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MANNED AVIATION DOMAIN

Manned Light Sport Aircraft

Featuring an autoclave-cured prepreg carbon fiber composite airframe, our two-seat light aircraft is optimized for pilot training, border observation, and general aviation flight operations.

PREPREG CARBON COMPOSITE AIRFRAME

Aerodynamic Precision & Safety

Designed with high structural safety margins, the composite monocoque fuselage delivers outstanding fuel efficiency, smooth handling, and low operating costs for flight schools and private pilots.

290 kgEmpty Weight
215 km/hCruise Speed
Rotax 912100 HP Engine
Teknosis Manned Light Aircraft

>_ LIGHT AIRCRAFT TECHNICAL SPECIFICATIONS

Aircraft CategoryLight Sport Aircraft (LSA) / Ultralight Manned Aircraft
Airframe Material100% Autoclave Prepreg Carbon Fiber & Kevlar Composite
Engine ModelRotax 912 ULS (100 HP) Aviation Engine
Cockpit Configuration2-Seat Side-by-Side Ergonomic Layout
Empty Weight290 kg
Max Takeoff Weight (MTOW)600 kg
Cruise Speed215 km/h
Certification StandardASTM F2245 Light Sport Aircraft Standard

Autoclave Cured

Monocoque carbon fiber fuselage cured at 250 °C for maximum structural strength and low empty weight.

Safety Certified

Designed strictly to ASTM F2245 light sport aircraft safety standards with dual flight control columns.

Fuel Efficiency

Aerodynamically refined wing profile enabling low fuel burn and long cross-country cruising ranges.

Avionics Integration

Ergonomic glass cockpit layout compatible with modern Garmin & Dynon digital flight displays.