Wing Derringer

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.

Development
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 FAA type certificate A9WE on December 20, 1966. The aircraft did not go into production due to internal problems within the Hi-Shear Corporation.

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.

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.

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 and then entered bankruptcy in July 1982, after which only one further aircraft was built before seven unfinished airframes were sold.

As of June 3, 1998, the D-1’s type certificate number A9WE was held by Emerald Enterprises LTD of San Diego, CA.

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

Specifications (D-1)
{{Aircraft specs
 * ref=Jane's All The World's Aircraft 1980-81
 * prime units?=kts


 * genhide=


 * crew=2
 * capacity=
 * length m=
 * length ft=23
 * length in=0
 * length note=
 * span m=
 * span ft=29
 * span in=2
 * span note=
 * height m=
 * height ft=8
 * height in=0
 * height note=
 * wing area sqm=
 * wing area sqft=121
 * wing area note=
 * volume note=
 * aspect ratio=7
 * airfoil=NACA 65{{sub|2}}-415
 * empty weight kg=
 * empty weight lb=2070
 * empty weight note=
 * gross weight kg=
 * gross weight lb=
 * gross weight note=
 * max takeoff weight kg=
 * max takeoff weight lb=3050
 * max takeoff weight note=
 * fuel capacity={{convert|88|USgal|L impgal|abbr=on}}}
 * more general=


 * eng1 number=2
 * eng1 name=Avco Lycoming IO-320-B1C
 * eng1 type=4-cylinder air-cooled horizontally-opposed piston engines
 * eng1 kw=
 * eng1 hp=160


 * power original=
 * thrust original=


 * prop blade number=2
 * prop name=Hartzell constant speed propellers
 * prop dia m=
 * prop dia ft=5
 * prop dia in=6
 * prop dia note=


 * perfhide=


 * max speed kmh=
 * max speed mph=
 * max speed kts=201
 * max speed note=at sea level
 * max speed mach=
 * cruise speed kmh=
 * cruise speed mph=
 * cruise speed kts=184
 * cruise speed note= at 13000 ft (65% power)
 * stall speed kmh=
 * stall speed mph=63
 * stall speed kts=
 * stall speed note= (landing gear and flaps down)


 * range km=
 * range miles=
 * range nmi=1007
 * range note=at 10000 ft (econ. cruise)
 * ceiling m=
 * ceiling ft=19600
 * ceiling note=
 * g limits=
 * roll rate=
 * glide ratio=
 * climb rate ms=
 * climb rate ftmin=1700
 * climb rate note=
 * time to altitude=
 * more performance=
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 * armament=
 * guns=
 * bombs=
 * rockets=
 * missiles=
 * hardpoints=
 * hardpoint capacity=
 * hardpoint rockets=
 * hardpoint missiles=
 * hardpoint bombs=
 * hardpoint other=

}}
 * avionics=