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Airborne Avenger

From Wikipedia, the free encyclopedia
Ultralight aircraft

Avenger
An Avenger in flight
General information
TypeUltralight aircraft
National originUnited States
ManufacturerAirborne Wing Design
StatusProduction completed

TheAirborne Avenger is an Americanultralight aircraft that was designed and produced byAirborne Wing Design in the early 1980s. The aircraft was supplied as a kit foramateur construction.[1]

Design and development

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With three-axis controls, the Avenger was intended to appeal to conventional light aircraft pilots and was designed to comply with the USFAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The Avenger's standard empty weight is 252 lb (114 kg). It has astrut-bracedhigh-wing, single-seat, open cockpit, singlepusher engine configuration, and is equipped withtricycle landing gear usingnosewheel steering.[1][2]

The aircraft is made from bolted-togetheraluminium tubing, with the wings and tail covered inDacron sailcloth. Thefuselage consists of a single aluminium keel tube that runs from the tail surfaces to the nose wheel. The cockpit is an open seat bolted to the main keel tube. Its 31 ft (9.4 m) span wing has an 80% double surface and features half-spanailerons. The wing is supported by dual parallellift struts withjury struts. The tricycle landing gear haspneumatic shock suspension and the nosewheel is steerable. There is also a small tailcaster as the aircraft sits on its tail with no occupant in the pilot's seat. The landing gear has notably high ground clearance for rough field operations and the engine, mounted on the wingtrailing edge, drives a propeller that is protected by the low-mounted tailboom. The standard engine supplied was theCuyuna 430 of 30 hp (22 kW).[1]

Available as either a kit forhome construction or as a complete aircraft,[2] the Avenger was introduced in the early 1980s when the market was becoming saturated with ultralight designs; as a result, the company quickly went out of business and production ended.[1]

Specifications

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Data from Cliche[1] and Jane's[2]

General characteristics

  • Crew: one
  • Length: 17 ft 0 in (5.18 m)
  • Wingspan: 31 ft 0 in (9.45 m)
  • Wing area: 135 sq ft (12.5 m2)
  • Aspect ratio: 7:12
  • Empty weight: 252 lb (114 kg)
  • Max takeoff weight: 552 lb (250 kg)
  • Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal)
  • Powerplant: 1 ×Cuyuna 430 two-cylinder piston snowmobile engine, 30 hp (22 kW)
  • Propellers: 2-bladed wooden

Performance

  • Maximum speed: 60 mph (97 km/h, 52 kn)
  • Cruise speed: 45 mph (72 km/h, 39 kn)
  • Stall speed: 16 mph (26 km/h, 14 kn)
  • Never exceed speed: 70 mph (110 km/h, 61 kn)
  • Rate of climb: 700 ft/min (3.6 m/s)
  • Wing loading: 4.09 lb/sq ft (19.95 kg/m2)

References

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  1. ^abcdeCliche, Andre:Ultralight Aircraft Shopper's Guide 8th Edition, page E32. Cybair Limited Publishing, 2001.ISBN 0-9680628-1-4
  2. ^abcTaylor, John W. (ed.):Jane's All The World's Aircraft 1983-1984 Edition, page 653. Franklin Watts, 1983.ISBN 0-7106-0789-X

External links

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Retrieved from "https://en.wikipedia.org/w/index.php?title=Airborne_Avenger&oldid=1321148525"
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