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  2. Basler BT-67 - Wikipedia

    en.wikipedia.org/wiki/Basler_BT-67

    Basler Turbo Conversions was founded in 1990 solely focused on converting existing C-47/DC-3 airframes into the BT-67. [2] Basler configures each new build to the client's specifications. Industries served include cargo, military, cloudseeding, and scientific research.

  3. Spectrum SA-550 - Wikipedia

    en.wikipedia.org/wiki/Spectrum_SA-550

    The Basler Turbo 37/Spectrum SA-550 is a twin-boom single engined aircraft converted from a Reims/Cessna FTB337G Skymaster by Basler Turbo Conversions and Spectrum Aircraft Corporation. The aircraft first flew on 1 February 1983. [1] [2] [3]

  4. Douglas DC-3 - Wikipedia

    en.wikipedia.org/wiki/Douglas_DC-3

    Other conversions featured Armstrong Siddeley Mamba or Pratt & Whitney PT6A turbines. The Greenwich Aircraft Corp DC-3-TP is a conversion with an extended fuselage and with Pratt & Whitney Canada PT6A-65AR or PT6A-67R engines fitted. [17] [18] [19] The Basler BT-67 is a conversion of the DC-3/C-47.

  5. List of Douglas DC-3 family variants - Wikipedia

    en.wikipedia.org/wiki/List_of_Douglas_DC-3...

    The second aircraft replaced the first which had been severely damaged in a fire. USAC DC-3 Turbo Express A turboprop conversion by the United States Aircraft Corporation, fitting Pratt & Whitney Canada PT6A-45R turboprop engines with an extended forward fuselage to maintain center of gravity. First flight of the prototype conversion, (N300TX ...

  6. Cessna 421 Golden Eagle - Wikipedia

    en.wikipedia.org/wiki/Cessna_421_Golden_Eagle

    Riley Turbine Rocket 421 Conversion of Cessna 421 aircraft by fitting two Lycoming LTP101 turboprop engines. Formal designation R421BL and R421CL for conversions of 421B and C respectively. [4] Riley Turbine Eagle 421 Conversion of Cessna 421C aircraft by fitting two 750hp Pratt & Whitney Canada PT6A-135 turboprop engines.

  7. Beechcraft Duke - Wikipedia

    en.wikipedia.org/wiki/Beechcraft_Duke

    Called the Royal Turbine Duke conversion, [8] the modification increases fuel capacity by 28 US gal (110 L) and the maximum useful load by 400 lb (180 kg). The take-off length required is shortened by over 1,500 ft (460 m) to only 1,000 ft (300 m) and the landing distance is reduced by over 2,000 ft (610 m) to only 900 ft (270 m).