U. S. Army Helicopter Hydraulic Servocylinder Reliability and Maintainability Investigation

Abstract

The report describes an investigation carried out to identify, isolate, and verify the causes of problems with hydraulic servocylinder actuators used on U.S. Army helicopters, and to trace the resulting effects on helicopter availability. Design requirements, quality assurance provisions, maintenance procedures and practices were analyzed to assess their impact upon the current problems. The analysis of the pertinent failure data and documentation revealed that five failure modes were responsible for over 90% of the total hydraulic servocylinder removals in a 6 1/2-year period. Subsequent analysis of the various policies, practices and procedures showed that these documents contain anomalies that contribute to the occurrence of the five predominant failure modes. The lack of stringent basic design requirements, quality control, and adequate maintenance manuals was shown to be a major contributor to the leaking failure mode. This mode accounts for approximately half of the servocylinder removals from U.S. Army helicopters.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1973
Accession Number
AD0767243

Entities

People

  • James L. Huffman
  • Sheldon Dockswell

Tags

Communities of Interest

  • Air Platforms
  • Engineered Resilient Systems
  • Ground and Sea Platforms
  • Human Systems
  • Weapons Technologies

DTIC Thesaurus Topics

  • Actuators
  • Air Force
  • Aircraft Equipment
  • Aircrafts
  • Airframes
  • Army Aircraft
  • Birds
  • Engineering
  • Failure Mode And Effect Analysis
  • Fixed Wing Aircraft
  • Helicopters
  • Maintenance
  • Maintenance Management
  • Maintenance Personnel
  • Personnel Management
  • Test And Evaluation
  • Test Methods

Readers

  • Aviation Safety Risk Assessment.
  • Facility/Structural Engineering.
  • Systems Analysis and Design