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Atlas / NTSB / FTW95LA105

NTSB CAROL · Event

Event FTW95LA105

1995-02-01 EL INDIO, Texas, United States Minor 1 aircraft Status: Completed

Registry · N6SR

FAA Aircraft Registry record.

Make / Model

EPIC AIRCRAFT LLC E1000

Year of manufacture

2021

TCDS

A00059SE · EPIC AIRCRAFT LLC

Engine

P&W CANADA PT6A-67A (1200 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

20211119

ADS-B equipped

Yes — Mode-S A7C42D

Registrant of record

BLACKHAWK AVIATION II LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

THE LOSS OF TAIL ROTOR EFFECTIVENESS. A FACTOR WAS THE GUSTY RIGHT QUARTERING TAILWIND.

Factual narrative

On February 1, 1995, approximately 1500 central standard time, a Bell 47G-4A, N6SR, was destroyed when it impacted terrain while maneuvering near El Indio, Texas. The airline transport rated pilot and one passenger were not injured, but a second passenger received minor injuries. Visual meteorological conditions prevailed. The following is based on the pilot/operator report. The helicopter was being used for predator control and was chasing a bobcat about 25 feet above the ground. The pilot said a right quartering tailwind gust caused the helicopter to lose tail rotor effectiveness and it began spinning to the right. He increased collective and throttle in an attempt to regain airspeed, but this caused the main rotor RPM to droop and altitude was insufficient to allow the helicopter to regain airspeed by diving. He then reduced collective to regain RPM, but the helicopter continued to spin and impacted the terrain. THE HELICOPTER, BEING USED FOR PREDATOR CONTROL, WAS 25 FEET ABOVE THE GROUND AND WAS CHASING A BOBCAT. THE PILOT SAID A RIGHT QUARTERING TAILWIND GUST CAUSED THE HELICOPTER TO LOSE TAIL ROTOR EFFECTIVENESS AND IT BEGAN SPINNING TO THE RIGHT. THE PILOT INCREASED COLLECTIVE AND THROTTLE IN AN ATTEMPT TO REGAIN AIRSPEED, BUT THIS CAUSED THE MAIN ROTOR RPM TO DROOP AND ALTITUDE WAS INSUFFICIENT TO ALLOW THE HELICOPTER TO REGAIN AIRSPEED BY LOWERING THE NOSE. THE PILOT THEN REDUCED COLLECTIVE TO REGAIN RPM, BUT THE HELICOPTER CONTINUED TO SPIN AND IMPACTED THE TERRAIN. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_FTW95LA105.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.