1. Molent L, Barter SA, Wanhill RJH. The lead crack fatigue lifing framework, DSTO-RR-0353, Defence Science and Technology Organisation, Melbourne, Australia; 2010.
2. Athiniotis N, Barter SA, Clark G. Summary of fatigue cracking in RAAF Macchi MB326H wings, DSTO Technical Report DSTO-TR-0757, Defence Science and Technology Organisation, Melbourne, Australia; 1999.
3. Wanhill RJH, Platenkamp DJ, Hattenberg T, Bosch AF, De Haan PH. GLARE teardowns from the MegaLiner Barrel (MLB) fatigue test, NLR Technical Publication NLR-TP-2009-068, National Aerospace Laboratory NLR, Amsterdam, the Netherlands, 2009. In: Bos MJ, editors. ICAF 2009: Bridging the Gap between Theory and Operational Practice, Springer Netherlands, Dordrecht, the Netherlands, 2009, p. 145–67.
4. Burgess PJ. Extending the life of the RAAF Macchi jet trainer – selection of the Durability and Damage Tolerance philosophy, Australian Aviation Symposium, Canberra, Australia; 1987.
5. Goldsmith NT, Clark G. Analysis of wing main spar cracking. In: Esakul KA, editors. Handbook of Case Histories in Failure Analysis, ASM International, Metals Park, Ohio, USA, 1, 1992. p. 9–11.