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Main features
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Engine mounting: formed by a framework of steel tubes CrMo 4130 (CRMO 4130); TIG welding TIG.
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Wing profile: biconvex asymmetrical characterized by high lift and weak resistance.
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Wing structure: aluminum spar with anterior antithorsional stern, posterior spar supporting the camping brackets of ailerons and flaps.
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Wing -tips for the reduction of vortexes.
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Structure of tail plane: aluminum spars and ribs.
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Covering of wings and tail planes: realized with aluminum 2017 T4 e 2024 T3, specific for aircraft use, nailed and sticked.
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Joints: the structural joints are nailed and sticked,[1] the non structural joints are riveted.
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Directional control: with steel cables inserted on Teflon guides and pulleys.
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Control of ailerons and elevators: hard rods, on spherical bushes and roll bearings, thus letting high roll rates with limited efforts on the bar.
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Gear: tricycle gear, with 6” shrouded wheels, hardened steel leaf sping, anterior wheel which is controlled by the rudder pedals.
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Braking system: hydraulic braking system with disc brake.
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Series homologated burst protecting tanks.
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Engine: Rotax 912 UL 80 HP or version 100 HP on request.
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Land adjustable pitch prop; variable pitch prop on flight on request.
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Cockpit: width 45,28 ", with wide baggage compartment behind the seats.
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Adjustable safety belts , at four points.
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Ballistic parachute Galaxy on request.
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