No fatalities

2 Jun 2018: PIPER PA 18-150 150 (N624MW) — Wasilla, AK

Wasilla, AK, United States

On 2 Jun 2018, a PIPER PA 18-150 150 (registration N624MW) was involved in an aviation accident near Wasilla, AK. No fatalities were reported. Investigators recorded the probable cause as: A total loss of engine power for reasons that could not be determined based on the available information. 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

A Piper PA-18-150 suffered a total loss of engine power shortly after departure, resulting in a forced landing in trees near Wasilla, Alaska. The private pilot was seriously injured.

Accident Overview

On June 2, 2018, about 1025 Alaska daylight time, a Piper PA-18-150, registration N624MW, sustained substantial damage during a forced landing after a total loss of engine power. The accident occurred near Lawrence Airstrip (55AK) in Wasilla, Alaska. The airplane was operated by the private pilot under 14 Code of Federal Regulations Part 91 as a visual flight rules flight. Visual meteorological conditions prevailed, and no flight plan was filed. The flight had departed 55AK about 1023, destined for Big Lake, Alaska.

Pilot Report

According to the pilot, all engine power was lost shortly after departure. The pilot reported no sights or sounds consistent with a catastrophic engine failure; the engine ceased operation consistent with fuel starvation. The pilot stated that the left fuel tank was about half full, the right fuel tank was empty, and the fuel selector was positioned to "BOTH."

Forced Landing and Impact

During the forced landing, the pilot attempted to return to the runway but impacted a forested area of tall spruce and birch trees. The impact resulted in substantial damage to the wings and rudder.

Engine Examination

On July 11, 2018, the engine, a Lycoming O-320-A2B, was examined at Alaska Claims Services under the supervision of National Transportation Safety Board investigators. Prior to removal, the gascolator was drained and small amounts of unidentified contaminants were found. The carburetor bowl was also drained, revealing more minute contaminants.

Engine Test Run

The engine was removed from the airframe and transported to Alaska Aircraft Engines in Anchorage, Alaska. On July 17, it was attached to an engine test truck with a four-bladed wooden club propeller. The engine started within three seconds and was warmed at idle power for five minutes. It was then run at idle and maximum power for five minutes each, followed by rapid manipulations from idle to maximum continuous power. No hesitations or anomalies were observed throughout the test run.

Contributing factors

Contributed to outcome