No fatalities

23 Oct 2019: Vans RV 6 (N615RJ) — Spanaway, WA

Spanaway, WA, United States

On 23 Oct 2019, a Vans RV 6 Undesignat (registration N615RJ) was involved in an aviation accident near Spanaway, WA. No fatalities were reported. Investigators recorded the probable cause as: A total loss of engine power during the initial climb for reasons that could not be determined. This summary draws on records from NTSB; 12 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On October 23, 2019, an experimental RV-6 (N615RJ) experienced engine power loss during climb, forcing a landing in a field near Spanaway, Washington. The pilot and passenger sustained injuries; the aircraft was substantially damaged.

Accident Overview

On October 23, 2019, at approximately 1200 Pacific daylight time, an experimental, amateur-built RV-6 airplane, registration N615RJ, was substantially damaged during a forced landing near Spanaway, Washington. The pilot sustained minor injuries, while the passenger sustained serious injuries. The flight was conducted under Title 14 Code of Federal Regulations Part 91 as a personal flight.

Sequence of Events

According to the pilot's report, the initial taxi and engine run-up were normal. However, during the takeoff roll, the engine sputtered, prompting the pilot to abort the takeoff. A subsequent engine run-up revealed no anomalies, and the pilot decided to attempt another takeoff. As the airplane climbed through about 200 feet above ground level, the engine began to sputter again and shortly thereafter lost all power. The pilot executed a forced landing to an open field near the airport, resulting in substantial damage to the aircraft. The pilot stated that there were 18 gallons of fuel onboard before departure.

Post-Accident Examination

Following recovery from the accident site, the engine was examined. The engine controls were continuous from the cockpit to the engine. Hand rotation of the crankshaft at the propeller established continuity through the valve train, and 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 showed no evidence of contamination. The exact amount of fuel onboard at the time of the accident was not determined.

Contributing factors

Engine (reciprocating)