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  2. Affordaplane - Wikipedia

    en.wikipedia.org/wiki/Affordaplane

    Data from Ultralight News, Pilot Mix. General characteristics Crew: one Capacity: one (ultralight configuration) Length: 17 ft 3 in (5.26 m) Wingspan: 27 ft 5 in (8.36 m) Height: 5 ft 0 in (1.52 m) varies by main landing gear wheel diameter Wing area: 123 sq ft (11.4 m 2) Empty weight: 254 lb (115 kg) Gross weight: 540 lb (245 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax ...

  3. American Champion Citabria - Wikipedia

    en.wikipedia.org/wiki/American_Champion_Citabria

    Data from Jane's All the World's Aircraft 1969–70 General characteristics Crew: one Capacity: one passenger Length: 22 ft 8 in (6.91 m) Wingspan: 33 ft 5 in (10.19 m) Height: 6 ft 7 + 3 ⁄ 4 in (2.03 m) Wing area: 165 sq ft (15.3 m 2) Aspect ratio: 6.72:1 Airfoil: NACA 4412 Empty weight: 1,037 lb (470 kg) Gross weight: 1,650 lb (748 kg) Fuel capacity: 39 US gal (32 imp gal; 150 L ...

  4. Rans S-12 Airaile - Wikipedia

    en.wikipedia.org/wiki/Rans_S-12_Airaile

    The wings are built from aluminium tube and ribs, feature flaps, and are folding or removable. [ 1 ] [ 2 ] [ 5 ] The present-day S-12XL is powered by the Rotax 503 of 50 hp (37 kW), with the Rotax 582 of 64 hp (48 kW), the Rotax 912UL of 80 hp (60 kW) and the Rotax 912UL of 100 hp (75 kW) available as options.

  5. Murphy Elite - Wikipedia

    en.wikipedia.org/wiki/Murphy_Elite

    The Elite features a strut-braced high-wing, three seats, tricycle landing gear and a single engine in tractor configuration. [1] [2] [5] [6] The aircraft is made from aluminum sheet. Its 30.3 ft (9.2 m) span wing is supported by single lift struts. The occupants are accommodated in an enclosed cabin of 44 in (111.8 cm) width, with doors for ...

  6. InterPlane Skyboy - Wikipedia

    en.wikipedia.org/wiki/InterPlane_Skyboy

    Data from Purdy, Cliche & InterPlane General characteristics Crew: one Capacity: one passenger Length: 20 ft 0 in (6.10 m) Wingspan: 34 ft 5 in (10.49 m) Wing area: 163.6 sq ft (15.20 m 2) Empty weight: 490 lb (222 kg) Gross weight: 1,000 lb (454 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 twin cylinder two-stroke aircraft engine, 64 hp (48 kW) Performance Maximum ...

  7. AAC Angel - Wikipedia

    en.wikipedia.org/wiki/AAC_Angel

    The Angel Aircraft Corporation Model 44 Angel is a twin-engine STOL utility aircraft produced in the United States since the mid-1990s. Designed by Carl Mortenson and The King's Engineering Fellowship to be well-suited for missionary work from remote locations around the world, it is a low-wing cantilever monoplane with a retractable tricycle undercarriage and eight seats.

  8. Wag-Aero CUBy - Wikipedia

    en.wikipedia.org/wiki/Wag-Aero_CUBy

    Data from Sport Aviation, Plane & Pilot and Purdy General characteristics Crew: one Capacity: one passenger in tandem seating Length: 22 ft 5 in (6.83 m) Wingspan: 35 ft 3 in (10.74 m) Height: 6 ft 8 in (2.03 m) Wing area: 178.5 sq ft (16.58 m 2) Airfoil: USA 35B Empty weight: 695 lb (315 kg) Gross weight: 1,400 lb (635 kg) Fuel capacity: 12 US Gallons, 45.42 litres Powerplant: 1 × Lycoming O ...

  9. Aero Designs Pulsar - Wikipedia

    en.wikipedia.org/wiki/Aero_Designs_Pulsar

    The Aero Designs Pulsar is an American two-seat, low wing, ultralight and homebuilt aircraft that was designed by Mark Brown and first produced by Aero Designs of San Antonio, Texas, introduced in 1985. When it was available the Pulsar was supplied as a ready-to-fly aircraft and as a kitplane for amateur construction. [1] [2]