Sneak Circuit Analysis of F-4C Flight Control System,
Abstract
This report documents the results of a Sneak Circuit Analysis which was performed on the F-4C Flight Control System and describes how the analysis was performed. This analysis uncovered 4 sneak circuits and 16 drawing errors. Fourteen design concern reports were prepared describing possible weaknesses in the design and causes for failure of components. High failure-rate components in the Control Amplifier were analyzed to determine the effect each component failure has on the flight of the aircraft. This analysis has shown that Sneak Circuit Analysis can uncover problems which have existed over several years resulting in unscheduled maintenance but which have not been identified by extensive testing, troubleshooting, and other methods of analysis. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 17, 1974
- Accession Number
- ADA108029
Entities
People
- Paul F. Stokes
Organizations
- Boeing