N129WT

Substantial
Minor

TAILWIND W10S/N: 001

Accident Details

Date
Saturday, August 3, 2024
NTSB Number
CEN24LA301
Location
West Livingston, TX
Event ID
20240805194846
Coordinates
30.686166, -95.018000
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A partial loss of engine power due to carburetor ice.

Aircraft Information

Registration
Make
TAILWIND
Serial Number
001
Engine Type
Reciprocating
Year Built
2014
Model / ICAO
W10
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
TAILWIND W10

Registered Owner (Current)

Name
HILL TOOL LLC
Address
PO BOX 7967
City
MISSOULA
State / Zip Code
MT 59807-7967
Country
United States

Analysis

On August 3, 2024, about 1000 central daylight time, an experimental, amateur-built Tailwind W10 airplane, N129WT, was substantially damaged when it was involved in an accident near West Livingston, Texas. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, he departed his local airport for a cross-country flight. About 30 minutes into the flight, he heard the engine “misfire,” but all engine instruments and temperatures appeared normal. The engine misfired again, and he decided to return to his departure airport. A few minutes later, the pilot experienced a significant loss of engine power, and elected to divert to a nearby airport. The pilot stated he did not have a lot of time to troubleshoot and executed a forced landing to the airport. During the landing roll, the airplane exited the runway surface, nosed over, and came to rest inverted. At some point while experiencing the engine issues, the pilot applied carburetor heat, which he felt exacerbated the problem, so he turned off the carburetor heat and continued the forced landing.

Postaccident examination of the airplane revealed substantial damage to the vertical stabilizer and rudder. Engine continuity was confirmed, and a compression check of the cylinders, and examination of the spark plugs and the ignition system all showed no anomalies. Fuel was observed in the fuel lines to the carburetor, and fuel flowed freely into the carburetor. Engine control continuity was confirmed. The examination revealed no evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation.

A review of the Carburetor Icing Probability Chart located in the Federal Aviation Administration’s Special Airworthiness Information Bulletin CE-09-35, Carburetor Icing Prevention, dated June 30, 2009, indicated that the atmospheric conditions in which the airplane was operating were conducive to the formation of serious icing at glide power settings.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN24LA301