ASN Wikibase Occurrence # 293545
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information.
If you feel this information is incomplete or incorrect, you can
submit corrected information.
Date: | Sunday 26 June 2005 |
Time: | 13:00 LT |
Type: | Air Command 532 Commander Elite |
Owner/operator: | Private |
Registration: | UNREG |
MSN: | 1 |
Fatalities: | Fatalities: 1 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Highgate, Vermont -
United States of America
|
Phase: | Unknown |
Nature: | Private |
Departure airport: | Highgate-Franklin County State Airport, VT (KFSO) |
Destination airport: | |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot purchased the used gyroplane about 2 weeks prior to the accident. After assembling it, and 2 days before the accident, he conducted a series of touch and go landings, or "crow hops" along a runway. The day before the accident flight was his first flight. During the accident flight, a main rotor blade "folded," and the gyroplane descended nose first into wooded terrain. Examination of the wreckage revealed airframe and rotor blade marks, consistent with retreating rotor blade stall, which could have resulted from either pilot input or "a sharp downdraft." Winds, about the time of the accident, at an airport 25 nautical miles to the south, were 7 knots, with no wind gusts reported. The make and model of gyroplane was known to be unstable, and the pilot was at least aware of a recommended upgrade kit to enhance stability, but had not installed it. The pilot was not rated in gyroplanes, and had spoken to a flight instructor about training, but then decided to self-train. The pilot also did not possess a repairman's certificate for the gyroplane.
Probable Cause: The pilot's improper cyclic input, which resulted in a retreating rotor blade stall, and its subsequent impact with the propeller. Also causal, was the pilot's failure to acquire proper training. A factor was the pilot's decision not to have a stability upgrade kit installed prior to flying the gyroplane.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | IAD05LA085 |
Status: | Investigation completed |
Duration: | 1 year and 2 months |
Download report: | Final report |
|
Sources:
NTSB IAD05LA085
Revision history:
Date/time | Contributor | Updates |
10-Oct-2022 07:30 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation