This standard specifies the general requirements for fatigue testing of shaft components of aviation gas turbine engines, test procedures, test data analysis and processing, test result evaluation and test report preparation, etc. This standard is applicable to fatigue testing of aviation gas turbine engine main shafts (including turbine shafts, compressor shafts, power turbine shafts and propeller shafts) or shaft components.
HB 20041-2011 Referenced Document
GJB 241 General specification for aerospace turbojet and turbofan engines
GJB 242 General specification for aerospace turboprop and turboshaft engines
HB 20041-2011 history
2011HB 20041-2011 Shaft assembly fatigue tests of aircraft engine