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
ENGINE DATA
| 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 |
| PERFORMANCE |
|
|
| 117 kW |
160 hp |
5800 1/min |
| **101 kW |
137 hp |
5500 1/min |
| TORQUE |
|
|
| 193 Nm |
142 ft lb |
5800 1/min |
| 175 Nm |
129 ft lb |
5500 1/min |
| DISPLACEMENT |
|
| 1352 cm³ |
82.6 cu in |
| FUEL* |
| min. MON 85 RON 95 min. AKI 91 |
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