Casualties unknown

1995-09-09: Bell 230 (N232UM) — Corporate Jets, Inc. — Ann Arbor, MI

Ann Arbor, MI, US

On September 9, 1995, a Bell 230 (registration N232UM) operated by Corporate Jets, Inc. was involved in an aviation accident near Ann Arbor, MI. Investigators recorded the probable cause as: A manufacturing defect involving a grinding process that removed material from the tail rotor blade skin, which initiated a fatigue crack and subsequent failure. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 5 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 helicopter experienced total loss of its tail rotor system during cruise flight but landed safely without injury. Investigation revealed a manufacturing defect in the blade skin caused a fatigue crack.

What happened

During cruise flight, the aircraft suffered a catastrophic failure involving the complete loss of the tail rotor system. Despite this significant mechanical failure, the pilot was able to land the helicopter successfully. The landing resulted in no additional damage to the airframe and no injuries were reported among those on board.

The investigation

A detailed examination of the failed components was conducted to determine the root cause of the incident. Investigators found that the failure originated from a fatigue crack located within the skin of one of the tail rotor blades. This structural defect allowed the blade to fail under operational loads, leading to the total loss of the system.

Findings

The manufacturer analyzed the manufacturing process used to produce the affected blades. They determined that a specific grinding process employed during production removed material from the tail rotor skin. This removal of material initiated the fatigue failure that ultimately led to the in-flight breakup of the tail rotor assembly.

Probable cause

A manufacturing defect involving a grinding process that removed material from the tail rotor blade skin, which initiated a fatigue crack and subsequent failure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001207X04439. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.