SA-E917Ti | 105 kW
SA-E917Ti | 105 kW
New generation helicopter piston engine
Four-stroke piston engine with 4 liquid cooled opposed cylinders
Air intake manifold in composite carbon fiber material
Short Gearbox with speed reduction ratio i=2.27
Double alternator 24 A each
Turbocharger with stainless steel exhaust manifolds
State-of-the-art redundant Electronic Fuel Injection (EFI), dual injector and dual ignition
Fault-tolerant Engine Management System (EMS)
Closed loop control based on lambda sensor
Fully integrated real time diagnostic with data logging (50 h)
Custom CANBUS protocol
Custom solutions available