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Rotax 916 iS Turbo Aircraft Engine

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916 iS
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Product Description

Rotax 916 iS Turbo Aircraft Engine

Dynamic, turbocharged iS engine with best power-to-weight ratio and TBO 2,000h.
  • Four-stroke piston engine with four liquid and air-cooled cylinders
  • Redundant electronic fuel injection and ignition, eco mode
  • Turbocharger, stainless steel exhaust
  • Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets
  • Engine management system (EMS)
  • Electric starter (12 or 24 Volt)
  • Propeller speed reduction gearbox
  • Intercooler
  • TBO 2,000 hrs
  • Maximum operating altitude 23,000 feet
  • Full take-off power up to 15,000 feet
WEIGHT kg lb
Engine with propeller speed reduction gearbox i= 2,54 with overload clutch, turbocharger, intercooler, exhaust system 85.8 189
Engine suspension frame 2.0 4.4
External alternator 3.0 6.6
Air guide baffle 0.4 0.8
117 kW 160 hp 5800 1/min
**101 kW 137 hp 5500 1/min
193 Nm 142 ft lb 5800 1/min
175 Nm 129 ft lb 5500 1/min
84.0 mm 3.31 in
61.0 mm 2.4 in
1352 cm³ 82.6 cu in
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

iS: ASTM compliant | iSc: certified according to EASA CS-E

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