Propeller blade separation leads to emergency landing

Casualties unknown • Philadelphia, PA, US

A propeller blade separated from an aircraft during cruise flight, causing electrical failure and forcing the pilot to perform a gear-up landing.

What happened

While cruising at 6,000 feet MSL, a propeller blade from the left propeller assembly separated from the aircraft. The departing blade penetrated the fuselage, which severed electrical lines and resulted in a total loss of electrical power.

At the time of the incident, the aircraft was flying in IMC. To seek better weather conditions, the pilot performed a 1el-degree turn. For approximately 40 minutes, the pilot operated the aircraft without electrical power or most flight instruments. After reaching an area of clear weather and successfully identifying his location, the pilot executed a gear up landing at the nearest airport. The pilot was not injured.

The investigation

A metallurgical examination of the separated blade was conducted to determine the cause of the failure. The analysis revealed that the separation was caused by fatigue cracking. These cracks originated from multiple sites located within corrosion pits found in the balancing hole.

Probable cause

The propeller blade separation was caused by fatigue cracking originating from corrosion pits in the balancing hole, which had gone undetected during the previous overhaul because required shot peening and painting procedures were not performed.

Frequently asked questions

What happened in the 1992-08-18 Mitsubishi MU-2-60 accident near Philadelphia, PA?

A propeller blade separated from an aircraft during cruise flight, causing electrical failure and forcing the pilot to perform a gear-up landing.

What aircraft was involved and where did it happen?

The accident on 1992-08-18 involved a Mitsubishi MU-2-60, registration N66LA, operated by Epps Air Service, at Philadelphia, PA.

What was the probable cause of the accident?

The propeller blade separation was caused by fatigue cracking originating from corrosion pits in the balancing hole, which had gone undetected during the previous overhaul because required shot peening and painting procedures were not performed.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X15511. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.

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