ROTAX 912 UL

912 UL / A / F

80 hp

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The highly reliable and efficient entry-level motor for light aviation aircraft manufacturers.

  • Four-stroke piston engine with four liquid and air-cooled cylinders
  • Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
  • The lightest engine in the Rotax aircraft engine portfolio
  • 2 carburetors
  • Mechanical fuel pump
  • Dual electronic ignition
  • Electric starter
  • Propeller speed reduction gearbox
  • TBO 2,000 hrs
Category:
ENGINE DATA
WEIGHTkglb
Engine with propeller speed reduction gearbox i = 2.27 (opt. i = 2.43)55.4122.0
Exhaust system4.08.8
Overload clutch1.73.7
External alternator3.06.6
Air guide hood0.40.8
Engine suspension frame2.04.4
PERFORMANCE
59.6 kW80 hp5800 1/min.
TORQUE
103 Nm75.9 ft. lb.4800 1/min.
Max RPM
5800 1/min.
BORE
79.5 mm3.13 in
STROKE
61.0 mm2.4 in
DISPLACEMENT
1211.2 cm³73.9 cu in

* leaded, unleaded, AVGAS 100LL, Ethanol 10

UL: ASTM compliant | A: certified according to JAR 22
F:
certified according to FAR33

Downloads

Datasheet 912 UL

Rotax Genuine Parts Flyer

Rotax Aircraft Engines Brochure

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