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CF34-10A

CF34-10A

CF34-10A

Product catalog summary
Introduction
The CF34-10A is a turbofan engine developed by GE Aviation, known for its economic efficiency and environmental performance. It integrates proven technologies from other GE and CFMI engines, such as the CFM56, CF6, and GE90, to meet the thrust requirements of the ARJ21 aircraft.
Specifications
  • Maximum takeoff thrust with APR: 17,640 lb
  • Bypass ratio: 5:1
  • Maximum overall pressure ratio: 29:1
  • Thrust/weight ratio: 5.1:1
  • Fan diameter: 53 in
  • Maximum diameter: 57 in
  • Length: 90 in (excluding centerbody)
  • Weight: 3,700 lb
  • Noise and emissions: Meets or surpasses ICAO Chapter 3 & 4 and '96 & '04 requirements
  • Specific fuel consumption: 35K/.78 Mn max cruise .65
Performance and Features
The CF34-10A offers an 18,000-pound thrust class and is designed for high reliability, low operating costs, and ease of maintenance. It is part of GE's successful CF34 engine family and is selected for the COMAC ARJ21 aircraft.
Milestones
  • First engine test: 2006
  • FAA engine certification: 2010
  • Entry into service: 2011
Applications
The engine is used in the COMAC ARJ21 aircraft, with GE providing the complete propulsion system, including nacelle/thrust reverser and Engine-Buildup Unit components.
Contact Information
GE Aviation, One Neumann Way, Cincinnati, Ohio 45215, U.S.A. Phone: 513-552-3272 (international), 877-432-3272 (within U.S.)
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Catalog excerpts

CF34-10A-1

GE Aviation The CF34-10A is an advanced 18,000 pound thrust class economy and outstanding environmental characteristics turbofan. It is a member of GE’s family of highly successful In addition to drawing upon the proven technologies CF34® commercial jet engines and has been selected to of other CF34 engine models, the CF34-10A also power the new COMAC ARJ21 aircraft family. Although incorporates the very best demonstrated GE and CFMI the -10A represents a considerable capability increase technologies from other large commercial airliner engines, over the other CF34 engine models, it incorporates the including the CFM56, CF6® and GE90®. To ensure that the same basic development philosophy and operational -10A meets the ARJ21’s thrust power requirements for features that have earned exceptional market success for greater aircraft payload and range, the CF34-10A will the CF34-3 and -8 Series engines: low-risk, proven enter into service at 18,000 pounds APR thrust and be technology, low operating costs through high reliability, capable of achieving higher thrust levels for the future. ease of maintenance, excellent fuel GE provides the total CF34-10A propulsion system for the ARJ21, including the nacelle/thrust reverser and EngineBuildup Unit (EBU) components for fuselage mounting. CF34-10A Turbofan 18,000 lb thrust class

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CF34-10A-2

CF34-10A turbofan propulsion Applications Performance Specifications Maximum takeoff thrust with APR* Bypass ratio Maximum overall pressure ratio Thrust/weight ratio Maximum diameter Meets or surpasses ICAO Chap. 3 & 4 requirements Meets or surpasses ICAO ‘96 & ‘04 requirements Specific fuel consumption 35K/.78 Mn max cruise *Uninstalled. Sea level flat-rated to 86oF/30oC. **Length does not include centerbody. Milestones First engine to test Entry into service Application photos courtesy of COMAC CF34, CF6, and GE90 are registered trademarks of General Electric Company. GE Aviation One Neumann...

 Open the catalog to page 2

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