Skip to main content

Multiple-Site Damage in Riveted Lap Joints – Experimental Observations

  • Chapter
  • First Online:
Riveted Lap Joints in Aircraft Fuselage

Part of the book series: Solid Mechanics and Its Applications ((SMIA,volume 189))

  • 2805 Accesses

Abstract

The present chapter is divided into two sections. In Sect. 8.1, two passenger aircraft accidents due to multiple-site damage (MSD) of riveted lap joints are described in detail. Section 8.2 presents some results of experimental investigations into MSD performed on full-scale fuselage panels and lap joint specimens.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 129.00
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 169.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 169.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Notes

  1. 1.

    Research into residual strength of fuselage panels will be considered in detail in Chap. 10.

References

  • Ahmed, A., Bakuckas, J.G., Jr., Tan, P.W., Awerbuch, J., Lau, A.C., Tan, T.-M.: Growth of multiple-site damage (MSD) in an undamaged fuselage lap joint curved panel. In: Proceedings of 7th Joint FAA/DoD/NASA Conference on Aging Aircraft, New Orleans, LA, 8–11 Sept 2003 (2003)

    Google Scholar 

  • Ahmed, A., Bakuckas, J.G., Jr., Averbuch, J., Lau, A.C., Tan, T.-M.: Evolution of multiple-site damage in the riveted lap joint of fuselage panel. In: Proceedings of 8th Joint NASA/FAA/DoD Conference on Aging Aircraft, Palm Springs, CA, Jan 31–Feb 3 2005 (2005)

    Google Scholar 

  • Aircraft Accident Report, Aloha Airlines, Flight 243, Boeing 737–200, N73711, near Manui, Hawaii, April 28, 1988, Report No. NTSB/AAR-89/03. National Transportation Safety Board, Washington, D.C. (June 1989)

    Google Scholar 

  • Bakuckas, J.G., Jr.: Full-scale testing and analysis of fuselage structures containing multiple cracks. Final Report, DOT/FAA/AR-01/46 (July 2002)

    Google Scholar 

  • Bakuckas, J.G., Jr., Bigelow, C.A., Tan, P.W.: Characterization of fatigue behaviour of aircraft fuselage structures. In: Guillaume, M. (ed.) Proceedings of 22nd ICAF Symposium, Fatigue of Aeronautical Structures as an Engineering Challenge, Lucerne, Switzerland, 7–9 May 2003, pp. 341–360. EMAS, Warley (2003)

    Google Scholar 

  • Bakuckas, J.G., Jr., Mosinyi, B., Steadman, D., Awerbuch, J., Lau, A.C., Tan, T.-M.: Teardown inspection and extended fatigue test of fuselage lap joints from retired passenger service airplane. In: Lazaretti L., Salvetti S. (eds.) Proceedings of 24th ICAF Symposium, Durability and Damage Tolerance of Aircraft Structures; Metals vs Composites, Naples, Italy, 16–18 May 2007, pp. 749–768. Publ. Pacini, Naples (2007)

    Google Scholar 

  • Blom, A.F.: Fatigue science and engineering – achievements and challenges. In: Rouchon, J. (ed.) 18th Plantema Memorial Lecture, Proceedings of 21th ICAF Symposium, Design for Durability in the Digital Age, Tolouse, France, 27–29 June 2001, pp. 3–63. Cépaduès Edition, Touluse (2001)

    Google Scholar 

  • Eastin, R., Mowery, J.: Aircraft structural fail safety: a noble but problematic concept. In: Lazaretti, L., Salvetti, S. (eds.) Proceedings of 24th ICAF Symposium, Durability and Damage Tolerance of Aircraft Structures; Metals vs Composites, Naples, Italy, 16–18 May 2007, pp. 55–72. Publ. Pacini, Naples (2007)

    Google Scholar 

  • Fredell, R.S.: Damage tolerant repair techniques for pressurized aircraft fuselages. Ph.D. thesis, TU Delft, Delft (1994)

    Google Scholar 

  • Gruber, M.L., Wilkins, K.E., Worden, R.E.: Investigation of fuselage structure subject to widespread fatigue damage. In: Bigelow, C.A. (ed.) Proceedings of FAA/NASA Symposium on the Continued Airworthiness of Aircraft Structures, Atlanta, GA, 28–30 Aug 1996. DOT/FAA/AR-97/2, pp. 439–459 (1997)

    Google Scholar 

  • Johnson, K.E., Ahmed, A., Bakuckas, J.G. Jr., Awebuch, J., Lau, A., Tan, T.-M.: Multiple-site damage nucleation and growth in a fuselage lap joint. In: Lazaretti, L., Salvetti, S. (eds.) Proceedings of 24th ICAF Symposium, Durability and Damage Tolerance of Aircraft Structures; Metals vs. Composites, Naples, Italy, 16–18 May 2007, pp. 988–1005. Publ. Pacini, Naples (2007)

    Google Scholar 

  • Kosai, M., Kobayashi, A.S., Ramulu, M.: Tear straps in airplane fuselage. In: Atluri S.N., Harris C.E., Hoggart A., Miller N., Sampath S.N. (eds.) International Workshop on Structural Integrity of Ageing Airplanes, Durability of Metal Aircraft Structures, Atlanta, GA, 31 Mar–2 Apr 1992, pp. 443–457. Atlanta Technical Publications, Atlanta (1992)

    Google Scholar 

  • Maclin, J.R.: Performance of fuselage pressure structure. In: Harris, C.E. (ed.) Proceedings of 3rd International Conference on Aging Aircraft and Structural Airworthiness, Washington D.C., 19–21 Nov 1991, vol. 3160, pp. 67–74. NASA Conference Publications (1991)

    Google Scholar 

  • Miller, M., Gruber, M.L., Wilkins, K.E, Worden, R.E.: Full-scale testing and analysis of fuselage structure. In: Harris, Ch.E. (ed) Proceedings of FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, Hampton, VA, 4–6 May 1994. NASA CP 3274, pp. 481–496 (1994)

    Google Scholar 

  • Müller, R.P.G.: An experimental and analytical investigation on the fatigue behaviour of fuselage riveted lap joints. The significance of the rivet squeeze force, and a comparison of 2024-T3 and Glare 3. Ph.D. thesis, TU Delft, Delft (1995)

    Google Scholar 

  • Müller, R.P.G., Hart-Smith, L.J.: Making fuselage riveted lap splices with 200-year crack-free-lives. In: Cook, R., Poole, P. (eds.) Proceedings of 19th ICAF Symposium, Fatigue in New and Aging Aircraft, Edinburgh, Scotland, 18–20 June 1997, pp. 499–522. EMAS, Warley (1997)

    Google Scholar 

  • Ottens, H.H.: Multiple crack initiation and crack growth in riveted lap joint specimens. In: Grandage, J.M., Jost, G.S. (eds.) Proceedings of 18th ICAF Symposium, Estimation, Enhancement and Control of Aircraft Fatigue Performance, Melbourne, Australia, 3–5 May 1995, pp. 487–506. EMAS, Warley (1995)

    Google Scholar 

  • Piascik, R.S., Willard, S.A.: The characterisation of multi-site damage in the fuselage riveted lap splice joint. In: Cook, R., Poole, P. (eds.) Proceedings of 19th ICAF Symposium, Fatigue in New and Ageing Aircraft, Edinburgh, Scotland, 18–20 June 1997, pp. 93–114. EMAS, Warley (1997)

    Google Scholar 

  • Piascik, R.S., Willard, S.A., Miller, M.: The characterisation of widespread fatigue damage in fuselage structure. In: Harris, Ch.E. (ed.) Proceedings of FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, Hampton, VA, 4–6 May 1994. NASA CP 3274, pp. 563–580 (1994)

    Google Scholar 

  • Samavedam, G., Thomson, D., Jeong, D.Y.: Evaluation of the fuselage lap joint fatigue and terminating action repair. In: Harris, Ch.E. (ed.) Proceedings of FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage, Hampton, VA, 4–6 May 1994, NASA CP 3274, pp. 653–664 (1994)

    Google Scholar 

  • Schijve, J.: Multiple-site-damage of riveted joints. In: Atluri S.N., Harris C.E., Hoggart A., Miller N., Sampath S.N. International Workshop on Structural Integrity of Ageing Airplanes, Durability of Metal Aircraft Structures, Atlanta, GA, 31 Mar–2 Apr 1992. Atlanta Technical Publication, Atlanta, GA, pp. 2–27 (1992)

    Google Scholar 

  • Schijve, J.: Multiple-site damage in aircraft fuselage structures. Fatigue Fract. Eng. Mater. Struct. 18, 329–344 (1995)

    Article  Google Scholar 

  • Schijve, J.: Fatigue of Structures and Materials, 2nd edn. Springer, Dordrecht/Heidelberg/London/New York (2009a) (with CD-Rom)

    Book  Google Scholar 

  • Schijve, J.: Fatigue damage in aircraft structures, not wanted, but tolerated? Int. J. Fatigue 31, 998–1011 (2009b)

    Article  MATH  Google Scholar 

  • Schra, L., Ottens, H.H., Vlieger, H.: Fatigue crack growth in simulated Fokker 100 lap joints under MSD and SSD conditions. Report NLR CR 95729 C. NLR, Amsterdam (1995)

    Google Scholar 

  • Skorupa, M.: Load interaction effects during fatigue crack growth under variable amplitude loading – a literature review. Part I: Empirical trends. Fatigue Fract. Eng. Mater. Struct. 21, 987–1006 (1998)

    Article  Google Scholar 

  • Steadman, D., Carter, A., Ramakrishnan, R.: Characterisation on MSD in an in-service fuselage lap joint. In: 3rd Joint FAA/DoD/NASA Conference on Aging Aircraft, Albuquerque, NM, Sept 1999 (Proceedings on CD-Rom)

    Google Scholar 

  • Swift, T.: Damage tolerance in pressurized fuselages. In: Simpson, D.L. (ed.) Proceedings of 14th ICAF Symposium, New Materials and Fatigue Resistant Aircraft Design, Ottawa, Canada, 8–12 June 1987. 11th Plantema Memorial Lecture, pp. 1–77. EMAS, Warley (1987)

    Google Scholar 

  • Terada, H.: A proposal on damage tolerant testing for structural integrity of aging aircraft – Learning from JAL accident in 1985. In: Erdogan, F. (ed.) Fracture Mechanics. ASTM STP 1220, vol. 25, pp. 557–574. ASTM, Philadelphia (1995)

    Google Scholar 

  • Terada, H.: Structural fatigue and joint degradation. Int. J. Fatigue 23, 21–30 (2001)

    Article  Google Scholar 

  • Vlieger, H.: Results of uniaxial and biaxial tests on riveted fuselage lap joint specimens. In: Harris, Ch.E (1994) Proceedings of FAA/NASA International Symposium of Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, Hampton, VA, 4–6 May 1994. NASA CP 3274, pp. 911–930 (1994)

    Google Scholar 

  • Vlot, A.: Glare. History of the Development of a New Aircraft Material. Kluwer Academic, Dordrecht (2001)

    Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Rights and permissions

Reprints and permissions

Copyright information

© 2012 Springer Science+Business Media Dordrecht

About this chapter

Cite this chapter

Skorupa, A., Skorupa, M. (2012). Multiple-Site Damage in Riveted Lap Joints – Experimental Observations. In: Riveted Lap Joints in Aircraft Fuselage. Solid Mechanics and Its Applications, vol 189. Springer, Dordrecht. https://doi.org/10.1007/978-94-007-4282-6_8

Download citation

  • DOI: https://doi.org/10.1007/978-94-007-4282-6_8

  • Published:

  • Publisher Name: Springer, Dordrecht

  • Print ISBN: 978-94-007-4281-9

  • Online ISBN: 978-94-007-4282-6

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics