N615RJ

Substantial
Serious

Vans RV 6S/N: 21603

Accident Details

Date
Wednesday, October 23, 2019
NTSB Number
WPR20LA014
Location
Spanaway, WA
Event ID
20191023X53135
Coordinates
47.070278, -122.371109
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
1
Uninjured
0
Total Aboard
2

Probable Cause and Findings

A total loss of engine power during the initial climb for reasons that could not be determined.

Aircraft Information

Registration
Make
VANS
Serial Number
21603
Engine Type
Reciprocating
Year Built
2006
Model / ICAO
RV 6
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
RV-6

Registered Owner (Current)

Name
THOMPSON JAMES R
Address
21023 44TH AVE E
City
SPANAWAY
State / Zip Code
WA 98387-6868
Country
United States

Analysis

On October 23, 2019, about 1200 Pacific daylight time, an experimental, amateur-built RV-6 airplane, N615RJ, was substantially damaged when it was involved in an accident near Spanaway, Washington. The pilot sustained minor injury and the passenger sustained serious injuries. The airplane was and operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that the initial taxi and engine run-up were normal; however, during the takeoff roll, the engine sputtered and the pilot aborted the takeoff. A subsequent engine run-up revealed no anomalies, and the pilot elected to take off again. As the airplane climbed through about 200 ft above ground level, the engine began to sputter and, shortly after, lost all power. The pilot performed a forced landing to an open field near the airport, resulting in substantial damage. The pilot reported 18 gallons of fuel onboard before departure.

The engine was examined following recovery from the accident site. The engine controls were continuous from the cockpit to the engine. The crankshaft was rotated by hand at the propeller and continuity was established through the valve train. Thumb compression was obtained on each cylinder. Both left and right magnetos produced spark at their terminal leads. The top spark plugs were removed and displayed normal operating signatures. Functional testing of the engine-driven fuel pump and throttle body injector revealed no anomalies. An unquantified amount of fuel remained in each of the wing fuel tanks and displayed no evidence of contamination. The amount of fuel onboard at the time of the accident was not determined.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR20LA014