N123JV

Substantial
Minor

BEECH F35S/N: D-4024

Accident Details

Date
Sunday, February 5, 2023
NTSB Number
WPR23LA104
Location
Gladewater, TX
Event ID
20230207106692
Coordinates
32.528833, -94.971750
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
4
Uninjured
0
Total Aboard
4

Probable Cause and Findings

The loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
BEECH
Serial Number
D-4024
Engine Type
Reciprocating
Year Built
1955
Model / ICAO
F35BE35
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
F35

Registered Owner (Current)

Name
DOWNING DANNY L
Address
815 NORRIS RD
City
KILGORE
State / Zip Code
TX 75662-1819
Country
United States

Analysis

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

The pilot reported that on the return leg of a cross-country flight, while landing at the planned destination, he switched to the left fuel tank on downwind and noticed that the windsock indicated a strong westerly crosswind. He continued in the traffic pattern and turned left base and then final. While on final approach, the pilot stated that he experienced moderate turbulence and, while attempting to land, the airplane floated about halfway down the runway, so he aborted the landing and executed a go-around.

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

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.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR23LA104