ROTAX 914 UL

914 UL | F

115 hp

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Low-weight engine with excellent performance at high altitudes.
  • Four-stroke piston engine with four liquid and air-cooled cylinders
  • Turbocharger
  • Automatic wastegate control
  • Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
  • 2 carburetors
  • Dual electronic ignition
  • Electric starter
  • Propeller speed reduction gearbox
  • Engine mount assembly
  • Air intake system
  • Exhaust system
  • TBO 2,000 hrs
Category:
ENGINE DATA
WEIGHTkglb
Engine with propeller speed reduction gearbox i = 2.4364.0140.8
Exhaust system4.08.8
Engine suspension frame2.03.7
Overload clutch1.73.7
External alternator3.06.6
PERFORMANCE
84.8 kW115 hp5800 1/min
TORQUE
144 Nm106 ft. lb.4900 1/min
Max RPM
5800 1/min
BORE
79.5 mm3.13 in
STROKE
61.0 mm2.4 in
DISPLACEMENT
1211.2 cm²73.91 cu in
FUEL*
min. MON 85 RON 95* min AKI 91*

Engine performance may vary depending on, among other things, general conditions, ambient temperature and altitude.

* leaded, unleaded, AVGAS 100LL, Ethanol 10
** max. continuous power at 5500 1/min
*** MOGAS, no hydraulic governor

Downloads

Datasheet 914 UL

Rotax Genuine Parts Flyer

Rotax Aircraft Engines Brochure

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