Casualties unknown

Uncontained Turbine Blade Failure Prompts Unscheduled Landing (N356PS)

Fresno, CA, US

On February 28, 1987, a British Aerospace BA146-200A (registration N356PS) operated by Pacific Southwest Airlines was involved in an aviation accident near Fresno, CA. Investigators recorded the probable cause as: Contaminated oil contributed to the failure of the number four turbine bearing, leading to overheating and damage to the overspeed sensors, which resulted in turbine overspeed and departure of the turbine blades. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 2 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
Aircraft registered N356PS
Aircraft registered N356PS. Photo: Aero Icarus from Zürich, Switzerland / CC BY-SA 2.0, via Wikimedia Commons

Approximately 40 minutes after takeoff, an aircraft experienced an uncontained failure of turbine blades on the number 4 power turbine wheel of the number 3 engine. Debris penetrated the pressure vessel, but the pilot performed an unscheduled landing without further incident.

Incident Summary

The flight was uneventful during takeoff and climb to an assigned cruise altitude of FL260. Approximately 40 minutes after takeoff, the number 3 engine suffered an uncontained failure of the turbine blades on the number 4 power turbine wheel. Debris from the engine penetrated the pressure vessel, forcing the pilot to make an unscheduled landing at an airport. No further complications were reported during the landing.

Engine Examination

Post-incident examination of the engine revealed that ferrous chips were present in the oil, indicating contamination. Additionally, oil was bypassing the engine oil filter, a condition that had persisted for at least 40 days. Despite this, no corrective actions were taken by company maintenance personnel. The oil and filter had been changed three times in the three months preceding the incident.

Contributing Factors

The examination concluded that the contaminated oil contributed to the failure of the number four turbine bearing. This failure subsequently led to overheating and damage to the overspeed sensors. Without proper overspeed protection, the turbine oversped, causing the turbine blades to depart the turbine disc.

Probable cause

Contaminated oil contributed to the failure of the number four turbine bearing, leading to overheating and damage to the overspeed sensors, which resulted in turbine overspeed and departure of the turbine blades.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001213X30257. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.