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Orenda Engines Limited manufactured J85-CAN-15 for the Canadair CF-116, 4,300 lbf (19 kN) thrust. Orenda was Canada’s prime aircraft engine manufacturer and parts supplier. As part of the earlier Avro Canada conglomerate, which became Hawker Siddeley Canada, they produced a series of military jet engines from the 1950s through the 1970s, including the J85-CAN-15. 


  • Type: Turbojet engine (with or without afterburner)
  • Diameter: 17.7 in (45 cm)
  • Length: 45.4 to 51.1 in (115 to 130 cm)
  • Compressor: 8 stages (9 in J85-21) axial
  • Dry weight: 396 to 421 lb (180 to 191 kg) 
  • Combustors: Annular
  • Turbine: 2 stages
  • Fuel type: Aviation turbine fuel
  • Specific fuel consumption: 0.96 to 0.97 lb/(lbf·h) (27 g/kN·s)
  • Maximum thrust: 2,850 to 3,100 lbf (12.7 to 14 kN) (dry)
  • Overall pressure ratio: 8:3
  • Turbine inlet temperature: 977C
  • Thrust-to-weight ratio: 7.5 (-21), 6.6 (-5), 6.8 (-13), 7 (-15)

What We Do Best: Keep Engines in the Air

The maintenance, repair, and overhaul (MRO) of the J85-CAN-15 turbojet is a step-by-step process similar to a medical check-up. It consists of interior and exterior visual inspections, washing and drying the jet engine parts, dismantling the engine, repairing and replacement of damaged parts and accessories, re-assembling, and then testing the engine to ensure ready-state performance. Aero Turbine Inc. specializes in these MRO services and more. 

To know more about how our products and services can help you, get in touch with us today.