ASN Wikibase Occurrence # 195192
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| Date: | Tuesday 2 May 2017 |
| Time: | 18:15 |
| Type: |  Bell 206B-3 JetRanger III |
| Owner/operator: | Marion Co Sheriff's Office |
| Registration: | N911GE |
| MSN: | 5271 |
| Year of manufacture: | 2001 |
| Total airframe hrs: | 8966 hours |
| Engine model: | Rolls-Royce 250-C20 SER |
| Fatalities: | Fatalities: 0 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | near Fort McCoy, Marion County, FL -
 United States of America
|
| Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
| Nature: | Fire fighting |
| Departure airport: | Ocala-Taylor Field, FL (OCF/KOCF) |
| Ocala-Taylor Field, FL (OCF/KOCF) | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
The commercial helicopter pilot had completed 25 to 30 water drops in a fire zone using a firefighting bucket on suspension cables. After refueling, he completed three or four additional drops and then filled and pulled the bucket from the water and immediately felt “a severely out of CG [center of gravity] condition to the right.” He assumed that the bucket cables were entangled in the right landing skid, so he released the water from the bucket. The condition persisted, so he rocked the helicopter to attempt to free the cable without success. He then released the cable with the cargo release button and heard the “clunk” sound typically heard when the bucket was released, but then he heard another “clunk.” The helicopter then began to spin violently and crashed into the water.
Examination of the wreckage revealed 6-inch long cable marks on the right rear landing skid tube and a torsional fracture of the tail rotor short shaft. Based on the pilot’s statement, the cable marks likely occurred initially when a cable became entangled on the skid tube, followed by the fracture of the tail rotor shaft due to cable or bucket contact with the tail rotor assembly. The pilot reported that there were no preaccident mechanical malfunctions or anomalies with the helicopter that would have precluded normal operation.
Probable Cause: The pilot's failure to maintain adequate clearance between the helicopter's skid and the firefighting bucket and suspension cable, which resulted in the cable becoming entangled on the landing skid and a subsequent loss of helicopter control.
Accident investigation:
 |
|
Sources:
NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=911GE
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 03-May-2017 11:00 | gerard57 | Added |
| 03-May-2017 11:03 | gerard57 | Updated [Narrative] |
| 03-May-2017 15:20 | Geno | Updated [Aircraft type, Registration, Cn, Operator, Location, Source, Damage] |
| 19-Nov-2018 14:41 | Aerossurance | Updated [Time, Aircraft type, Location, Source, Narrative] |
| 28-Nov-2018 14:44 | ASN Update Bot | Updated [Time, Operator, Nature, Departure airport, Destination airport, Source, Narrative, Accident report, ] |
| 30-May-2023 00:30 | Ron Averes | Updated [[Time, Operator, Nature, Departure airport, Destination airport, Source, Narrative, Accident report, ]] |
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