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brochure-m250turboprop-tcm92-12978

brochure-m250turboprop-tcm92-12978

brochure-m250turboprop-tcm92-12978

Product catalog summary
Overview: The M250-B17 turboprop engine is a highly refined, reliable engine designed for light aircraft. It is part of the M250 family, which has evolved from the M250-B15 to the current 450shp M250-B17 model.
Specifications:
  • Power: 450shp
  • Width: 19.4 inches
  • Length: 45 inches
  • Weight: 212 pounds
  • Certification and Entry into Service: 1971
Key Features:
  • Low direct operating cost
  • Suitable for single and twin-engine applications
  • Compact and simplified construction
  • Excellent power-to-weight ratio
  • Multi-fuel capability
  • Global factory-authorized support network
Applications and Usage: The M250 turboprop is favored for its small size and high power-to-weight ratio, making it ideal for OEMTC designs and STC conversions of piston-engined aircraft. Over 1,400 units are in operation, accumulating over five million flight hours. It operates on all certified aircraft fuels, beneficial for remote operations.
Performance Data:
  • Sea level static rating for take-off allows a measured gas temperature up to 810°C, provided maximum torque is not exceeded.
  • Delivered shaft horsepower varies across models and conditions, with the B17C delivering 450shp at take-off.
  • Specific fuel consumption (Sfc) ranges from 0.613 to 0.715 lb/shp-hr depending on the model and cruise condition.
Continuous Improvement: The M250 series benefits from ongoing enhancements, maintaining its position at the forefront of small gas turbine engine design.
Disclaimer: The information is proprietary to Rolls-Royce plc and is provided without warranty or representation.
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Catalog excerpts

brochure-m250turboprop-tcm92-12978-1

Powering the world's light aircraft

 Open the catalog to page 1
brochure-m250turboprop-tcm92-12978-2

Powering the world’s light aircraft The M250-B17 turboprop engine series represents the latest refinement of a rugged and highly ● Single and twin engine applications reliable small turboprop engine. ● Simplified, compact construction ● Excellent power-to-weight ratio As a part of the M250® family, the first M250-B15 turboprop has grown with the core engine into a family of highly successful engines for light fixed-wing aircraft, culminating in today’s 450shp M250-B17. ● Low direct operating cost ● Multi-fuel capability ● Factory authorised support network

 Open the catalog to page 2
brochure-m250turboprop-tcm92-12978-3

simply delivers more The M250 turboprop is popular due to its small size and The M250 turboprop enjoys the benefits from a continuous high power-to-weight ratio, which make it ideal for Original improvement culture which has seen the M250 remain at the Equipment Manufacture Type Certified (OEMTC) designs forefront of small gas turbine engine design. and for Supplemental Type Certificate (STC) conversions of existing piston-engined designs. Over 1,400 M250 The M250-B17 has a factory authorised global support turboprops are flying, with over five million flight hours. network of overhaul, maintenance,...

 Open the catalog to page 3
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Sea level static rating Delivered Measured gas Sfclb/shp-hr shaft horsepower temperature (C) (max) •Measured gas temperature for takeoff up to 810 C is permitted provided maximum torque is not exceeded The information in this document is the property of Rolls-Royce pic 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 pic. Whilst this information is given in good faith based upon the latest information available to Rolls-Royce pic, no warranty or representation is given...

 Open the catalog to page 4

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