Product-Improvement Test, Maintainability and Reliability Characteristics of the OH-58A Helicopter between 1,200 and 2,400 Flight Hours.

Abstract

Evaluation of data obtained during this test revealed no significant difference in the maintainability and reliability of the OH-58A Helicopter during the 1,200- through 2,400-flight-hour period as compared with the 0- through 1,200-flight hour period. Copies of the complete data printouts are attached for each of the test helicopters.

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Feb 29, 1972
Accession Number
ADA061868

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Artificial Intelligence
  • Capillary Electrophoresis
  • Carbonate Esters
  • Flight
  • Helicopters
  • Instruction Set Architecture
  • Maintainability
  • Microarchitecture
  • Mission Profiles
  • Observation Aircraft
  • Plastic Explosives
  • Reliability
  • Test And Evaluation
  • Three Dimensional
  • United States

Readers

  • Aerospace Engineering
  • Aviation Science / Aeronautics.
  • Business Analytics