ASN Wikibase Occurrence # 198991
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: | Saturday 30 April 2005 |
Time: | 18:45 |
Type: | Bell 206L-1 LongRanger II |
Owner/operator: | Private |
Registration: | N66RR |
MSN: | 45278 |
Year of manufacture: | 1979 |
Total airframe hrs: | 6931 hours |
Engine model: | Allison 250-C28B |
Fatalities: | Fatalities: 0 / Occupants: 1 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Cherokee, NC -
United States of America
|
Phase: | Unknown |
Nature: | Executive |
Departure airport: | Cherokee, NC |
Destination airport: | Cherokee, NC |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot was repositioning the helicopter to the refueling area behind the helipad, to take on more fuel before flying his next sightseeing operation. He checked that all gauges were in normal operating ranges and that no warning lights were on. The pilot spooled up the helicopter to 100-percent and again, checked to make sure all gauges were in normal operating ranges. The pilot slowly began to raise the collective. The pilot stated that the front end of the helicopter started to raise up and the helicopter began to go backwards before fully off the ground. He continued raising the collective until he noticed that the right rear skid was buried into the gravel. The pilot pushed the collective down immediately and the helicopter rolled to the right onto its side and then came to rest inverted. The pilot did not report any mechanical malfunctions with the helicopter prior to the accident. Examination of the accident site revealed a flat, gravel helipad. Examination of the wreckage revealed the helicopter inverted and the main rotor severed off. The roof of the cabin had crush damage and was detached from the rest of the cabin. Both main rotor blades were bent, the tip of one rotor blade was broken off and the tail rotor drive shaft was damaged. A passing automobile also sustained damage from flying helicopter debris.
Probable Cause: The pilot's improper use of the helicopter flight controls during a hover that resulted in a dynamic rollover.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | ATL05CA077 |
Status: | Investigation completed |
Duration: | |
Download report: | Final report |
|
Sources:
NTSB:
https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20050531X00689&key=1 Location
Revision history:
Date/time | Contributor | Updates |
19-Aug-2017 16:17 |
ASN Update Bot |
Added |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation