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General Electric TF34
The Engine Specifications
 
The TF34 was launched in 1967 for the U.S. Navy S-3 Viking.  First flown in 1971, it has since been used by the U.S. Air Force A-10 and has a growing civil market.  The civil version of the TF34 is designated the CF34.
Turbofan
single-stage fan
14-stage compressor
Mass flow: 338 lbs/sec
 
Models Used by
 
TF34-GE-100: 9,065 lb (40.3 kN) thrust
CF34-3A1: 9,220 lb (41.0 kN) thrust
Fairchild Republic A-10
Thunderbolt II
Canadair CRJ Regional Jet
Lockheed S-3 Viking
 
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General Electric: TF34
 

page updated 04 July 2003

 

  

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