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1.4
Descriptive data
1.4.1
Aeroplane description
UFM - 13 ultralight aeroplane is intended for recreational and
cross-country flying. It is not approved for aerobatic operation.
UFM - 13 is
a single engine, all-
fibreglass aeroplane
with
two
side-by-
side
seats.
aeroplane
equipped with fixed
two
main
wheel
undercarriage with a
steer able tail wheel.
The fuselage is a
fibreglass shell with
fibreglass
seats
integrated.
Safety
belts are attached to
the seats and to a
shelf intended for
putting off lightweight objects (headphones, maps, etc.).
The wing is a monospar construction with a sandwich skin com-
posed of two layers of fibreglass and special foam. Control surfaces and
empennage is of the same construction.
The aeroplane is controlled by dual push-pull control system, only
rudder drive is controlled by cable. The ailerons and elevator are controlled
by the control stick located between the pilot's legs (co-pilot's). The rudder
is controlled by the rudder pedals, flaps are operated by a control lever
located between the pilots on the fuselage main spar.
Date of Issue: 30. 1. 2008
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1-4
- Quick Links:
- Airspeed
- Weight
- Performance
- Weight and Balance
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