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  2. Canadair CT-114 Tutor - Wikipedia

    en.wikipedia.org/wiki/Canadair_CT-114_Tutor

    The Canadair CT-114 Tutor (company model CL-41) is a jet trainer that was designed and produced by Canadian aircraft manufacturer Canadair. It served as the standard jet trainer of the Royal Canadian Air Force (RCAF), and later Canadian Armed Forces , between the early 1960s and 2000.

  3. Canadair - Wikipedia

    en.wikipedia.org/wiki/Canadair

    CT-114 Tutor Tebuan Trainer (aircraft) 2 0 Launch date: 1960 First flight: 1962 First del'y: 1966 CL-43 Twin-engine logistics concept aircraft [18] Never built, but later influenced the design for the CL-204 (later as CL-215); modified floatplane based on PBV-1 Canso (PBY-1 Catalina) with two R-1340 engines [citation needed] CL-44: CC-106 Yukon

  4. Template:Canadian Forces aircraft - Wikipedia

    en.wikipedia.org/wiki/Template:Canadian_Forces...

    Main page; Contents; Current events; Random article; About Wikipedia; Contact us; Help; Learn to edit; Community portal; Recent changes; Upload file

  5. Canadair CT-133 Silver Star - Wikipedia

    en.wikipedia.org/wiki/Canadair_CT-133_Silver_Star

    The Canadair CT-133 Silver Star (company model number CL-30) is the Canadian license-built version of the Lockheed T-33 jet trainer aircraft, in service from the 1950s to 2005. The Canadian version was powered by the Rolls-Royce Nene 10 turbojet , instead of the original Allison J33 .

  6. Allison TF41 - Wikipedia

    en.wikipedia.org/wiki/Allison_TF41

    The Engines of Pratt & Whitney: A Technical History. Reston. Virginia: American Institute of Aeronautics and Astronautics. ISBN 978-1-60086-711-8. Gunston, Bill (2006). World Encyclopedia of Aero Engines, 5th Edition. Phoenix Mill, Gloucestershire, England, UK: Sutton Publishing Limited. p. 9. ISBN 0-7509-4479-X.

  7. General Electric J85 - Wikipedia

    en.wikipedia.org/wiki/General_Electric_J85

    The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 3,500 lb f (16 kN ) of thrust dry; afterburning variants can reach up to 5,000 lb f (22 kN). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg).