RR500  
Initial Operational Capability (IOC): 2010
Total Production: ?
Origin: United Kingdom
Corporations: Rolls-Royce
Parent System: RR500
Initial Operational Capability (IOC): 2010
Total Production: ?
Family Members: RR500TS
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Description: The Rolls-Royce RR500 is a turboprop engine intended for general aviation market and derived from the RR300 turboshaft powering the Robinson R66 helicopter. Being multi-fuel capable, and developing 350 to 450 shp of power, the new engine is suitable for a range of light single and twin-engine fixed wing aircraft applications which require excellent altitude performance. Rolls-Royce forecasts that between 2,500 to 3,000 of these aircraft will be delivered annually between 2010 and 2020. The RR500 turbine is based on the RR300 engine core and features an electronic engine monitoring system, extended time between overhauls, smoothness of operation and excellent performance in take-off, climb, cruise and descent segments of flight.

RR500 Specifications

Power
Max Power at TakeOff: 450 shp (336 kW)
CEP: Circular Error Probable
Meters (m)   Kilometers (km)   Nautic Miles (nm)   Inch (in)   Yard (yd)   Foot (ft)   Millimeter (mm)
Pound (lb)   Kilogram (kg)   kN (KiloNewton)   Ton (t)
Meters per Second (mps)   Kilometers per Hour (kph)   Knot (kt)   Miles per Hour (mph)
Liter (l)   Galon (gl)
Year (yr)   Minutes (min)   Second (sec)
Shaft-Horse-Power (shp)

RR500 News

There are 4 news between
29 Jul 2008 and 6 Mar 2011
Sunday, March 6, 2011Rolls-Royce hits key milestone with first development test of new RR500 engine
Monday, February 23, 2009Rolls-Royce and PZL-Swidnik Explore RR500 Applications
Friday, August 1, 2008Rolls-Royce Explores Future RR500 Turboprop Applications with Mooney Airplane Company
Tuesday, July 29, 2008Rolls-Royce Launches RR500 Turboprop Engine for General Aviation Market
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