NTSB CAROL · Event
Event SEA01TA172
Registry · N458CC
FAA Aircraft Registry record.
Make / Model
WILLIAMS HELICOPTER CORP UH-1H
Year of manufacture
1967 · 34 years old at event
Engine
LYCOMING T53L-703 (1400 hp)
Seats / Engines
15 seats · 1 engine
Last airworthiness date
20120203
ADS-B equipped
Yes — Mode-S A59009
Registrant of record
ELKHORN AVIATION INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot-in-command's failure to maintain seperation/clearance from trees while maneuvering.
Factual narrative
On September 17, 2001, about 1600 mountain daylight time, a Bell 205 helicopter, N458CC, sustained substantial damage following a main rotor blade strike while conducting firefighting operations near Libby, Montana. The helicopter is registered to Billings Flying Service, Billings, Montana, and was being operated by the United States Forest Service (USFS) as a public use aircraft. The commercial pilot, the sole occupant of the helicopter, was not injured. Visual meteorological conditions prevailed, and USFS VFR flight following procedures were in effect. In a written statement dated September 26, 2001, the pilot reported that he was maneuvering near a shoreline in an effort to get a full bucket of water. "I made 40-50 bucket drops on the fire and flew out my fuel cycle before breaking off from the fire and returned to Troy Airport. On the return flight to Troy airport, I noticed a vertical vibration at approximately 90 knots (forward airspeed)." He continued to Troy airport at a slower speed to avoid the vibration. After landing without incident, the pilot noted damage to the helicopter's main rotor blades. He also noted that pine needles had been ingested into the aircraft's induction system. The pilot did not recall coming into contact with anything during the flight. Personnel from the USFS reported that the helicopter was conducting external load long-line (100 feet) operations when the helicopters main rotor blades contacted trees. Postaccident examination of the helicopter, by a certified mechanic, revealed that both main rotor blades sustained substantial damage. The pilot stated that the weather was clear with more than 20 miles visibility, with the sky partially obscured by occasional smoke. The pilot reported no mechanical failure or malfunction of the aircraft. The pilot was returning from an external load long-line firefighting flight when he noticed a vertical vibration above 90 knots. After landing at Troy he noticed damage to the main rotor blades. Subsequently, he noticed that pine needles had been ingested by the helicopter's induction system. The pilot reported that he had no memory of hitting any objects during the operation. The weather was clear with 20 miles visibility, and the sky was partially obscured by smoke. There was no report of mechanical failure or malfunction with the helicopter. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_SEA01TA172.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type. Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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Browse the full corpus — academia portal ↗