WAH-64 Apache HUMS Phase-1 Implementation

VFS-F58-00190

6/11/2002

Authors
Abstract
Content

A Health and Usage Monitoring System is being introduced into the WAH-64 Apache (AH-MK1) helicopter. This paper describes the Phase-1 part of the implementation, which includes cockpit voice recording, flight data recording, engine power performance monitoring and engine, aircraft and APU usage monitoring. Growth provisions are provided to introduce Rotor Track and Balance, Transmission Vibration Monitoring, Engine Vibration Monitoring and Airframe Vibration Monitoring in future phases. The HUMS on the WAH-64 Apache is fully integrated with the aircraft onboard avionics system. The HUMS is fully configurable through an upload from the PCMCIA card. This paper presents the WAH-64 Apache Phase-1 design, installation, system integration testing, and aircraft ground and flight testing.

Meta TagsDetails
DOI
https://doi.org/10.4050/VFS-F58-00190
Citation
Cameron, B. and Shanthakumaran, P., "WAH-64 Apache HUMS Phase-1 Implementation," Forum 58 - Montreal, Canada 2002, Montreal, Canada, June 11, 2002, https://doi.org/10.4050/VFS-F58-00190.
Additional Details
Publisher
Published
6/11/2002
Product Code
VFS-F58-00190
Content Type
Technical Paper
Language
English