RR500 turbopropFor a new era of general aviation and military turboprop aircraft

The RR500 turboprop engine is a new addition

to the growing family of Rolls-Royce small gas

turbine engines.

It is a larger derivative of the RR300, with the engine

core scaled up for increased power. It will require

less frequent maintenance than piston engines of

similar power.

● Excellent hot and high performance

● 2,000 / 4,000 hour maintenance intervals

● Designed for ease of retrofit

● Multi-fuel capability - not dependant on AvGas

● Excellent power to weight ratio

● World-class service solutions

RR500 turboprop

For a new era of general aviation and military turboprop aircraft

Power 450shp Width 23.4in Length 43.1in Weight 225lb Certification Expected 2012

The RR500 is multi-fuel capable and offers 350 to 450 shp.

It is designed for a range of light single and twin-engine

fixed wing aircraft applications and offers excellent altitude

performance.

The engine delivers greater speed, improved comfort,

increased reliability and unmatched operational capability

in a compact design. All of this is available in a powerplant

offering excellent value and lower lifecycle costs.

Rolls-Royce has unmatched turboprop engine

experience that assures the RR500 operator outstanding

performance and global support. Additionally, the RR500

is well suited for Supplemental Type Certificate (STC)

conversions of popular general aviation aircraft to

turbine power.

Rolls-Royce is an innovative leader in

developing, producing and supporting reliable

turboprop engines. The RR500 simply delivers

more of what today’s operators demand.

Power 450shp Width 23.4in Length 43.1in Weight 225lb Certification Expected 2012

s i m p l y d e l i v e r s m o r e

© Rolls-Royce plc 2009

The information in this document is the property of Rolls-Royce plc and may not be copied, or communicated to a third party, or used, for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc.

Whilst this information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.

VCOM13797 July 2009

www.rolls-royce.com

Printed on 75% recycled material

Flight mode

Take-o�

Maximum continuous

Normal cruise

Economic cruise

Performance

Delivered prop shaft power (HP)

450

380

320

270