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AmEagle American Eaglet

The AmEagle American Eaglet was a highly unorthodox ultralight sailplane marketed in the U.S. for homebuilding. It was a one-seat, high-wing braced monoplane that carried an inverted V-tail on a long boom extending from a pod-like fuselage. Intended for self-launching, it was equipped with a McCulloch go-kart engine and a folding propeller behind the cabin. Its first flight was on 19 November 1975, and by 1978, at least 250 sets of plans had been sold, with 12 aircraft reportedly completed.

American Eaglet
Role Ultralight sailplane
Manufacturer AmEagle
Designer Larry Haig
First flight 19 November 1975

Specifications

Data from Jane's all the World's Aircraft 1947[1]

General characteristics

  • Crew: 2
  • Length: 22 ft 9 in (6.94 m)
  • Wingspan: 34 ft 4 in (10.47 m)
  • Height: 7 ft 0 in (2.14 m)
  • Wing area: 164.4 sq ft (15.27 m2)
  • Empty weight: 638 lb (289 kg)
  • Gross weight: 1,050 lb (476 kg)
  • Powerplant: 1 × Continental A50 air-cooled, horizontally opposed, four-cylinder piston engine, 50 hp (37 kW)

Performance

  • Maximum speed: 92 mph (148 km/h, 80 kn) * Landing speed: 28 mph (24 kn; 45 km/h)
  • Range: 225 mi (362 km, 196 nmi)
  • Service ceiling: 14,500 ft (4,400 m)
  • Rate of climb: 700 ft/min (3.6 m/s)

See also

Aircraft of comparable role, configuration, and era

References

  1. ^ Bridgman, Leonard, ed. (1947). Jane's all the World's Aircraft 1947. London: Sampson Low, Marston & Co. p. 178c.
  • Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions.


ameagle, american, eaglet, highly, unorthodox, ultralight, sailplane, marketed, homebuilding, seat, high, wing, braced, monoplane, that, carried, inverted, tail, long, boom, extending, from, like, fuselage, intended, self, launching, equipped, with, mcculloch,. The AmEagle American Eaglet was a highly unorthodox ultralight sailplane marketed in the U S for homebuilding It was a one seat high wing braced monoplane that carried an inverted V tail on a long boom extending from a pod like fuselage Intended for self launching it was equipped with a McCulloch go kart engine and a folding propeller behind the cabin Its first flight was on 19 November 1975 and by 1978 at least 250 sets of plans had been sold with 12 aircraft reportedly completed American EagletRole Ultralight sailplaneManufacturer AmEagleDesigner Larry HaigFirst flight 19 November 1975Specifications EditData from Jane s all the World s Aircraft 1947 1 General characteristicsCrew 2 Length 22 ft 9 in 6 94 m Wingspan 34 ft 4 in 10 47 m Height 7 ft 0 in 2 14 m Wing area 164 4 sq ft 15 27 m2 Empty weight 638 lb 289 kg Gross weight 1 050 lb 476 kg Powerplant 1 Continental A50 air cooled horizontally opposed four cylinder piston engine 50 hp 37 kW Performance Maximum speed 92 mph 148 km h 80 kn Landing speed 28 mph 24 kn 45 km h Range 225 mi 362 km 196 nmi Service ceiling 14 500 ft 4 400 m Rate of climb 700 ft min 3 6 m s See also EditAircraft of comparable role configuration and era Birdman TL 1 Pterodactyl Ascender Eipper Quicksilver Mitchell U 2 Superwing Ultraflight Lazair Zenair ZipperReferences Edit Bridgman Leonard ed 1947 Jane s all the World s Aircraft 1947 London Sampson Low Marston amp Co p 178c Taylor Michael J H 1989 Jane s Encyclopedia of Aviation London Studio Editions The Rigid Wing Web Site Gliding and Motorgliding International This article on an aircraft of the 1970s is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title AmEagle American Eaglet amp oldid 1089001732, wikipedia, wiki, book, books, library,

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