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Cracking in cargo aircraft main landing gear truck beams due to abusive grinding following chromium plating

  • Published:2005-06 Issue:3 Volume:12 Page:337-347
  • ISSN:1350-6307
  • Container-title:Engineering Failure Analysis
  • language:en
  • Short-container-title:Engineering Failure Analysis

Author:

Eliaz Noam,Sheinkopf Haim,Shemesh Gil,Artzi Hillel

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference7 articles.

1. MIL-I-6868. Inspection process. Magnetic particles

2. MIL-STD-1501. Chromium plating, low embrittlement, electrodeposition

3. MIL-STD-866B. Grinding of chrome plated steel and steel parts heat treated to 180,000 psi or over

4. MIL-STD-870. Cadmium plating, low embrittlement, electrodeposition

5. Elementary engineering fracture mechanics;Broek,1984

Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Microstructure Modifications due to Abusive Grinding Resulted in Unexpected Catastrophic Failure of Main Landing Gear in Civilian Aircraft;Journal of Failure Analysis and Prevention;2023-01-30

2. Fatigue fracture analysis of helicopter landing gear cross tube;Engineering Failure Analysis;2021-11

3. Fatigue stress concentration sensitivity and stress ratio effect of a 40CrNi2Si2MoVA steel;Materials Letters;2017-01

4. Suspension and landing gear failures;Handbook of Materials Failure Analysis with Case Studies from the Aerospace and Automotive Industries;2016

5. Design evaluation of the fractured main landing gear of a BAE Jetstream SX-SKY aircraft;International Journal of Structural Integrity;2015-08-10
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