Aerospace engine

As our engines are built to order, and comes with several options and in multiple configurations, orders must be places directly with us or via our global dealers via email or phone.

- Technical Engine Data

•  Engine Displacement: ccm3
•  Bore x Stroke: xmm
•  Gearbox reduction ratio:
•  Engine weight w/gearbox w/overload clutch, turbocharger, intercooler, exhaust system: Kg / lb
•  Engine suspension frame: 2Kg / lb
•  External Alternator: 3Kg / lb
•  Air Guide Baffle: Kg / lb
•  Fuel Pump Assy: Kg / lb
•  Power output: HP (Kw) 
•  Torque: Nm (ft/lb) @ rpm
•  PTO Torque: Nm (ft/lb)@ rpm
•  Fluids: 50/50 Glycol/Water mix (silicate free), XPS 5W

- Operating Limitations

•  Idle speed: rpm
•  Max rpm: rpm (max 5 minutes)
•  Max cont.

  rpm: rpm

•  Cruise rpm: rpm
•  Critical Altitude: MAT max 50°C – ’ Note – The power is available up to critical altitude
•  Operating Al