Incident Overview

Date: Wednesday 5 September 2001
Aircraft Type: Lockheed C-130E Hercules
Owner/operator: United States Air Force – USAF
Registration Number: 68-10934
Location: 9 km NW of Laurinburg, NC – ÿ United States of America
Phase of Flight: En route
Status: Substantial, repaired
Casualties: Fatalities: 0 / Occupants:
Component Affected: The first stage turbine wheel.The first stage turbine wheel.
Category: Accident
A tactical airdrop mission involving the no. 4 engine experienced a fire during shutdown. The fire continued until the engine departed the aircraft, resulting in a landing at Fayetteville Regional Airport. Investigation revealed that the first stage turbine wheel disintegrated, with sections exiting through the turbine inlet case at specific points. Teardown of the turbine indicated significant loss of the first stage wheel and all attached blades.A tactical airdrop mission involving the no. 4 engine experienced a fire during shutdown. The fire continued until the engine departed the aircraft, resulting in a landing at Fayetteville Regional Airport. Investigation revealed that the first stage turbine wheel disintegrated, with sections exiting through the turbine inlet case at specific points. Teardown of the turbine indicated significant loss of the first stage wheel and all attached blades.

Description

During a tactical airdrop mission the no. 4 engine caught fire. The engine was shut down but the fire continued until the engine departed the aircraft. The Hercules landed safely at the Fayetteville Regional Airport. PROBABLE CAUSE: “The AIB President found that general maintenance and servicing was accomplished in compliance with technical data and was not a factor in this mishap; however there is clear and convincing evidence that the following item was causal: The first stage turbine wheel disintegrated. Sections of the turbine wheel web, rim and blades exited through the turbine inlet case at the 1 to 2 o’clock,4 and 7 to 8 o’clock positions (aft looking forward). Teardown of the turbine clearly indicates that the majority of he first stage wheel and all the attached blades were missing. All the turbine inlet case struts were cracked.”

Primary Cause

The disintegration of the first stage turbine wheel.The disintegration of the first stage turbine wheel.

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