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Atlas / NTSB / FTW96LA005

NTSB CAROL · Event

Event FTW96LA005

1995-10-03 EDINBURG, 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 pilot's improper takeoff planning which resulted in the loss of conrol. A factor was the gusty crosswind condition.

Factual narrative

On October 3, 1995, at 1310 central daylight time, a Bell 47G-4A, N6SR, registered and operated by Smith Helicopters under Title 14 CFR Part 91 was substantially damaged following a loss of control near Edinburg, Texas. Visual meteorological conditions prevailed for the local flight and a flight plan was not filed. The airline transport rated pilot and one passenger were not injured, while another passenger received minor injuries. The flight was originating, at the time of the accident, from the Santa Anita Ranch. According to the pilot, he lifted off from a flat bed trailer and was hovering at a height of 6 feet. As the helicopter transitioned forward (approximately 20 knots indicated airspeed) and at a height estimated at 15 to 20 feet AGL, the helicopter encountered a 30 knot wind gust approximately 60 to 80 degrees off the left side. The aircraft rolled right, nose pitched down, and the right skid contacted the water. The aircraft came to rest in a pond in approximately 3 1/2 feet of water. Examination of the aircraft revealed that the tailboom had separated from the helicopter, the main rotor mast separated, the main rotor blades and the tail rotor were destroyed, the cockpit windshield was shattered, and the right fuel tank was missing (presumed sunk). According to the pilot, he had lifted off from a flat bed trailer and was hovering at a height of 6 feet. As the helicopter transitioned forward (approximately 20 knots indicated airspeed) and at a height estimated at 15 to 20 feet AGL, the helicopter encountered a 30 knot wind gust approximately 60 to 80 degrees off the left side. The aircraft rolled right, the nose pitched down, and the right skid contacted the water. The aircraft came to rest in a pond in approximately 3-1/2 feet of water. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_FTW96LA005.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 or causal vocabulary (loss of control). 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 ↗