Casualties unknown

1992-09-05: Weatherly 201B (N2935W) — Hendrickson Flying Service — Chana, IL

Chana, IL, US

On September 5, 1992, a Weatherly 201B (registration N2935W) operated by Hendrickson Flying Service was involved in an aviation accident near Chana, IL. Investigators recorded the probable cause as: The separation of the number 8 connecting rod across the I-beam section, which flailed against adjacent engine parts, resulting in total engine failure. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 3 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

An aircraft experienced engine power loss while returning from an aerial application mission, resulting in a forced landing in a pasture and significant structural damage due to internal engine failure.

What happened

The pilot was operating an aircraft during the return phase of an aerial application flight when the engine suddenly lost power. With no option to continue the flight normally, the pilot executed a forced landing in a nearby pasture characterized by rough terrain and uneven surfaces. The impact with the ground resulted in substantial structural damage to the airframe.

The investigation

Following the accident, mechanics performed a detailed disassembly of the engine to determine the root cause of the power loss. The inspection revealed a catastrophic internal failure within the engine block. Specifically, the connecting rod associated with cylinder number 8 had separated across its I-beam section. This broken component then flailed violently against adjacent parts inside the engine interior, causing widespread mechanical destruction that led to the immediate cessation of engine function.

Findings

The primary factor in this incident was the internal mechanical failure of the engine. The separation of the number 8 connecting rod prevented the engine from generating power, leaving the pilot with no choice but to land outside of a controlled environment. The rough surface of the pasture exacerbated the damage sustained during the landing.

Safety message

Regular and thorough inspection of engine components is critical for aerial application operations, which place high stress on airframes and powerplants. Early detection of internal wear or fatigue in connecting rods can prevent in-flight power loss and subsequent forced landings in unprepared areas.

Probable cause

The separation of the number 8 connecting rod across the I-beam section, which flailed against adjacent engine parts, resulting in total engine failure.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X15638. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.