A single-seat parasol-wing LSA microlight first flown in 1986. Fitted with detachable wings. The kit price in 1997 was US$6884 and plans US$150. In 2007 the kit price was US$9993 and plans US$250.
Speed max: 63 mph. Cruise: 59 mph. Range: 120 sm. Stall: 24 mph. ROC: 800 fpm. Take-off dist: 50 ft. Landing dist: 200 ft. Service ceiling: 12,000 ft. Engine: Rotax 277, 28 hp. HP range: 28-40. Fuel cap: 5 USG. Weight empty: 240 lbs. Gross: 500 lbs. Height: 5.25 ft. Length: 16.33 ft. Wing span: 28 ft. Wing area: 112 sq.ft. Seats: 1. Landing gear: tail wheel. Cockpit width: 23.6 in
A single-seat, LSA legal high-wing microlight. With detachable wings, the J-3 Kitten first flew in 1986. The kit price in 1997 was US$6684 and plans US$100. By 2007 the kit price was US$10,893.
Speed max: 63 mph. Cruise: 59 mph. Range: 120-140 sm. Stall: 24 mph. ROC: 800 fpm. Take-off dist: 50 ft. Landing dist: 200 ft. Service ceiling: 12,000 ft. Engine: Rotax 277, 28 hp. HP range: 28-40. Fuel cap: 5 USG. Weight empty: 254 lbs. Gross: 500 lbs. Height: 5.25 ft. Length: 16.3 ft. Wing span: 30 ft. Wing area: 120 sq.ft. Seats: 1. Landing gear: tail wheel. Cockpit width: 23.6 in
Established in 1984. Offers plans and kits to construct J-3 Kitten single-seat high-wing microlight and higher-powered J-5 Super Kitten, plans and kits for J-4 Sportster single-seat parasol-wing microlight and more-powerful Super Sportster, and kits for Reliant single-seat high-wing microlight and morepowerful Reliant SX. 1995-7: PO Box 266, Saluda, NC 28773, USA.
High monowing, strut-braced, Kevlar/foam construction. Full three-axis control system. Powered by a WAE two-cylinder horizontally opposed British microlight engine. The landing gear was Chrome-moly steel, trike type.
After spending something like $200k developing the aircraft and all the tooling, the original designers found they couldn’t obtain product liability insurance and they decided to sell the project to someone who was going to manufacture it in Mexico. That never came to.
Only 10 came out of the factory.
Engine: WAE 2 cyl, 30 hp Wingspan 31 ft Wing area 112 sq.ft Length 18 ft Empty weight 245 lb Payload 245 lb Gross 600 lb Wing loading 4 lbs/sq.ft L/D 22:1 Cruise speed 60 mph Stall speed 19 mph Vmax 63 mph Climb rate 1000 fpm Takeoff run 150-200 ft Landing roll 150-200 ft Fuel capacity 5 USG
Receiving the “Best New Design” award at Oshkosh 1984 the Buccaneer was a conventional double-surface high-wing, three-axis control ultralight. Powered by a Rotax 277 single-cylinder, it came in three models — open framework, pod, and retractable amphibian. The landing gear was taildragger, or retractable/amphibian, using reinforced fiberglass hull & sponsons. Centre mounted joy stick, rudder pedals, tailwheel steerable through rudder pedals. Later marketed by Keuthan Aviation as the Buccaneer SX and Buccaneer II, and by Arnet Pereyra Inc as the Aventura 1 HP/A and Aventura II A. A modified version, retrofitable to Buccaneers was marketed by Advanced Aeromarine as the Mallard. The Mallard was available as a conversion for existing Buccaneers or as a complete kit. First flown in 1993. Although produced as an amphibious flying boat, the Buccaneer can be converted to a land plane by removing the boat hull and floats.
The Aero Adventure Aventura II Sport is a new model designed to minimize the expense and complexity of buying, building, and flying a two seat Aventura. With a strong 65 H.P. Rotax 582, the complete kit started at only $33,400. This is by far the most inexpensive two place amphibian on the market. Invest 250 hours of assembly time and this plane will be flying you and a friend anywhere. The 100 H.P. 4-Stroke Rotax 912ULS with its 18 gallon fuel tank allows a solid 3 hours of flight with reserve. $44,900 for the complete kit. The Aventura II XLR has a new engine cowling available, a new graphics package, an amazing new panel with AVMAP’s daylight readable GPS, a VSI, mode-C transponder, and more. Electric gear with indicator lights, differential hydraulic brakes, carpeting, headliner, 600-6 Soft Turf Tires, a 100 H.P. Rotax 912 ULS with an Air Box, a custom stainless steel exhaust, a warp drive 3-blade nickel edge prop and a spinner.
The Arnet Pereyra Buccaneer SX first flew in May 1986. The Arnet Pereyra Buccaneer II first flew in March 1984. The Arnet Pereyra Aventura UL and HP first flew in March 1995. The Arnet Pereyra Aventura II first flew in June 1995.
Buccaneer (Land) Empty wt: 228 lbs. Empty weight (De Luxe) 250 lbs. Wing span: 35 ft. Wing area: 147 sq.ft. Aspect ratio 8:1 Length: 17 ft 6 in Fuel cap; 4.5 USG. Construction: Aluminium, Dacron. Engine: Rotax 277 (268cc) 28hp. Max wt: 500 lbs. Stall speed: 20 mph. Max speed: 51 mph. Vne: 75 mph. Climb rate: 600 fpm @ 28 mph. Design limit: +5, -3.5g. Glide ratio: 8-1. Wing loading: 3.4 lbs/sq.ft. Power loading: 17.86 lbs/hp. Pilot weight category 90-225 lbs all models.