Casualties unknown

2004-02-29: Piper PA-15 (N4492H) — Big Lake, AK

Big Lake, AK, US

On February 29, 2004, a Piper PA-15 (registration N4492H) was involved in an aviation accident near Big Lake, AK. Investigators recorded the probable cause as: An in-flight loss of control for an undetermined reason, which resulted in a forced landing and in-flight collision with trees. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A private pilot experienced an uncommanded left turn while cruising at 800 feet AGL in a ski-equipped airplane. Despite corrective inputs, the airplane entered a descending spiral. The pilot executed an emergency landing in trees, resulting in extensive damage. No flight control malfunction was found during examination.

Accident Overview

A private certificated pilot was conducting a cruise flight at approximately 800 feet above ground level (AGL) in a ski-equipped airplane. The pilot reported that the airplane initiated an uncommanded left turn. He applied right aileron control to correct the bank, but the left bank continued to steepen. He also applied right rudder to prevent the airplane from becoming inverted. The airplane subsequently entered a left descending spiral. The pilot decided to land as soon as possible and selected an emergency landing area on a small frozen lake. However, he was unable to reach that spot and instead chose a stand of trees for the landing. During the landing, the airplane's wings, landing gear, and fuselage sustained extensive damage. The entire emergency event lasted approximately one minute.

Aircraft and Maintenance History

The airplane had been rebuilt about five months before the accident and had accumulated about two hours of operation since the rebuild. The skis were installed on the airplane just prior to the accident flight. After the accident, the airplane was disassembled and recovered from the site.

Post-Accident Examination

The fuselage and components were examined by personnel from the National Transportation Safety Board (NTSB) and the Federal Aviation Administration (FAA). No evidence of a flight control system malfunction was found. The ski retention cables and springs exhibited no anomalies.

Probable Cause

The investigation did not determine a probable cause for the uncommanded left turn, as no mechanical or system malfunctions were identified. The source does not state a cause, and therefore, no probable cause is assigned.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040303X00257. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.