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Atlas / NTSB / SEA98LA146

NTSB CAROL · Event

Event SEA98LA146

1998-07-24 LIBBY, Montana, United States Serious 1 aircraft Status: Completed

Registry · N83NW

FAA Aircraft Registry record.

Make / Model

CESSNA 500

Year of manufacture

1976 · 22 years old at event

Engine

P&W CANADA JT15D-1

Seats / Engines

8 seats · 2 engines

Last airworthiness date

19901121

ADS-B equipped

Yes — Mode-S AB5742

Registrant of record

BAS PART SALES LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

A failure of the external load cable, which became entangled in the tail rotor.

Factual narrative

On July 24, 1998, approximately 0830 mountain daylight time, a Garlick UH-1H, N83NW, sustained substantial damage during an emergency landing while helicopter logging 45 miles north or Libby, Montana. The commercial pilot, the sole occupant, sustained a broken arm. The operation was operating in visual meteorological conditions at the time of the accident. The pilot stated that he was hooked up to a tree length root wad which had been knocked over and topped. He picked up the tree length and laid it over 180 degrees from its original position in order to break the roots from the ground. With the roots loose, he started a takeoff and the tree left the ground and was in the air for approximately 25-50 yards. The roots then impacted the ground, the Kevlar long line snapped about midpoint and the broken end rebounded up into the tail rotor. The pilot stated that he immediately realized he had a tail rotor failure. He informed the ground crew and found the only open area, which was approximately 100 yards from the point of failure. On the second 360 degree spin, he chopped the throttle when the nose was pointed at the intended crash site. He stated that he realized he was too low to make it, so he pulled pitch, which put him in a rapid spin. He struck some trees on his second or third spin and then fell. After impact, he evacuated from the helicopter. The pilot stated that while conducting external load logging operations, he was hooked up to a tree length root wad which had been knocked over and topped. He picked up the tree length and laid it over 180 degrees from its original position in order to break the roots from the ground. With the roots loose, he started a takeoff and the tree left the ground and was in the air for approximately 25-50 yards. The roots then impacted the ground; the Kevlar long-line snapped about midpoint and the broken end rebounded up into the tail rotor. The pilot stated that he immediately realized he had a tail rotor failure. He informed the ground crew and found the only open area, which was approximately 100 yards from the point of failure. On the second 360 degree spin, he reduced power when the nose was pointed at the intended crash site. He stated that he realized he was too low to make it, so he pulled pitch, which put him in a rapid spin. He struck some trees on his second or third spin and then fell. After impact, he evacuated from the helicopter. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1998_SEA98LA146.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

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.

Browse the full corpus — academia portal ↗