1. Anon. Fractured trunnion, Boeing B747-300 aircraft, JA 8184 at Sydney Aero., Aviation Safety Investigation Report. Australian Transport Safety Board, Occurrence No. 200502400; June 2006.
2. The lead rack fatigue lifing framework;Molent;Int J Fatigue,2011
3. Dixon B, Molent L, Barter SA, Mau V. Flaw identification through the application of loads: teardown of the F/A-18 centre barrel from USN F/A D buno No. 163507, DSTO-TR-1740, Defence Science and Technology Organisation, Air Vehicles Division, Melbourne, Australia; July 2004.
4. Investigation using quantitative fractography of an unexpected failure in an F/A-18 centre fuselage bulkhead in the FINAL teardown program;Barter;Eng Fail Anal,2009
5. Lewis FG, Glanvill DW, Bishop BC. Accident to Viscount aircraft VH-RMQ – metallurgical examination of components from the wing structure, ARL Applied Report 66, Aeronautical Research Laboratory, Melbourne, Australia; August 1969.