating the required amount of fuel for a
flight.
For flight operation without wheel fairings the resulting performance
variations is given in %.
Summary of Contents for DA20-100
Page 1: ...MANUAL DA20 100 Katana ...
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