Casualties unknown

1990-04-13: Schweizer G-164B (N48455) — O'brien Flying Service — Reeves, LA

Reeves, LA, US

On April 13, 1990, a Schweizer G-164B (registration N48455) operated by O'brien Flying Service was involved in an aviation accident near Reeves, LA. Investigators recorded the probable cause as: The freezing of the number 3 cylinder exhaust rocker-arm bearing, which led to a lockup of the rocker-arm and subsequent separation of the rocker-box cover, resulting in an in-flight engine power loss. 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

An agricultural airplane experienced an in-flight power loss while conducting aerial seeding operations. The pilot executed a forced landing in a rice field, resulting in significant structural damage to the airframe and landing gear.

What happened

The incident occurred during an agricultural operation specifically identified as an aerial seeding flight. While performing this duty, the engine of the agricultural airplane experienced a sudden loss of power. Unable to maintain altitude or continue the mission, the pilot initiated a forced landing procedure.

The aircraft touched down in a rice field located near the operational area. Upon impact with the ground, the main landing gear assembly failed structurally and broke off from the airframe. The momentum of the aircraft caused it to flip forward, coming to rest in an inverted position on its roof. This sequence of events resulted in substantial physical damage to the lower fuselage and propulsion system.

The investigation

Post-accident examination of the wreckage revealed specific mechanical failures within the engine assembly. Investigators found that the bearing associated with the number 3 cylinder exhaust rocker-arm had frozen solid. This seizure locked the rocker-arm in place, preventing normal valve operation.

The excessive force generated by the locked component caused the rocker-box cover to rupture and break open. This internal engine failure is consistent with the reported loss of power during the flight phase.

Probable cause

The freezing of the number 3 cylinder exhaust rocker-arm bearing, which led to a lockup of the rocker-arm and subsequent separation of the rocker-box cover, resulting in an in-flight engine power loss.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001212X22916. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.