Rotax 916 iS 160 HP

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

Engine with components

Engine suspension frame

External alternator

Air guide baffle

PERFORMANCE

max. continuous power at 5500 1/min*

TORQUE

BORE

STROKE

DISPLACEMENT

FUEL *

85.8 kg / 189 lb

2.0 kg / 6.6 lb

3.0 kg / 4.4 lb

0.4 kg / 0.8 lb

117 kW / 160 hp / 5800 1/min

101 kW* / 137 hp

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 / 24. in

1352 cm³ / 82.6 cu in

min. MON 85 RON 95 min. AKI 91
*leaded, unleaded, AVGAS 100LL, Etanol 10

Retractable landing gear 80 m takeoff length 5 m needed to land (in optimal conditions)

Retractable landing gear
80 m takeoff length
5 m needed to land (in optimal conditions)