1. Young G. D., Macchi MB326H Aircraft Structural Integrity Management Plan, Issue 1, RAAF Logistics Systems Agency, Logistics Command, Melbourne, Australia, December 1994.
2. Jones, “Chapter 4, Crack patching: Design aspects”, Bonded repair of aircraft structure, edited by A. A. Baker and R. Jones, Martinus Nijhoff, 1988.
3. Bland, L., “Final engineering report: A8–112 wing pivot fitting failure investigation, (Manufacturing processes)”, FZM-12–5130A, General Dynamics, Fort Worth, USA, June 1982.
4. Jones R., Molent L., Paul J., Saunders T., Chiu W. K. (1994), “Development of a composite repair and the associated inspection intervals for the F111C stiffener runout region”, FAA/NASA International Symposium on Advanced Structural Integrity Methods for Airframes Durability and Damage Tolerance, NASA Conference Publication 3274, Part 1, pp 339–351, 1994.
5. Barter S. and Clark G., Fatigue and fracture control in components from modern military aircraft, Proceedings International Aerospace Congress 1991, Melbourne, Australia, 12–16th May, 1991, Vol 1, pp35–43, 1991.