Airworthiness and Flight Characteristics Test CH-47C Helicopter (Chinook) Stability and Control
Abstract
The second phase of the CH-47C airworthiness and flight characteristics (A and FC) test program consisted of the stability and control test of the production helicopter. The CH-47C was evaluated to determine compliance with the military specification, MIL-H-8501A, with deviations as defined in the detail specification. The helicopter was also evaluated with respect to its mission as a transport helicopter. The CH-47C stability and control characteristics are acceptable for the transport helicopter mission.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 01, 1972
- Accession Number
- AD0903488
Entities
People
- Alan R. Todd
- Donald G. Broadhurst
- Gary L. Skinner
- John I. Nagata
- Philip J. Bohn
Organizations
- Edwards Air Force Base