ASN Wikibase Occurrence # 284494
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: | Wednesday 1 August 2007 |
Time: | 15:35 LT |
Type: | Bell 206B JetRanger III |
Owner/operator: | Rotors Of The Rockies |
Registration: | N568TD |
MSN: | 2976 |
Year of manufacture: | 1980 |
Total airframe hrs: | 9353 hours |
Engine model: | Rolls Royce 250-620B |
Fatalities: | Fatalities: 0 / Occupants: 4 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Broomfield, Colorado -
United States of America
|
Phase: | Unknown |
Nature: | Unknown |
Departure airport: | Broomfield-Rocky Mountain Metropolitan Airport, CO (BJC/KBJC) |
Destination airport: | Broomfield-Rocky Mountain Metropolitan Airport, CO (BJC/KBJC) |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:According to the pilot, this was his sixth sightseeing flight of the day. He had just landed and three passengers disembarked. Three other passengers boarded the helicopter. As the pilot brought the throttle to full rpm and increased torque, the helicopter turned left about 15 degrees. Approximately 3 inches of opposite pedal was used to bring the helicopter back to its original heading. The pilot continued to increase torque and as the skids started to come off the ground, the nose pitched up rapidly and the helicopter rolled to the right. The left skid was about 3 inches off the ground during the yaw. The right skid never left the ground. Full forward and left cyclic had no effect. The pilot then lowered collective and tried to roll off the throttle. The helicopter rolled right until the main rotor blades contacted the ground. A piece of main rotor blade struck a nearby hangar. The pilot reported no control anomalies and a subsequent examination revealed no discrepancies. FAA's "Rotorcraft Flying Handbook" (FAA-H-8083-21) defines "dynamic rollover" as "the tendency of a helicopter to continue rolling when the critical angle is exceeded, if one gear is on the ground, and the helicopter is pivoting around that point."
Probable Cause: The pilot's failure to maintain control of the helicopter, resulting in an inadvertent dynamic rollover.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | DEN07LA132 |
Status: | Investigation completed |
Duration: | 1 month |
Download report: | Final report |
|
Sources:
NTSB DEN07LA132
Revision history:
Date/time | Contributor | Updates |
30-Sep-2022 17:36 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation