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Corrosion Control Practices On Commercial Aircraft
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English
Abstract
This paper describes corrosion control practices used in Boeing commercial aircraft. Years of airline service experience and laboratory tests have resulted in a better understanding of the role between metal finishing and design practices. This has resulted in significant improvements in corrosion control practices in today's aircraft. Included are discussions on processing/finishing of metals, the joining of dissimilar materials, sealing practices and drainage management.
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Citation
Marceau, J., "Corrosion Control Practices On Commercial Aircraft," SAE Technical Paper 870747, 1987, https://doi.org/10.4271/870747.Also In
References
- International Air Transport Association “Guidance Material on Design and Maintenance Against Corrosion of Aircraft Structures” Doc. GEN/2637A 2 November 1983
- Fontana M. G. Greene N. D. “Corrosion Engineering” Second McGraw-Hill, Inc. 1983
- 1986 Annual Book of ASTM Standards 03.02
- 1986 Annual Book of ASTM Standards 03.02
- Marceau J. A. et. al. “A Wedge Test for Evaluating Adhesive Bonded Surface Durability” Adhesives Age Oct. 1977
- McMillan J. C. “Surface Preparation - Key to Bondraent Durability” AGARD Lecture Series No. 102 2-3 April 1979 Oslo, Norway
- Douglas Aircraft Company “Primary Adhesively Bonded Structure Technology (PABST) Phase lb: Preliminary Design” 1976 AFFDL-TR-76-141
- Holmquist H. W. “Development of and Service Experience With H 3 PO Anodization” Abstracts of Ninth Annual Meeting of Adhesion Society Feb. 9-12. 1986