Casualties unknown

1999-05-23: Piper PA-28RT-201T (N8252S) — Wings OF Denver Flying Club — Great Bend, KS

Great Bend, KS, US

On May 23, 1999, a Piper PA-28RT-201T (registration N8252S) operated by Wings OF Denver Flying Club was involved in an aviation accident near Great Bend, KS. Investigators recorded the probable cause as: the chafed through turbocharger oil supply hose, the failure of maintenance personnel to install a clamp on the turbocharger oil supply hose, and the inability of the pilot to maintain aircraft control. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 4 related events involving the same aircraft type or operator are linked below.

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

A pilot reported smoke in the cockpit during cruise flight before radar and radio contact were lost. The aircraft impacted an alfalfa field near Great Bend Municipal Airport. Examination revealed a chafed turbocharger oil supply hose and engine bearing distress.

Accident Overview

During cruise flight, the pilot reported smoke in the cockpit to air traffic control. Subsequently, radar and radio contact were lost. The aircraft impacted the terrain in a level open alfalfa field located 9.2 statute miles and 108 degrees magnetic from the Great Bend Municipal Airport.

Witness Observations

A witness who was driving reported seeing the aircraft "diving at an angle..." and thought he "...saw smoke coming from the plane..." prior to impact.

Aircraft Examination

Examination of the control system and airframe structure revealed no anomalies that could be associated with a preexisting condition. The aft fuselage side and bottom exhibited oil streaks in the longitudinal direction.

Engine and Turbocharger Findings

Engine examination showed the connecting rod bearing surfaces exhibited evidence of distress and discoloration of the bearing material. The turbocharger had charred black deposits on its exterior surfaces. The turbocharger oil supply hose was chafed through in the area adjacent to the propeller governor control cable. No clamps were found on the turbocharger oil supply hose, and it did not have a fire sleeve jacket. In contrast, the oil supply and return lines to the oil cooler and the fuel supply hoses did have fire sleeve jackets.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X18708. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.