SOLO АС-4



Motorglider AC-5M



Solo AC-5К



SINGLE MOTORGLIDER AC-5К.

 

"АС-5К" - the single glider-paritel equipped with withdrawable and letting out in flight screw-engineinstal lation, providing independent launch, and as if necessary flight continuation in a motor mode in the absence of ascending streams. A fuselage of type "monocook" and as all steering aerodynamic surfaces are made of fiber glass fabric, polyfoam and epoxide pitches. The cabin has the raised safety factor, is equipped regulated, in conformity with growth of the pilot, pedals and a moved back of sitting. The glider wing is executed from the facilitated multilayered composite, on modern technology in precision matrixes with use of curing in vacuum. The wing has scope of 12,6 m and is executed from 2 demountable parts (the left and right consoles) which can be removed for transportation or storage. On the wing ends winglets are located. On the top part of a wing air brakes (inceptors) the sliding design, executed under the scheme "Schempp-Hirth" are placed. The Control system of flight consists of usual management on three axes and managements interceptors, made for management of a trajectory and speed. The wing is equipped by flaps. An elevator, elerons and inceptors cope with the help of metal pipes. Drafts of management by elerons, intercepters and flaps will be automatically connected in an installation time of wings. A metal cable is used for management of a direction wheel. Chassis are equipped with pnevmo-gidroammortizators. The glider "АС-5К" is designed according to the norms which are meeting the requirements of standard JAR-22.
At flight with the engine the screw is coming from a fuselage, but thus the engine remains inside a fuselage. It is the basic difference from glider АС-5М. 
 
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Solo AC-6



Планер двухместный AC-7



Motorglider AC-7М



Motoglider AC-7К