Evaluation, Modification And Damage Tolerance Of An In-Service Aircraft Critical Area-Reference-Cited by-同舟云学术

Evaluation, Modification And Damage Tolerance Of An In-Service Aircraft Critical Area

Published:2009 Issue: Volume: Page:301-327
ISSN:
Container-title:ICAF 2009, Bridging the Gap between Theory and Operational Practice
language:
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Author:

Rutledge R. S.,Backman D. S.,Hiscocks R. J.

Publisher

Springer Netherlands

Link

http://link.springer.com/content/pdf/10.1007/978-90-481-2746-7_18.pdf

Reference16 articles.

1. DND, (2001), ‘Canadian Forces Lifing Policy, CF-18 Structural Integrity Standard for Continued Airworthiness, Appendix 9 to Annex A, CF-18 CMATC’.

2. Hiscocks, R., (2006), ‘Test Plan for FT312 CF-18 Wing-Fold Aft-Spar Shear-Tie’, LTR-SMPL-2006-0051, National Research Council Canada.

3. Zavitz, D. et al., (1993), ‘CF/RAAF IFOSTP Post-LEX Period Mission Block (IARPO3) Definition and Analysis’, LTR-ST-1928, National Research Council Canada.

4. Rutledge, R., Hiscocks, R., and Backman, D., (2006) ‘Strain Survey for FT312 CF-18 Wing-Fold Aft Spar Shear-Tie’, LTR-SMPL-2006-0072, National Research Council Canada.

5. Rutledge, R., Hiscocks, R., and Backman, D., (2007), ‘FT312 CF-188 Wing-Fold Aft-Spar Shear-Tie Fatigue Test Final Report’, LTR-SMPL-2007-0103, National Research Council Canada.

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