No fatalities

Landing Gear Collapse and Ditch Impact During Landing (N29SK)

Seneca, KS, US

On May 29, 2003, a Grumman G-164A (registration N29SK) was involved in an aviation accident near Seneca, KS. No fatalities were reported. Investigators recorded the probable cause as: The pilot's failure to maintain directional control while landing. Factors contributing to the accident were the collapse of the left main landing gear strut and the ditch. 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 2026-07-04Data APIEditorial standards

During landing, the airplane's left main landing gear collapsed, causing the left wing to strike the runway and the airplane to slide into a ditch. The aircraft sustained substantial damage. Post-accident inspection found no anomalies in the main landing gear brakes or brake assemblies.

Accident Sequence

The airplane experienced a collapse of the left main landing gear during landing, resulting in substantial damage. After touchdown, the aircraft turned abruptly to the right. The pilot applied left rudder in an attempt to regain control, causing the airplane to slide sideways down the runway.

Pilot Actions

Following the abrupt right turn, the pilot reported applying left rudder. The airplane then slid sideways, leading to the collapse of the left main landing gear strut. The left wing subsequently struck the runway, and the airplane continued sliding into a ditch.

Inspection Findings

An on-scene inspection of the airplane revealed no anomalies in the main landing gear brakes or brake assemblies. The right main landing gear strut was found intact.

Frequently asked questions

What happened in the 29 May 2003 Grumman G-164A accident near Seneca, KS?

During landing, the airplane's left main landing gear collapsed, causing the left wing to strike the runway and the airplane to slide into a ditch. The aircraft sustained substantial damage. Post-accident inspection found no anomalies in the main landing gear brakes or brake assemblies.

Were there any fatalities in the 29 May 2003 Grumman G-164A accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 29 May 2003 involved a Grumman G-164A, registration N29SK, at Seneca, KS.

What was the probable cause of the accident?

The pilot's failure to maintain directional control while landing. Factors contributing to the accident were the collapse of the left main landing gear strut and the ditch.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20030603X00767. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.