N878TD

Substantial
None

TONY DUBEANSKY RV10S/N: 40669

Accident Details

Date
Wednesday, June 16, 2021
NTSB Number
CEN21LA273
Location
Fort Worth, TX
Event ID
20210617103279
Coordinates
32.930230, -97.411447
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A partial loss of engine power due to a separated electronic ignition system connector. Contributing to the accident was the location of the ignition boxes, which provided limited access to the connectors for visual inspection.

Aircraft Information

Registration
N878TD
Make
TONY DUBEANSKY
Serial Number
40669
Year Built
2021
Model / ICAO
RV10

Registered Owner (Historical)

Name
SALE REPORTED
Address
8762 RIVERTON CT
Status
Deregistered
City
DAPHNE
State / Zip Code
AL 36526-8354
Country
United States

Analysis

On June 16, 2021, about 0730 central daylight time, an experimental, amateur-built RV-10 airplane, N878TD, was substantially damaged when it was involved in an accident near Fort Worth, Texas. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot departed Hicks Airfield (T67), Fort Worth, Texas, about 0700 and headed northwest before returning to T67. The pilot reported that, during the initial climb following a touch-and-go landing, the engine backfired and lost power about 200 ft above ground level (agl). As the airplane descended, it collided with a power line before impact with terrain and a tree. The pilot added that the engine continued to run before the impact but did not develop enough power to maintain altitude. The airplane sustained damage to the landing gear, engine, and substantial damage to the fuselage during the accident.

Examination of the airplane revealed that the engine was equipped with an electronic ignition system, (labeled as #1 and #2) and automotive-style sparkplugs. The sparkplugs and valve covers were removed from each cylinder and the engine rotated by hand. Continuity through the valve train to the accessory section was noted. The bottom set of sparkplugs appeared wet and black in color. (See Figure 1.)

Figure 1: Bottom set of sparkplugs

The ignition system was field tested by passing a magnet over the flywheel ignition sensor; spark was only observed on one bank of the ignition system. The ignition leads and coil labels did not necessarily correspond to the associated cylinder. The ignition firing order was not confirmed.

The ignition control boxes were located behind the firewall, and the fuselage was cut open to allow access to the boxes. The output cable on ignition box #1 was found disconnected. (see Figure 2.)

Figure 2: Output cable as found on ignition box #1

The pin connectors were fully secured. Additionally, as mounted, access to the boxes were limited and could only be done from under the instrument panel and by reaching above the rudder pedals.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN21LA273