N42CS

Substantial
Serious

VANS RV8S/N: 80546

Accident Details

Date
Tuesday, December 10, 2024
NTSB Number
CEN25LA058
Location
Smithville, TX
Event ID
20241211199413
Coordinates
30.028208, -97.167039
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

A loss of engine power for undetermined reasons.

Aircraft Information

Registration
N42CS
Make
VANS
Serial Number
80546
Engine Type
Reciprocating
Year Built
2003
Model / ICAO
RV8RV8
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
DAVIS ROBERT W
Address
111 OAK HOLLOW LN
Status
Deregistered
City
BUDA
State / Zip Code
TX 78610-3158
Country
United States

Analysis

On December 10, 2024, about 1130 central standard time, a Vans RV-8, N42CS, was substantially damaged when it was involved in an accident near Smithville, Texas. The pilot was seriously injured. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot reported that the accident flight was the second flight of the day. He had flown from San Marcos Airport (KHYI), San Marcos, Texas, to Smithville Crawford Municipal Airport (84R), Smithville, Texas, earlier that morning. He had both fuel tanks topped off before departing 84R. After takeoff, the engine began to cut out and lose engine power. When the airplane reached about 100 to 150 ft agl, the engine lost total power. The airplane was in a left bank, so the pilot rolled the wings level, but the airplane entered an aerodynamic stall before it descended and impacted terrain about 1,000 ft north of the departure end of the runway.

The airplane was recovered to a salvage facility for further examination. On March 7, 2025, an engine run was conducted, and the engine started and ran without any problems noted. The engine was able to produce rated power. The engine continued to run with the ignition switch in the “off” position. The switch connection’s ground intermittently and appeared to be in a condition which would have allowed continued operation of the magnetos. Disassembly of the switch did not find any anomalies.

The loss of engine power could not be replicated.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN25LA058