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Atlas / NTSB / NYC95LA161

NTSB CAROL · Event

Event NYC95LA161

1995-07-13 WARREN, Vermont, United States Airport · 0B7 Minor 1 aircraft Status: Completed

Registry · N5204G

FAA Aircraft Registry record.

Make / Model

EUROCOPTER AS 350 B2

Year of manufacture

1998

TCDS

H9EU · AIRBUS HELICOPTERS

Engine

TURBOMECA ARRIEL 1SER (681 hp)

Seats / Engines

6 seats · 1 engine

Last airworthiness date

19980811

ADS-B equipped

Yes — Mode-S A68BD9

Registrant of record

U S DEPT OF HOMELAND SECURITY

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

a failed elevator cable which resulted in an inflight loss of control and uncontrolled contact with trees.

Factual narrative

On July 13, 1995, at 1530 eastern daylight time, a Cessna 305A, N5204G, struck trees while on approach to land at Warren Sugarbush Airport, Warren, Vermont. The Airline Transport rated pilot, received minor injuries, and the airplane was destroyed. Visual meteorological conditions prevailed, and no flight plan had been filed for the local glider towing flight which was conducted under 14 CFR Part 91, and had departed at 1520. The airplane had been used for several flight during the day, towing gliders aloft. In the NTSB Accident Report, the pilot stated: The tow was normal and the glider released at 3,800 FT AGL. Returned to the airport, entered the traffic pattern for a landing on rw 22, the elevator control cable seized and I was unable to control the descent of the aircraft. The A/C impacted in the trees about 1/2 mile NNE of the airport. Time was about 3:30 EDT. An FAA Inspector examined the wreckage and in a report stated: The up elevator cable appeared to have broken prior to the crash and showed signs of wear. (station: 110) The elevator cable pulley may also have been binding. (station: 110) The rest of the aircraft and cables appeared to be in a well maintained condition.... After a discussion with the aircraft owner...about the inspections requirements and the difficulty of inspections in this area of the aircraft. [The owner]...contacted several other soaring associations and initiated a reinspection of all aircraft elevator cables in this area. Several aircraft were found to have evidence of elevator cable wear and corrective action has been initiated. In a telephone interview, the FAA reported that they were unable to determine if the inspection on the airplane had been inadequate due to the length of time (75 hours) between the previous inspection and the accident. THE PILOT WAS RETURNING THE AIRPLANE TO THE AIRPORT, AFTER TOWING A GLIDER. IN THE TRAFFIC PATTERN, THE ELEVATOR CONTROL SEIZED AND THE PILOT WAS UNABLE TO CONTROL THE DESCENT, AFTER WHICH THE AIRPLANE IMPACTED TREES. EXAMINATION REVEALED THE ELEVATOR CABLE HAD FAILED NEAR A PULLEY. THE AIRPLANE HAD LAST BEEN INSPECTED 75 HOURS PRIOR TO THE ACCIDENT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12

Verbatim from NTSB's published report. Source file NTSB_1995_NYC95LA161.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 ↗