Downloaded from https://www.everyspec.com ADS-79D-HDBK APPENDIX A FATIGUE LIFE MANAGEMENT A.1 SCOPE A.1.1 Purpose. The purpose of this appendix is to define the criteria for acceptance of CBM Credit/Debit for incorporation of CBM into Army aircraft systems from a Fatigue Life Management (FLM) point of view. This appendix also documents potential applications of FLM. A.2 APPLICABLE DOCUMENTS (Copies of this document are available at http://www.redstone.army.mil/amrdec/rdmr- se/tdmd/StandardAero.htm ) (Copies of this document are available from https://assist.daps.dla.mil/quicksearch/ DLA Document Services, Building 4/D, 700 Robbins Avenue, Philadelphia, PA 19111-5094.
215-697-6396.) (Copies of these documents are available from sources as noted.) 34 AVIATION POLICY MEMORANDUM Aviation Policy Memorandum Number 08-03 Memorandum, Program Executive Officer (PEO), System Safety Risk Management Process, 20 Jun 2008 JOINT SERVICE SPECIFICATION GUIDE JSSG-2001 Department of Defense Joint Service Specification Guide, Air Vehicle, 29 Jan 2009. JSSG-2006 Department of Defense Joint Service Specification Guide, Aircraft Structure, 30 October 1998. VARIOUS REFERENCES Benton, Robert E, Jr. ―Further Advances in a Recently Developed Cumulative- Damage Reliability Method‖, American Helicopter Society 66th Annual Forum Proceedings, Phoenix, AZ, May 11-13, 2010. Collins, J.
A. Failure of Materials in Mechanical Design: Analysis, Prediction, Prevention. Wiley & Sons: New York, 1993. Adams, D. O. and J. Zhao "Searching for the Usage Monitor Reliability Factor Using an Advanced Fatigue Reliability Assessment Model", presented at the American Helicopter Society 65th Annual Forum, Grapevine, Texas, May 27-29, 2009. Zhao, J. and D. O. Adams ―Achieving Six-Nine‘s Reliability Using an Advanced Fatigue Reliability Assessment Model‖, Presented at the American Helicopter Society 66th Annual Forum, Phoenix, AZ, May 11-13, 2010