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Atlas / NTSB / ATL95LA115

NTSB CAROL · Event

Event ATL95LA115

1995-06-20 LIVINGSTON, Alabama, United States Serious 1 aircraft Status: Completed

Registry · N101VB

FAA Aircraft Registry record.

Make / Model

CESSNA 182S

Year of manufacture

1999

TCDS

3A13 · TEXTRON AVIATION INC

Engine

LYCOMING IO-540 SER (300 hp)

Seats / Engines

4 seats · 1 engine

Last airworthiness date

20211027

ADS-B equipped

Yes — Mode-S A00A48

Registrant of record

ALPHA VESSLCO LLC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The loss of engine power for undetermined reasons.

Factual narrative

On June 20, 1995, at 1600 central daylight time, a Bell 47G3B1, N101VB, was substantially damaged following a collision with terrain during a forced landing near Livingston, Alabama. The commercial pilot received serious injuries in the accident. The aircraft was being operated under the provisions of CFR Part 91 by Morris Helicopters of Deatsville, Alabama. Visual meteorological conditions existed at the time, and no flight plan had been filed for the local agricultural flight. Witnesses in the area reported hearing the helicopter engine make a popping noise. The helicopter was observed descending and turning toward an open area just prior to impact with the terrain. The pilot stated that he was returning to the truck platform to reload with chemicals, when the aircraft engine lost power. He executed an autorotation into field, but was unable to see the ground due to the vegetation. He stated that the aircraft fell about 20 feet prior to impacting the terrain. Examination of the aircraft engine revealed that there was continuity of the engine drive train. The induction system was clear of obstructions, and the air filter was intact. The carburetor throttle valve, main nozzle and venturi were intact. There was fuel found in the carburetor bowl, and the fuel was free of contamination. The engine spark plugs appeared to have moderate wear, and the electrode gaps were the correct spacing. The magnetos, and ignition wiring were examined and found to be operational. THE PILOT STATED THAT WHILE RETURNING TO RELOAD THE AIRCRAFT WITH CHEMICALS, THE AIRCRAFT ENGINE LOST POWER. HE ATTEMPTED AN AUTOROTATION INTO A FIELD, BUT THE THICK VEGETATION PREVENTED HIM FROM OBSERVING THE GROUND, AND THE HELICOPTER FELL ABOUT 20 FEET PRIOR TO IMPACTING THE TERRAIN. EXAMINATION OF THE AIRCRAFT ENGINE DID NOT REVEAL ANY PROBLEMS WHICH WOULD HAVE PREVENTED THE ENGINE FROM OPERATING. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_ATL95LA115.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.