[1. I. A. Anderson, R. G. Parker, Full Scale Fatigue Test of the Pilatus PC9/A trainer aircraft, 20th ICAF Symposium, Bellevue, Washington, USA, 14-16 July 1999]Search in Google Scholar
[2. L. Molent, S.A. Barter, P. White, B. Dixon, Damage tolerance demonstration testing for the Australian F/A-18, International Journal of Fatigue pp. 1031-1038, 24 May 200810.1016/j.ijfatigue.2008.05.009]Search in Google Scholar
[3. R. S. Rutledge1, D. S. Backman1 and R. J. Hiscocks1, Evaluation, modification and damage tolerance of an in+service aircraft critical area, 25th ICAF Symposium, Rotterdam, 27–29 May 2009]Search in Google Scholar
[4. S. Klimaszewski, A.Leski, J. Zurek, The Role of AFIT in the Polish Aging Military Aircraft Programs, Proceedings of 7th Joint FAA/DoD/NASA Conference on Aging Aircraft, New Orleans, 9-11 September 2003.]Search in Google Scholar
[5. Klimaszewski S., Leski A., Dragan K., Kurdelski M. Aircraft Structural Integrity Program of Polish Su-22 Fitter. ASIP 2006 Conference, San Antonio 30.11-06.12.2006. USA, www.asipcon.com]Search in Google Scholar