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The Davis D-1 is an American light two-seat parasol-winged monoplane of the late 1920s.

Davis D-1
Airworthy Davis D-1-W with 145 h.p. Warner Scarab at Bartow Municipal Airport, Florida, in April 2009
Role	light sports aircraft Type of aircraft
National origin	United States
Manufacturer	Davis Aircraft Corporation
Introduction	1929
Status	some still flying
Primary user	private pilot owners
Produced	1929-1930

Development and design

The Davis D-1 was developed from the Davis V-3, which in turn was developed from the Vulcan American Moth. The Davis Aircraft Corporation had its factory at Richmond, Indiana. The D-1 is a parasol-winged aircraft of mixed construction with a two-spar wing and a rectangular welded steel-tube fuselage, the whole being covered by fabric. There are tandem open cockpits and it is fitted with a fixed tailwheel undercarriage which is attached by struts to the fuselage top and bottom. The wing is braced by struts from the lower fuselage. Various engines of between 60 to 125 hp (45 to 93 kW) have been fitted.[1]

Operational history

The D-1 was used from 1929 by sporting pilots and by private pilot owners for leisure flying. In September 1930, Art Chester bought a Davis D-1-85 parasol, and flew it to victory in the 1930 National Air Races.[2] A late model D-1W "The Whistler II" was built in 1933 for Davis with a canopy. It was raced in the 1934 Miami air race by Art Davis winning the category at 133.478 mph. It was later owned by movie star Richard Arlen, and restored to become a Grand Champion antique.[3]

Most Davis aircraft were sold in the United States but at least one went to Argentina. Fourteen examples remained in 2001 in various states of airworthiness[4] and several are still airworthy in 2011.

Variants

(Data from Aerofiles)

D-1

60 hp (45 kW) LeBlond 5D (23 built)

D-1-166

85 hp (63 kW) LeBlond 5DF (4 built)

D-1-K

100 hp (75 kW) Kinner K-5 (10-15 built)

D-1-L

prototype of the D-1-166 with 90 hp (67 kW) Lambert R-266 (1 built - also known as D-1-85)

D-1-W

125 hp (93 kW) Warner Scarab (8 converted from D-1-K)

Specifications (D-1-W)

Data from Green

General characteristics

• Crew: one
• Capacity: one passenger
• Length: 20 ft 4 in (6.20 m)
• Wingspan: 30 ft 2 in (9.19 m)
• Height: 7 ft 3 in (2.21 m)
• Empty weight: 925 lb (420 kg)
• Gross weight: 1,461 lb (663 kg)
• Powerplant: 1 × Warner Scarab seven-cylinder radial air-cooled piston, 125 hp (93 kW)

Performance

• Maximum speed: 142 mph (229 km/h, 123 kn)
• Cruise speed: 122 mph (196 km/h, 106 kn)
• Stall speed: 46 mph (74 km/h, 40 kn)
• Range: 480 mi (770 km, 420 nmi)
• Service ceiling: 14,800 ft (4,500 m)

Notes

References

External links

Wikimedia Commons has media related to Davis D-1.

• Information and photographs of the D-1 series (Sourced from Aerofiles)

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