Standard FAA Airworthiness Certificated Airplane Glider in the Utility Category for spin recovery approved.

Pilot Adjustable Hoffmann HO-V62R right rotation, fine, course, feather pitch adjustments, instant un-feather for fast restarts.

Fowler increases wing area for increased performance in thermal soaring.

Detachable wings for storage or trailering.

Upper and lower effective wing spoilers. Wingspan is 56 feet with the wings forward swept.

12volt, ammeter, T & Bank, fuel quantity, oil pressure gages, Navigation lights, Anti-collision white strobe light.

Easy manipulation flight controls and systems. Adjustable rudder peddles.

Steering tail wheel with a shock absorbing system. 360-degree ground maneuvering free spin tail wheel feature.

Unfeathering the propellor from glides it will go into the fine pitch setting instantly for maximum climb performance if needed.

Lifted for gear swing checks or service work. Engine exhaust and oil temperature gages are by thermocouple.

Down drafted carburetor with cold engine choke control and an internal accelerator and 12volt fuel pump.

Mikron 3-AE 65HP 4 Cycle, Four Cylinder Engine, all 77/80 or better compressions, Cockpit controlled Cowl flaps.

Imported from Czech Republic 1993 (Parts are available with international shipping services)

Roomy and will accommodate tall humans as much as 6'- 5" tall.

Airworthiness Directives compiled with, airframe, engine, propeller log books and documents complete since new will be included.

Fuselage center structure has a low charge hydrogen pressurization system and gage to warn of (unlikely) structure issues.

Folding horizontal stabilizers, elevators for maintenance, storage or trailering.

Great visibility canopy with sun slider blinds.

Retractable landing gear, tail wheel. F.A.A. Approved Spin recovery training aircraft.

No Airman medical certificate required for the motor glider pilots, State DL. or Basic Med. Safe and well-built airplane. Any ?'s