CFM56-5B

Maintenance Capabilities

  • EIS: 1994
  • Two-shaft turbofan engine with nine thrust categories ranging from 23,300 to 32,000 lbf
  • Five-stage low-pressure compressor
  • Nine-stage high-pressure compressor
  • Single-stage high-pressure turbine
  • Four-stage low-pressure turbine
  • Full MRO capability, including test cell
  • Airbus A320 CEO (A318/319/320/321)

Other Engines