The Implications of Handling Qualities in Civil Helicopter Accidents Involving Hover and Low Speed Flight
NASA NTRS · Technical Memorandum (TM) · 20060051639 · Published 2019-07-10 · Ames Research Center · 2 authors
Abstract and citation only, verbatim from NASA NTRS; full text lives there. All credit to the authors and Ames Research Center.
Abstract
Because of increasing accident rates in Army helicopters in hover and low speed flight, a study was made in 1999 of accidents which could be attributed to inadequate stability augmentation. A study of civil helicopter accidents from 1993-2004 was then undertaken to pursue the issue of poor handling qualities in helicopters which, in almost all cases, had no stability augmentation. The vast majority of the mishaps studied occurred during daylight in visual meteorological condition, reducing the impact of degraded visual environments (DVE) on the results. Based on the Cooper-Harper Rating Scale, the handling qualities of many of the helicopters studied could be described as having from "very objectionable" to "major" deficiencies. These costly deficiencies have resulted in unnecessary loss of life, injury, and high dollar damage. Low cost and lightweight augmentation systems for helicopters have been developed in the past and are still being investigated. They offer the potential for significant reductions in the accident rate.
Authors
- Dugan, Daniel C. NASA Ames Research Center
- Delamer, Kevin J. NASA Ames Research Center
Citation
Dugan, Daniel C., Delamer, Kevin J. (2019). The Implications of Handling Qualities in Civil Helicopter Accidents Involving Hover and Low Speed Flight. Ames Research Center. NASA NTRS ID 20060051639. https://ntrs.nasa.gov/citations/20060051639 ↗