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  2. Spar (aeronautics) - Wikipedia

    en.wikipedia.org/wiki/Spar_(aeronautics)

    Main spar of a de Havilland DH.60 Moth. In a fixed-wing aircraft, the spar is often the main structural member of the wing, running spanwise at right angles (or thereabouts depending on wing sweep) to the fuselage. The spar carries flight loads and the weight of the wings while on the ground.

  3. AeroCad AeroCanard - Wikipedia

    en.wikipedia.org/wiki/AeroCad_AeroCanard

    The AeroCanard line of aircraft all feature a cantilever mid-wing, a canard tail, a four seat enclosed cabin and a single engine in pusher configuration. The tricycle landing gear features either fixed main wheels and a retractable nose wheel or fully retractable gear, depending on the model. [1] [2] The aircraft is made from composites.

  4. Dallach Sunrise - Wikipedia

    en.wikipedia.org/wiki/Dallach_Sunrise

    The wing has a nose made of fiberglass. The main spar is built from CFK. The Sunrise has a fixed tailwheel undercarriage, with the mainwheels hinged from the fuselage on V-form, cross-connected struts. Some Sunrises have wheel fairings. [1] The Sunrise can be powered by one of several engines in the 28-66 kW (38-90 hp) power range. [2]

  5. Applebay Zia - Wikipedia

    en.wikipedia.org/wiki/Applebay_Zia

    The Applebay Zia is an American, single-seat, high-wing, twin-boom, pusher configuration motor glider that was designed by George Applebay for the 1982 Sailplane Homebuilders Association Homebuilt Sailplane Design Contest. The aircraft was intended to be offered as a factory completed aircraft or as a kit. [1] [2] It first flew in 1982. [3]

  6. Alisport Silent 2 - Wikipedia

    en.wikipedia.org/wiki/Alisport_Silent_2

    Alisport Silent 2. The fuselage is carbon and glass fiber composite with epoxy resin. The wings have an elliptical planform, vertical or elliptical design winglets. The wing structure includes extensive use of carbon fiber, both in the sandwich skins and in the tapered I-beam wing spar which uses pultruded carbon rods for the spar caps.

  7. Murphy Renegade - Wikipedia

    en.wikipedia.org/wiki/Murphy_Renegade

    The lower wing has 3 degrees of dihedral. Ailerons are of the Friese type, with two ailerons on the lower wing standard and four ailerons optional. The front wing spar was initially a 3 in (7.6 cm) aluminum tube and the rear spar is "C" channel. Starting 1 January 1989 the front spar was changed to a rectangular spar and an outboard drag brace ...

  8. Schweizer SGS 2-33 - Wikipedia

    en.wikipedia.org/wiki/Schweizer_SGS_2-33

    The 2-33 retained the 2-22 and 1-7's metal wing, single spar and single strut arrangement. [1] [2] [5] The 2-33 was manufactured in three variants and remained in production for 14 years. Production was only curtailed when demand dropped off due to the import of higher-performance two-place sailplanes from Europe. [3]

  9. Preceptor N3 Pup - Wikipedia

    en.wikipedia.org/wiki/Preceptor_N3_Pup

    Data from Manufacturer's website & Kitplanes General characteristics Crew: one Length: 16 ft 6 in (5.03 m) Wingspan: 30 ft 6 in (9.30 m) Height: 5 ft 0 in (1.52 m) Wing area: 120 sq ft (11 m 2) Empty weight: 254 lb (115 kg) Gross weight: 535 lb (243 kg) Fuel capacity: 5 US Gallons (19 litres) Powerplant: 1 × Hummel Half VW 1037 cc four-stroke, two-cylinder horizontally opposed aircraft engine ...