T.O. 1U-10A-1 U-10 A/B/D Flight Manual
U-10 Helio
This manual contains the necessary information for
safe and efficient operation of the U-10A and U-10B
aircraft. These instructions provide you with a
general knowledge of the aircraft, its characteristics,
and specific normal and emergency operating procedures.
Your flying experience is recognized, and
therefore, basic flight principles are avoided.
Instructions In this manual are for a crew inexperienced
in the operation of this aircraft. This manual
provides the best possible operating instructions
under most circumstances, but it is a poor substitute
for sound judgment. Multiple emergencies,
adverse weather, terrain, etc. may require modification
of the procedures.
The aircraft is a single engine, high wing, five place
monoplane, except aircraft coded D which is six
place, manufactured by Helio Aircraft Corporation of
Bedford, Mass. This all-metal (except for fabric covered
ailerons) aircraft is designed as a liaison and light cargo aircraft to be operated from moderately
rough, unprepared fields requiring short field takeoff
and landing capabilities . The aircraft is characterized
by a large, full cantilever wing and a forward
mounted fixed landing gear . The fixed gear may be
replaced by a twin float. Power Is provided by a
Lycoming six-cylinder, normally -aspirated engine
driving a three-bladed Hartzell propeller. Dual flight
controls are provided. Dual brakes are provided on
aircraft coded A1, D . Aircraft coded A, B, B3
shall be landed and taken off only from the pilot's
seat since the wheel brakes can be operated only from
that position.
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