Suvarna Garge (Editor)

Wing Derringer

Updated on
Edit
Like
Comment
Share on FacebookTweet on TwitterShare on LinkedInShare on Reddit
Top speed
  
372 km/h

Wingspan
  
8.89 m

Cruise speed
  
337 km/h

First flight
  
April 1962

Range
  
1,007 km

Length
  
7.01 m

Engine type
  
Lycoming O-320

Wing Derringer images9fotkicomv131photos5416559712398Wing

1982 wing derringer d 1 ma7537jlh263


The Wing D-1 Derringer is an American light twin-engined two-seat monoplane tourer designed by John Thorp and developed by the Hi-Shear Corporation and built by the Wing Aircraft Company.

Contents

Wing Derringer Derringer Aircraft Company Wing Derringer D1 N976DA Flickr

N8602s wing derringer


Development

Wing Derringer Wing Derringer Photograph by Matt Abrams

The D-1 Derringer light twin design was originally designed in 1958 by John Thorp as the Thorp T-17 a twin-engined development of his Thorp T-11 Sky Scooter. The design was taken over by George Wing of the Hi-Shear Corporation. The Derringer is a low-wing cantilever monoplane with a retractable tricycle landing gear. It had room for two in an enclosed cockpit with an unusual up and backward opening canopy. It was powered by two 100 hp Continental O-200 engines, one mounted on the leading edge of each wing. The prototype aircraft (registered N3621G) first flew on May 1, 1962 at Torrance. A second prototype flew in November 1964 but crashed a few weeks later due to an in-flight airframe failure. A static test aircraft and two more aircraft were built for testing which resulted in the award of a type certificate on December 20, 1966. The aircraft did not go into production due to internal problems within the Hi-Shear Corporation.

Wing Derringer Wing Derringer Wikipedia

The Derringer used manufacturing techniques that were considered new at the time it was developed. Butt-joined, flush-riveted, chemically-milled and stretched skins are used throughout the airframe.

Wing Derringer WING DERRINGER Plane Pilot Magazine

Development of a two-seat Coin/military trainer version designated Wing D-2M Derringer was begun but failed to develop further than the design stage.

Wing Derringer 1965 Wing D1 Derringer twinengine twoseat cabin monoplane

In 1978 George Wing left Hi-Shear and started the Wing Aircraft Company. The company built one-pre-production aircraft followed by six production aircraft, entering bankruptcy in July 1982, after which only one further aircraft was built before seven unfinished airframes were sold.

Nine D-1 aircraft were on the U.S. civil aircraft register in May 2009.

Specifications (D-1)

Data from Jane's All The World's Aircraft 1980-81

General characteristics

  • Crew: 2
  • Length: 23 ft 0 in (7.01 m)
  • Wingspan: 29 ft 2 in (8.89 m)
  • Height: 8 ft 0 in (2.44 m)
  • Wing area: 121.0 sq ft (11.24 m2)
  • Aspect ratio: 7
  • Empty weight: 2,099 lb (952 kg)
  • Max takeoff weight: 3,049 lb (1,383 kg)
  • Fuel capacity: fuel:88 US gal (333.1 l; 73.3 imp gal), oil:4 US gal (15.1 l; 3.3 imp gal)
  • Powerplant: 2 × Avco Lycoming IO-320-B1C (or -C1A) 4-cyl air-cooled horizontally opposed piston engines, 160 hp (119 kW) each
  • Propellers: 2-bladed Hartzell HC-C2YL/8450-18, 5 ft 6 in (1.68 m) diameter constant speed fully feathering propellers
  • Performance

  • Maximum speed: 201 kn (231 mph; 372 km/h) at sea level
  • Cruise speed: 190 kn (219 mph; 352 km/h) maximum: 75% power at 3,050 m (10,010 ft)
  • Economical cruising speed: 182 kn (337 km/h; 209 mph) at 65% power at 3,050 m (10,010 ft)
  • Approach speed: 82.5 kn (152.8 km/h; 94.9 mph)
  • Stall speed: 69.5 kn (80 mph; 129 km/h) gear & flaps up, 63 kn (117 km/h; 72 mph) gear & flaps down
  • Range: 544 nmi; 626 mi (1,007 km) at economical cruising speed
  • Endurance: 5 hours 30 minutes at economical cruising speed
  • Service ceiling: 19,603 ft (5,975 m)
  • Rate of climb: 1,700 ft/min (8.6 m/s)
  • Wing loading: 28.46 lb/sq ft (138.95 kg/m2)
  • Power/mass: 0.168 kW/kg (0.103 hp/lb)
  • References

    Wing Derringer Wikipedia