NEW GENERATION HELICOPTER PISTON ENGINE | SA-E917Ti | 160 HP
Best power-to-weight ratio.
Four-stroke piston engine 1416 cc, four liquid cooled opposed cylinders.
State-of-the-art redundant Electronic Fuel Injection (EFI), dual injector and dual ignition.
Turbocharger with stainless steel exhaust manifolds and titanium muffler.
Air intake manifold in composite carbon fiber material.
Dry-sump forced lubrication with separate oil tank.
Speed reduction gearbox 2.27 ratio.
Double alternator 22 A each.
Redundant, multiple fault-tolerant Engine Management System (EMS).
Fully integrated real time diagnostic with data logging.
Custom CAN-bus and CANaerospace protocols.
CANBUS strategies and fans management.
Installed weight: 76,9 kg
Max operating altitude 24.000 ft
Full take-off power up to 16.000 ft
TBO 1200 hours