Trisha Shetty (Editor)

Davis DA 2

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Top speed
  
193 km/h

Wingspan
  
5.86 m

Cruise speed
  
177 km/h

Engine type
  
Flat-four engine

Range
  
725 km

Length
  
5.44 m

Unit cost
  
2,300–2,300 USD (1971)

Davis DA-2 Flying the Davis DA2A Homebuilt

100 giant foam rc davis da 2 scatch built maiden flight


The Davis DA-2 is a light aircraft designed in the United States in the 1960s and was marketed for homebuilding. While it is a low-wing monoplane of largely conventional design with fixed tricycle undercarriage, the DA-2 is given a distinctive appearance by its slab-like fuselage construction and its V-tail. The pilot and a single passenger sit side-by-side. Construction of the aircraft is sheet aluminum throughout, with the sole compound curves formed a fiberglass cowling and fairings.

Contents

Davis DA-2 Langair Machining Inc Davis DA 2A

The DA-3 was a single DA-2 enlarged to accommodate four people. Work proceeded through 1973-74, but the aircraft was never completed.

Davis DA-2 Flying the Davis DA2A Homebuilt

Operational history

Davis DA-2 Leeon Davis Aircraft

Examples of the DA-2 have been completed in the United States, Canada and the United Kingdom and are currently (2015) actively flying in those countries.

Variants

  • DA-2
  • DA-2A
  • DA-3
  • Specifications (typical DA-2)

    Data from Popular Mechanics August 1973

    General characteristics

    Davis DA-2 httpsuploadwikimediaorgwikipediacommonsthu

  • Crew: One pilot
  • Capacity: 1 passenger
  • Length: 17 ft 10 in (5.44 m)
  • Wingspan: 19 ft 3 in (5.86 m)
  • Height: 5 ft 5 in (1.65 m)
  • Wing area: 83 ft2 (7.7 m2)
  • Empty weight: 610 lb (277 kg)
  • Gross weight: 1,125 lb (510 kg)
  • Powerplant: 1 × Continental A65 horizontally-opposed four-cylinder piston engine, 65 hp (49 kW)
  • Performance

  • Maximum speed: 120 mph (193 km/h)
  • Cruise speed: 110 mph (177 km/h)
  • Range: 450 miles (725 km)

  • Davis DA-2 FileDavis DA2A N187Mjpg Wikimedia Commons

    References

    Davis DA-2 Wikipedia