1. Cox , A. F 1988 Fatigue Cracking in the Upper Plate of Wing Pivot Fittings in F-111 Aircraft Aeronautical and Maritime Research Laboratory
2. Anon 1988 RAAF F-111C Durability and Damage Tolerance Analysis Details Lockheed Martin Corporation
3. McDonald ., M Watters , K. C Burchill , M. Kaye , R 2000 Summary of F-111 Wing Pivot Fitting Finite Element Stress Analysis Investigations Aeronautical and Maritime Research Laboratory
4. Molent , L. Swanton , G 1994 A Parametric Survey of Cracking in RAAF F-111C WPF Stiffeners Aeronautical and Maritime Research Laboratory
5. Paul , J. 1999 F-111 Stiffener Run Out #2 Parametric Study Aeronautical and Maritime Research Laboratory