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Atlas / NTSB / FTW96TA383

NTSB CAROL · Event

Event FTW96TA383

1996-09-10 RANGELY, Colorado, United States None 1 aircraft Status: Completed

Registry · N1335X

FAA Aircraft Registry record.

Make / Model

BELL 47G-3B-1

Year of manufacture

1966 · 30 years old at event

TCDS

2H3 · SCOTT'S-BELL 47 INC

Engine

LYCOMING TVO-435-GIA (280 hp)

Seats / Engines

3 seats · 1 engine

Last airworthiness date

20050608

ADS-B equipped

Yes — Mode-S A08973

Registrant of record

HENDRICKSON FLYING SERVICE INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

the pilot's excessive cyclic control input during a low altitude operation, and his failure to maintain altitude/clearance from high vegetation (sage brush). The proximity of high vegetation was a related factor.

Factual narrative

On September 10, 1996, approximately 1615 mountain daylight time, a Bell 47G-3B-1, N1335X, was substantially damaged during a hard landing near Rangely, Colorado. The private pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the business flight conducted under Title 14 CFR Part 91. The flight originated near Rangely approximately 1530. The following is based on the Pilot/Operator Aircraft Accident Report and a conversation the pilot had with an FAA inspector. The pilot was working under a Bureau of Land Management contract. While attempting to turn some horses, he applied excessive aft cyclic control and the tail rotor struck a large sage brush. Directional control was lost and the helicopter turned right. The pilot attempted a "hovering autorotation" from 15 feet and a hard landing ensued. The main rotor blades struck and severed the tail boom, and the right skid collapsed. While attempting to turn some horses, the pilot applied excessive aft cyclic control and the tail rotor struck a large sage brush. Directional control was lost and the helicopter turned right. The pilot attempted a 'hovering autorotation' from 15 feet and a hard landing ensued. The main rotor blades struck and severed the tail boom, and the right skid collapsed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1996_FTW96TA383.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.