CAN40

Manufactured by Orenda Engines Limited for the Canadair CT-114 Tutor and Canadair CL-41 Tutor, military classes of the J85-CAN-40 engine generate up to 2,650 lbf (11.8kN) thrust.

Performance

• Type: Turbojet engine
• Length: 115 – 130 cm (45.4 – 51.1 in) (varies depending on additional equipment)
• Diameter: 17.7 in (45 cm)
• Compressor: 8 stages axial
• Dry weight: 180 – 191 kg (396 – 421 lb) (varies depending on additional equipment)
• Turbine: 2 stages
• Fuel type: Jet fuel
• Combustors: Annular
• Maximum thrust: 2,850 – 3,100 lbf (12.7 to 14 kN) (dry)
• Turbine inlet temperature: 977C
• Thrust-to-weight ratio: 7.5 (-21), 6.6 (-5), 6.8 (-13), 7 (-15)
• Specific fuel consumption: 0.96 – 0.97 lb/(lbf·h) (27 g/kN·s)
• Overall pressure ratio: 8.3

Applications

• Canadair CL-41 Tutor
• Canadair CT-114 Tutor

Allow us to reshape the standard engine maintenance plan according to your personalized needs to reduce costs and increase your fleet’s technical reliability. Whatever service you need around the power horses of your aircraft, our specialists will support you with competence.

Your Benefits at a Glance

• Short- and long-term cost reduction
• Customized solutions
• Complete Foreign Military Sales (FMS) support

Our experience and knowledge in engine parts and accessories literally pays off for our clients. Get more information on our capabilities by speaking to one of our technical support associates at +1 (209) 983-1112.