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Diamond DA50

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Unit cost
  
325,000–425,000 EUR

First flight
  
April 4, 2007

Diamond DA50 TurbinePowered Diamond DA50 Takes Flight Flying Magazine

Diamond da50 superstar private prop plane features specs


The Diamond DA50 Super Star and DA50 Magnum are Austrian five-place single-engine composite aircraft designed by Diamond Aircraft Industries. Introduced in 2006, the project was later put on hold until the turboprop JP7 variant was introduced in 2015.

Contents

Diamond DA50 Diamond DA50 Specifications A photo

Diamond da50


Development

Diamond DA50 Diamond DA50 Superstar Untitled Aviation Photo 1327749

The DA50 was unofficially presented in December 2006 at a company Christmas party and is to be able to be operated with gasoline and diesel engines up to 350 hp. The new five seater will have one of the largest cabins of the new generation of general aviation airplanes.

Diamond DA50 httpsuploadwikimediaorgwikipediacommonsthu

The avgas powered version of the DA50 is to be equipped with a single FADEC-equipped Continental TSIO-550-J powerplant with twin turbo chargers producing 350 hp (261 kW). The plane's wingspan is currently reported as 38', 4", with overall fuselage length of 29 feet. The maximum takeoff weight is planned to be 3,527 lbs. The Diamond DA50 Super Star will be pressurized and offer a Ballistic Recovery Systems aircraft parachute system as an option.

The DA50 made its maiden test flight on April 4, 2007 at the Wiener Neustadt East Airport, Austria. The plane made its public debut at the AERO Friedrichshafen show in Germany on April 19, 2007.

Diamond DA50 Diamond DA50 YouTube

The DA50 project was put on hold in 2009 as the economy entered an extended downturn and Diamond turned all their attention to the Diamond D-Jet.

Diamond DA50 Welcome to Aircraft Compare

On 19 January 2015 the prototype now designated DA50-JP7 and powered by a Ivchenko-Progress Motor Sich AI-450S turboprop powerplant, was test-flown in Wiener Neustadt. In 2015 type certification was expected near the end of 2016.

Variants

DA50 SuperStar
Pressurized version powered by a Teledyne Continental TSIOF-550J. US FAA certification was initially forecast for 2012.
DA50 Magnum
Unpressurized version, with a standard integral oxygen system, powered by an Austro Engine AE 300 170 hp (127 kW) diesel, US FAA certification originally forecast for mid-2010
DA50-JP7
7-seat version powered by a 465 hp (347 kW) FADEC-controlled Ivchenko-Progress Motor Sich AI-450S turboprop engine. Two sub-variants are planned, one "tundra" version with rugged landing gear, and one high-performance version for training and private customers. Certification is expected mid to end 2016.

Specifications (DA50 SuperStar)

Data from Diamond Aircraft

General characteristics

  • Crew: one
  • Capacity: four passengers
  • Length: 28 ft 11 in (8.81 m)
  • Wingspan: 38 ft 4 in (11.68 m)
  • Height: 7 ft 3 in (2.21 m)
  • Wing area: 148 sq ft (13.7 m2)
  • Empty weight: 2,200 lb (998 kg)
  • Gross weight: 3,560 lb (1,615 kg)
  • Fuel capacity: 74 US gallons (280 litres)
  • Powerplant: 1 × Teledyne Continental TSIOF-550J six cylinder, four-stroke, piston aircraft engine, 350 hp (260 kW)
  • Propellers: 3-bladed constant speed, with 4-bladed propeller optional
  • Performance

  • Cruise speed: 200 kn (230 mph; 370 km/h)
  • Avionics

  • Garmin G1000 three-screen
  • References

    Diamond DA50 Wikipedia


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