Casualties unknown

1982-04-11: Bell 47G-4 (N87623) — North American Corp — ST Genevieve, MO

ST Genevieve, MO, US

On April 11, 1982, a Bell 47G-4 (registration N87623) operated by North American Corp was involved in an aviation accident near ST Genevieve, MO. Investigators recorded the probable cause as: The No. 5 connecting rod had failed at the crankshaft end due to a broken rod cap bolt, causing the cap to straighten out and the rod to separate from the crankshaft. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

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

About 40 minutes after takeoff, a helicopter experienced a drop in oil pressure followed by engine failure. The pilot attempted an emergency landing in a small clearing but struck trees short of the opening. Investigation found the No. 5 connecting rod had failed at the crankshaft end due to a broken rod cap bolt.

Incident Overview

According to the official accident investigation, the pilot reported that approximately 40 minutes after takeoff, there was a drop in oil pressure. Almost immediately afterward, the helicopter's engine failed while the aircraft was over a wooded area. The pilot attempted an emergency landing in a small clearing, but the helicopter struck trees before reaching the opening.

Engine Examination

An investigation of the engine revealed that the No. 5 connecting rod had failed at the crankshaft end. Specifically, a rod cap bolt had broken, causing the cap to straighten out and the rod to separate from the crankshaft. A large hole was found in the crankcase, and the oil tank was empty. However, oil was noted inside the engine and on all bearings and journals except the No. 5 connecting rod. Additionally, all main bearings and all rod bearings and journals, except those for the No. 5 connecting rod, appeared normal.

Investigation Findings

No further details regarding the helicopter's registration, type, operator, or occupants were provided in the source. The investigation did not specify the extent of damage to the helicopter, injuries, or the time of day. No mention was made of weather conditions or air traffic control involvement.

Probable cause

The No. 5 connecting rod had failed at the crankshaft end due to a broken rod cap bolt, causing the cap to straighten out and the rod to separate from the crankshaft.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20020917X02472. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.