ASN Wikibase Occurrence # 357144
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| Date: | Monday 1 July 1996 |
| Time: | 07:00 LT |
| Type: |  Bell 206B III |
| Owner/operator: | Joe Brigham Inc. |
| Registration: | N444JB |
| MSN: | 3258 |
| Year of manufacture: | 1981 |
| Engine model: | Allison 250-C20 |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | South Carver, MA -
 United States of America
|
| Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
| Nature: | Agricultural |
| Departure airport: | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
The pilot was doing aerial spraying of a cranberry bog, and had completed four passes before he executed a right turn to the north to begin the next run. After completing the turn, the helicopter began to spin to the right. After about three to four turns it stopped in a level hover, but then started spinning again to the right. After another three to four spins, it again stopped, and began a final spin to the right when it collided with the bog. Bell Helicopter Textron (BHT) published an Operations Safety Notice, in 1983, which dealt with unanticipated right yaw of the Bell 206 series. It stated that unanticipated right yaw could occur when maneuvering between hover and 30 MPH, and that a tail wind could reduce relative wind speed if a down wind translation occurred. It also stated that a loss of translational lift could result in a high power demand and an additional anti-torque requirements, which included high power demand situations such as low speed downwind turns. A local automated weather report indicated that the winds from were from 210 degrees at 6 knots. The pilot stated that the uncontrolled event initiated when he had completed a right hand application turn, and did not report a lateral cyclic displacement during the last application run.
Probable Cause: The pilot's failure to maintain control of the helicopter during an aerial application maneuver. This put the helicopter in a low slow down wind, high power demand turn, where it encountered a loss of tail rotor effectiveness, and the subsequent collision with the marsh.
Accident investigation:
 |
|
Sources:
NTSB NYC96LA135
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 13-Mar-2024 14:43 | ASN Update Bot | Added |
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