JORA aircraft is a two seat ultra light Airplane,
with upper placed wings and front engine, two seats side by Side,
and tail surface type T. Undercarriage is boward, has three
wheels, the wheels of the main undercarriage are braked, bow wheel
is operated, resilience is executed by indio-rubber blocks.
All wooden parts are affixed by paste Chs-Epoxy 371. Polyester fabric
facing is affixed by contact paste Chemopren 140. Glassy-laminate
is from epoxide resin Chs-Epoxy 512 or L 285 with glassy reinforce
Vertex.
The wing is divided in the middle between two half, both of the half are
connected to the Centroplane by pegs and they are supported by
fraces. Bearing part of the wing is created by torsion case, which
is consisted of wooden girder and laminate cover. Strips of the
girder are made from spruce wood, standing from birch or beech
plywood. Form stableness is safed by foam polyester ribs. The ribs
which create back part of the wing are sticked from spruce Listels.
Back part cover of the wing is from polyester fabric.
Flaperons which have the function both of winglets and uplift lids have
the same construction as the wing. They are found at all wing span
and they are turningly put at altogether 10 hangings.
Tail areas are T type. Its construction is similar like wing
constriction.
Fuselage is all laminate, armored by several ribs. Engine bed and front
wheel leg are fastened to engine partition made from plywood,
astringent crew seats are fastened on pilot s partition, there are
two wooden ribs in the back part, these ribs armor the keel.
Centroplane is riveted together from duralumin bugles, crew space
is covered by transparent case from non-splintering material.
There is laminate reservoir sticked under the seats. This
reservoir has conductive graphite layer on its inward surface.
Undercarriage is forward
with three wheels. Swing
arms of the main undercarriage are concocted from steel bugles and
they are kept by pull which is finished by rubber stirrup.
The wheels are equipped disk brakes which are operated
mechanically by
little lever on driving lever.
Forward wheel is turning, its operating is connected to leg-rage and it is also
resilianced by rubber stirrup.
Driving unit is consisted from two-cylinder two-stroke engine Rotax with
mechanical gearbox. The
propeller is two-blade wooden or composition.
Driving is doubled, driving lever is found in the middle between the
seats - one for both pilots. When the airplane is used for
training, the driving lever is forked in upper part, leg driving
has doubled pedals. The lids are operated by lever placed in upper
part between both pilots.