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Compilation Of Damage Findings From Multiple Recent Teardown Analysis Programs

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ICAF 2009, Bridging the Gap between Theory and Operational Practice

Fleet managers depend upon various tools to assure the safe operation of their aircraft. Performing a structural teardown analysis program of one or more aircraft with known service history provides precise damage data resulting from a given usage. These data can then be used to validate NDI methods, update damage models and reduce uncertainty in the damage condition assessment of the remaining fleet.

In the past six years the USAF Academy Center for Aircraft Structural Life Extension (CAStLE) has been involved, at various levels, in multiple teardown analysis programs. CAStLE' level of involvement has ranged from consultant through failure analysis support to planning and executing all elements of an entire program. In each program large regions of selected aircraft were disassembled by precision means, cleaned of all coatings and inspected by a variety of NDI techniques. These NDI indications were then evaluated by failure analysis methods to determine the root cause of failure—the type of damage which resulted in the NDI indication. Failure analysis findings which were a result of aircraft operations were further analyzed to obtain detailed damage characteristics.

This work presents a summary of findings from teardown programs conducted on eight aircraft ranging from small military trainers to large transports. Comparisons are presented for damage types and categories of aircraft. Damage type and scale is also presented categorized by the type of damaged component (skin, stiffener, fitting, etc.). Data are also provided with regard to measurable features within regions of damage initiation.

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References

  1. MIL-STD-1530C, DoD Standard Practice, Aircraft Structural Integrity Program (ASIP) (2005), Aeronautical Systems Center, Wright-Patterson AFB, Ohio.

    Google Scholar 

  2. Shoales, G. (2008), Procedures for Aircraft Structural Teardown Analysis, USAFA TR-2008-02, USAF Academy, Colorado.

    Google Scholar 

  3. Shoales, G. (2009), Procedures for Aircraft Structural Teardown Analysis: Development of a Best Practices Handbook, Proceedings of the 25th International Conference on Aeronautical Fatigue Symposium, Rotterdam, Netherlands.

    Google Scholar 

  4. Shoales, G. (2008), Procedures for Aircraft Structural Teardown: Best Practices Handbook Development, 2008 Aircraft Structural Integrity Program Conference, San Antonio, Texas.

    Google Scholar 

  5. Steadman, D. and Bakuckas, Jr., J., (2007), DOT/FAA/AR-07/22, Destructive Evaluation and Extended Fatigue Testing of Retired Transport Aircraft, U.S. Department of Transportation, Federal Aviation Administration, Washington, D.C.

    Google Scholar 

  6. Final Report, C-5A Structural Risk and Model Revalidation Program, (2007), 730th Aircraft Sustainment Group, Robins AFB Georgia.

    Google Scholar 

  7. Shoales, G., Shah, S., Rausch, J., Walters, M., Arunachalam S., and Hammond, M. (2006), C-130 Center Wing Box Structural Teardown Analysis Final Report, USAFA TR-2006-11, USAF Academy, Colorado.

    Google Scholar 

  8. Arunachalam S. and Shoales, G. (2009), C/KC-135 Teardown Analysis Program Protocols, Protocol 8: Failure Analysis, USAFA TR-2009-06, USAF Academy, Colorado.

    Google Scholar 

  9. Shoales, G. (2009), C/KC-135 Teardown Analysis Program Protocol Development and Validation,” Aging Aircraft 2009 Conference, Kansas City, Kansas.

    Google Scholar 

  10. Brooks, C. Honeycutt, K. and Prost-Domasky S. (2000), Case Studies for Life Assessments With Age Degradation, Aging Aircraft 2000 Conference, St. Louis, Missouri.

    Google Scholar 

  11. Powell, G., (Ed.) (1986), ASM Handbook, Volume 11: Failure Analysis and Prevention, ASM International, Materials Park, Ohio.

    Google Scholar 

  12. Swift, T. (1993), Widespread Fatigue Damage Monitoring —Issues and Concerns, Proceedings of the 5th International Conference on Aging Aircraft, Hamburg, Germany.

    Google Scholar 

  13. T.O. 33B-1-2, Nondestructive Inspection General Procedures and Process Controls (2008), Tinker AFB, Oklahoma.

    Google Scholar 

  14. Brooks, C., Peeler, D., Honeycutt, T. and Prost-Domasky, S. (1999), Predictive Modeling for Corrosion Management: Modeling Fundamentals, Aging Aircraft 1999 Conference, Albuquerque, New Mexico.

    Google Scholar 

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© 2009 Springer-Verlag Berlin Heidelberg

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Shoales, G.A., Fawaz, S.A., Walters, M.R. (2009). Compilation Of Damage Findings From Multiple Recent Teardown Analysis Programs. In: Bos, M.J. (eds) ICAF 2009, Bridging the Gap between Theory and Operational Practice. Springer, Dordrecht. https://doi.org/10.1007/978-90-481-2746-7_11

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  • DOI: https://doi.org/10.1007/978-90-481-2746-7_11

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-90-481-2745-0

  • Online ISBN: 978-90-481-2746-7

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