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Cirrus VK-30

General Aviation and Light Aircraft

The Cirrus VK-30 was a single-engine, pusher-propeller homebuilt aircraft sold as a kit by Cirrus Design, now Cirrus Aircraft, and it was the company's first model. Its name stands for Viken-Klapmeier, after two of the college friends who conceived it in the early 1980s alongside Dale Klapmeier. The all-composite five-seat design used natural laminar flow surfaces and a mid-mounted engine driving a propeller behind the tail, and it was introduced at the 1987 EAA convention in Oshkosh before first flying on 11 February 1988. Only about 40 kits were delivered before production stopped in 1993, but the lessons of the VK-30 led the founders toward the conventional certified layout of the later SR20 and SR22.

Facts
Year
1988 2
Engine Class
Piston 1
Status
Out of production 1
Power (kW)
224 1
Mass (kg)
1089 1
Maximum Mass (kg)
1633 1
Engine
Continental IO-550 2
Engine
Continental IO-550-G 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Ancestor Of

Cirrus ST-50, Vehicles
Source Cirrus VK-30 (Wikipedia)

Exemplifies

Source Cirrus VK-30 (Wikipedia)

Of Make

Source Cirrus VK-30 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Cirrus VK-30 (Wikipedia)Lead, manufacturer
Quote, Lead, manufacturer
originally sold as a kit by Cirrus Design (now Cirrus Aircraft)

Originated In

Also in Geography Atlas: where this subject originated.

Source Cirrus VK-30 (Wikipedia)Design and development
Quote, Design and development
Oshkosh, Wisconsin
Sources
1. Cirrus VK-30 (Wikipedia)
  • Design and development, first flight
    The aircraft's first flight was made on 11 February 1988
  • Design and development, production end
    Cirrus discontinued production of the aircraft in 1993
  • Lead
    single-engine pusher-propeller homebuilt aircraft
  • Specifications, powerplant
    Continental IO-550-G horizontally opposed piston engine
  • Specifications, power
    300 hp (220 kW)
  • Specifications, empty weight
    Empty weight: 2,400 lb (1,089 kg)
  • Specifications, max takeoff weight
    Max takeoff weight: 3,600 lb (1,633 kg)
  • Lead, manufacturer
    originally sold as a kit by Cirrus Design (now Cirrus Aircraft)
  • Design and development
    Oshkosh, Wisconsin
  • Ancestor Of: Cirrus ST-50, Variants, predecessor
    The VK-30 was the predecessor of the Cirrus ST-50
View the Source
2. EAA Aviation Museum: 1991 Cirrus VK-30 - N33VK
EAA Aviation Museum
  • Collection entry, test flight
    Jim Patton flew the test flight on February 11, 1988.
  • Collection entry, specifications
    Powerplant: Continental IO-550
View the Source
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