Failure Analysis, Cadmium Brush Plate Qualification and Salt Fog Testing of the AH-64 Shock Strut Mount, P/N 7-311113409

Abstract

A failure analysis was performed on a shock strut mount from an AH-64 Apache attack helicopter. It was concluded that the failure was attributed to stress corrosion cracking and/or corrosion fatigue and had initiated at a region where the protective cadmium plating was worn away in service. Based upon this conclusion, it was necessary to qualify two facilities (Hunter Army Air Field, Savannah, GA and Ft. Lewis, Dupont, WA) for the cadmium brush plating rework of these components found to have worn coatings during routine inspections. The U.S. Army Research Laboratory was involved in the qualification process for both facilities, and the results of each quality audit are included. Finally, the results of salt fog testing of cadmium brush plated specimens, plated at the respective facilities, are also included, as well as a comparison of the grain size of the material in the failed component vs. the material from the struts plated at each facility. a

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 2002
Accession Number
ADA409732

Entities

People

  • Marc S. Pepi

Organizations

  • United States Army Research Laboratory

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force Facilities
  • Aircrafts
  • Chemistry
  • Corrosion
  • Engineering
  • Environment
  • Grain Size
  • Hydrogen Embrittlement
  • Iron
  • Manufacturing
  • Materials
  • Mechanical Working
  • Mechanics
  • Military Research
  • Stress Corrosion
  • Stress Corrosion Cracking
  • Tensile Strength

Readers

  • Fluid Dynamics.
  • Software Engineering
  • Surface Engineering/Surface Coating Technology.