ASN Wikibase Occurrence # 160559
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| Date: | Monday 16 September 2013 |
| Time: | 15:35 |
| Type: |  Bell UH-1B Iroquois |
| Owner/operator: | R&R Conner |
| Registration: | N204UH |
| MSN: | 554 |
| Year of manufacture: | 1962 |
| Engine model: | Lycoming T5313B |
| Fatalities: | Fatalities: 1 / Occupants: 1 |
| Aircraft damage: | Substantial |
| Category: | Accident |
| Location: | Near Detroit, Oregon -
 United States of America
|
| Phase: | Manoeuvring (airshow, firefighting, ag.ops.) |
| Nature: | External load operation |
| Departure airport: | Detroit, OR |
| Detroit, OR | |
| Investigating agency: | NTSB |
| Confidence Rating: |  Accident investigation report completed and information captured |
Witnesses reported that, when the helicopter was just above the trees during an external load logging operation, they either observed or heard the load of logs release early and impact the ground hard. Witnesses then observed the helicopter’s tailboom separate from the fuselage and descend through the trees. The fuselage impacted the ground inverted, and the tailboom came to rest about 140 ft away. A mechanic reported that the pilot had indicated before the flight that the helicopter felt like it “shuffled” during translational lift; however, the mechanic suspected that the transmission mounts were starting to wear and would need to be changed at a later date.
Postaccident examination of the airframe and engine revealed control continuity throughout the airframe except for a portion of the tail rotor drive shaft that extended from the transmission, which was not found. The tailboom had separated from the aft fuselage at the tailboom attachment points. The lower two tailboom attachment fittings exhibited features consistent with overstress failure and did not show indications of fatigue and/or other failure modes. The upper two tailboom attachment fittings both contained fatigue cracks throughout almost the entire fracture surface.
The pilot purchased the helicopter about 3 years before the accident; that same year, the helicopter was issued a new airworthiness certificate. According to the Federal Aviation Administration, the previous owner had relinquished the helicopter’s airworthiness certificate to avoid punitive action for poor maintenance of the helicopter. Maintenance records located within the helicopter did not contain sufficient information to determine when the most recent maintenance was performed; however, the documents did reveal that several component inspections were not completed within the manufacturer’s recommended time. It is likely that long-term, inadequate maintenance of the helicopter contributed to the failure and separation of the tailboom.
Probable Cause: The fatigue failure of the upper two tailboom attachment points, which resulted in the tailboom separating from the fuselage during logging operations. Contributing to the accident was poor maintenance throughout the helicopter’s operational life.
Accident investigation:
 |
|
Sources:
NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=N204UH
History of this aircraft
Other occurrences involving this aircraft
| 5 May 1999 | N97HM | Whitewater Tranport Co. | 1 | Wrangell, AK | |
non |
| Construction | ||||||
Location
Revision history:
| Date/time | Contributor | Updates |
|---|---|---|
| 17-Sep-2013 07:12 | gerard57 | Added |
| 17-Sep-2013 07:13 | harro | Updated [Aircraft type] |
| 17-Sep-2013 16:11 | Geno | Updated [Time, Registration, Cn, Source] |
| 23-Sep-2013 03:57 | Anon. | Updated [Narrative] |
| 21-Dec-2016 19:28 | ASN Update Bot | Updated [Time, Damage, Category, Investigating agency] |
| 29-Nov-2017 09:14 | ASN Update Bot | Updated [Operator, Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative] |
| 09-Mar-2024 17:42 | harro | Updated [Cn, Other fatalities, Source] |
Corrections or additions? ... Edit this accident description
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