No fatalities

5 Feb 2023: BEECH F35 (N123JV) — Gladewater, TX

Gladewater, TX, United States

On 5 Feb 2023, a BEECH F35 (registration N123JV) was involved in an aviation accident near Gladewater, TX. No fatalities were reported. Investigators recorded the probable cause as: The loss of engine power for undetermined reasons. This summary draws on records from NTSB; 10 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On February 5, 2023, a Beech F-35 sustained substantial damage during a forced landing after the engine lost power during a go-around near Gladewater, Texas. The pilot and three passengers received minor injuries.

Accident Overview

On February 5, 2023, at approximately 1316 central standard time, a Beech F-35 airplane, registration N123JV, was substantially damaged in an accident near Gladewater, Texas. The pilot and three passengers sustained minor injuries. The flight was conducted as a personal flight under Title 14 Code of Federal Regulations Part 91.

Pilot Report

The pilot reported that during the return leg of a cross-country flight, while landing at the planned destination, he switched to the left fuel tank on downwind and observed a windsock indicating a strong westerly crosswind. He continued the traffic pattern, turning left base and then final approach. On final, the pilot encountered moderate turbulence. While attempting to land, the airplane floated about halfway down the runway, prompting the pilot to abort the landing and execute a go-around.

Engine Power Loss and Forced Landing

During the go-around, the engine abruptly lost power, and the airplane climbed only about 100 feet above ground level. The pilot maneuvered to avoid obstacles at the end of the runway, but then the engine lost total power. He initiated a forced landing. During the forced landing, the airplane’s right wing struck a tree, causing substantial damage. The airplane then impacted a pond and came to rest submerged in water, with only the empennage and top of the fuselage visible above the waterline.

Postaccident Examination

Postaccident examination of the airframe and engine revealed no evidence of preimpact failures or malfunctions that would have precluded normal operation. The airplane was equipped with a pressure-type carburetor. According to the Federal Aviation Administration Pilot’s Handbook of Aeronautical Knowledge, “the danger of fuel vaporization icing is practically eliminated” in this type of carburetor.

Contributing factors

Engine (reciprocating)