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LiteWing Aircraft LiteWing

January 05, 2023

The LiteWing Aircraft LiteWing, also called the Lite Wing Trike, is an American ultralight trike that was designed and produced by LiteWing Aircraft of Caryville, Tennessee in the late 1990s. The aircraft was supplied as a kit for amateur construction.[1][2]

LiteWing
Role Ultralight trike
National origin United States
Manufacturer LiteWing Aircraft
Status Production completed
Number built 20 (February 2000)

Design and development

The aircraft was designed to be a US homebuilt aircraft as its empty weight exceeds the US FAR 103 Ultralight Vehicles rules, which imposes a category maximum empty weight of 254 lb (115 kg). The LiteWing has a standard empty weight of 280 lb (127 kg). It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat, open cockpit with a three-piece fiberglass cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.[1][2]

The aircraft is made from welded and bolted 6061-T6 aluminum tubing, with its NorthWing 157 wing covered in Dacron sailcloth. Its 32 ft (9.8 m) span wing is supported by a single tube-type kingpost and uses an "A" frame control bar. The engine factory supplied was the 40 hp (30 kW) Rotax 447 twin cylinder, two-stroke, air-cooled aircraft engine. The aircraft can accept engines of 40 to 50 hp (30 to 37 kW). Brakes on the main wheels are standard equipment.[1][2]

Twenty examples had been completed and flown by February 2000.[2]

Specifications (LiteWing)

Data from Cliche and Kitplanes[1][2]

General characteristics

  • Crew: one
  • Length: 8 ft 6 in (2.59 m)
  • Wingspan: 32 ft (9.8 m)
  • Height: 7 ft 6 in (2.29 m)
  • Wing area: 160 sq ft (15 m2)
  • Empty weight: 280 lb (127 kg)
  • Gross weight: 600 lb (272 kg)
  • Fuel capacity: 6 U.S. gallons (23 L; 5.0 imp gal)
  • Powerplant: 1 × Rotax 447 twin cylinder, two-stroke aircraft engine, 40 hp (30 kW)
  • Propellers: 2-bladed wooden

Performance

  • Cruise speed: 60 mph (97 km/h, 52 kn)
  • Service ceiling: 10,000 ft (3,000 m)
  • Rate of climb: 1,000 ft/min (5.1 m/s)

References

  1. ^ a b c d Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page C-13. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4
  2. ^ a b c d e Downey, Julia: 2000 Trike and 'Chute Directory, Kitplanes, Volume 17, Number 2, February 2000, page 46. Kitplanes Acquisition Company. ISSN 0891-1851

January 05, 2023
litewing, aircraft, litewing, also, called, lite, wing, trike, american, ultralight, trike, that, designed, produced, litewing, aircraft, caryville, tennessee, late, 1990s, aircraft, supplied, amateur, construction, litewingrole, ultralight, trikenational, ori. The LiteWing Aircraft LiteWing also called the Lite Wing Trike is an American ultralight trike that was designed and produced by LiteWing Aircraft of Caryville Tennessee in the late 1990s The aircraft was supplied as a kit for amateur construction 1 2 LiteWingRole Ultralight trikeNational origin United StatesManufacturer LiteWing AircraftStatus Production completedNumber built 20 February 2000 Design and development EditThe aircraft was designed to be a US homebuilt aircraft as its empty weight exceeds the US FAR 103 Ultralight Vehicles rules which imposes a category maximum empty weight of 254 lb 115 kg The LiteWing has a standard empty weight of 280 lb 127 kg It features a cable braced hang glider style high wing weight shift controls a single seat open cockpit with a three piece fiberglass cockpit fairing tricycle landing gear with wheel pants and a single engine in pusher configuration 1 2 The aircraft is made from welded and bolted 6061 T6 aluminum tubing with its NorthWing 157 wing covered in Dacron sailcloth Its 32 ft 9 8 m span wing is supported by a single tube type kingpost and uses an A frame control bar The engine factory supplied was the 40 hp 30 kW Rotax 447 twin cylinder two stroke air cooled aircraft engine The aircraft can accept engines of 40 to 50 hp 30 to 37 kW Brakes on the main wheels are standard equipment 1 2 Twenty examples had been completed and flown by February 2000 2 Specifications LiteWing EditData from Cliche and Kitplanes 1 2 General characteristicsCrew one Length 8 ft 6 in 2 59 m Wingspan 32 ft 9 8 m Height 7 ft 6 in 2 29 m Wing area 160 sq ft 15 m2 Empty weight 280 lb 127 kg Gross weight 600 lb 272 kg Fuel capacity 6 U S gallons 23 L 5 0 imp gal Powerplant 1 Rotax 447 twin cylinder two stroke aircraft engine 40 hp 30 kW Propellers 2 bladed woodenPerformance Cruise speed 60 mph 97 km h 52 kn Service ceiling 10 000 ft 3 000 m Rate of climb 1 000 ft min 5 1 m s References Edit a b c d Cliche Andre Ultralight Aircraft Shopper s Guide 8th Edition page C 13 Cybair Limited Publishing 2001 ISBN 0 9680628 1 4 a b c d e Downey Julia 2000 Trike and Chute Directory Kitplanes Volume 17 Number 2 February 2000 page 46 Kitplanes Acquisition Company ISSN 0891 1851 Retrieved from https en wikipedia org w index php title LiteWing Aircraft LiteWing amp oldid 1066457630, wikipedia, wiki, book, books, library,

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