SC-POH-1-1-17
SECTION 7
DESCRIPTION OF
AIRPLANE AND SYSTEMS
Revision: -
Date of issue: 2011-09-01
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7. DESCRIPTION OF AIRPLANE AND SYSTEMS
7.1 General
This section provides description and operation of the aircraft and its systems.
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aircraft is a single-engine, all metal, low-wing monoplane of
semi-monocoque structure with two side-by-side seats. The airplane is
equipped with a fixed tricycle undercarriage with castering nose wheel.
Some parts of airplane are made from fiberglass laminate.
7.2 Airframe
All-metal construction, stressed skin, single curvature metal skins riveted to
stiffeners. Construction is of 6061-T6 aluminum sheet metal riveted to
aluminum angles with Avex rivets. This high strength aluminum alloy
construction provides long life and low maintenance costs thanks to its
durability and corrosion resistance characteristics.
The wing has a high lift airfoil equipped with flaps.
7.3 Flight controls
The plane is equipped with a dual stick control, the adjustable rudder pedals
with pedal hydraulic brakes for easy ground control of the castering nose
wheel.
Lateral and longitudinal control movement is transferred by mechanical
system of pull rods and levers.
Rudder control is controlled by pedals of foot control. The rudder is
interconnected with foot control pedals by cable system.
The elevator and aileron trims are electrically actuated by buttons on the
control stick.
Wing flaps are electrically actuated by the rocker switch located on the middle
panel.
