ADS-79D-HDBK Downloaded from https://www.everyspec.com APPENDIX J SEEDED FAULT TESTING J.1 SCOPE This Appendix provides guidance for the development and performance of component Seeded Fault Testing programs for the purposes of validating the accuracy and robustness of condition indicators (CIs) and health indicators (HIs) used as part of a condition based maintenance (CBM) system. J.2 REFERENCES AND APPLICABLE DOCUMENTS The documents listed below are not necessarily all of the documents referenced herein, but are those most useful in understanding the information provided by this document. The following references form a part of this appendix to the extent specified herein.
(Copies of these documents are available at https://assist.daps.dla.mil ) (Copies of these documents are available from sources as noted.) 175 DATA ITEM DESCRIPTIONS DI-NDTI-80566A Test Plan – Data Item Description, 14 November 2006. DI-NDTI-80809B Test/Inspection Report, 24 January 1997. VARIOUS REFERENCES CBM Test Requirements US Army Aviation Engineering Directorate (AED) Condition Based Maintenance (CBM) Office, June 2009. Decker, H.J., and D.G. Lewicki, ―Spiral Bevel Pinion Crack Detection in a Helicopter Gearbox‖, NASA Glenn Research Center, US Army Research Laboratory, June 2003. Keller, J.A., and P.
Grabill ―Inserted Fault Vibration Monitoring Tests for a CH- 47D Aft Swashplate Bearing‖, US Army RDECOM, June 2005. Prinzinger, J., and T. Rickmeyer ―Summary of US Army Seeded Fault Tests for Helicopter Bearings,‖ US Army Aviation Engineering Directorate (AED) Propulsion Division, September 2012.