No fatalities

Engine Failure During Aerial Application Takeoff Leads to Nose-Over (N14RY)

Dighton, KS, US

On June 1, 2006, a Grumman G-164B (registration N14RY) was involved in an aviation accident near Dighton, KS. No fatalities were reported. Investigators recorded the probable cause as: A fractured rocker arm boss on the number 1 cylinder that left the exhaust valve closed, resulting in a loss of engine power. 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 an aerial application takeoff, the engine lost power shortly after lift-off. The pilot landed toward the departure end, but the aircraft exited the runway into a wheat field, nosed over, and sustained damage. The pilot suffered minor injuries. Examination found a fractured rocker arm boss on the number 1 cylinder.

Accident Overview

An aerial application flight experienced an engine failure shortly after takeoff. The commercial pilot executed a landing on the remaining runway, aiming toward the departure end. However, the aircraft overran the runway and entered a wheat field. The main landing gear tires became embedded in soft, wet soil, causing the aircraft to nose over. This resulted in the engine fracturing and separating from the fuselage, and the vertical stabilizer and rudder were crushed downward. The pilot sustained minor injuries. Visual meteorological conditions prevailed at the time of the accident.

Engine Examination

Post-accident examination of the engine revealed a fracture in the rocker arm boss on the number 1 cylinder. This fracture prevented the exhaust valve from opening, leading to the loss of engine power. The failure of the rocker arm boss was the direct cause of the engine failure during the takeoff phase.

Probable cause

A fractured rocker arm boss on the number 1 cylinder that left the exhaust valve closed, resulting in a loss of engine power.

Frequently asked questions

What happened in the 1 Jun 2006 Grumman G-164B accident near Dighton, KS?

During an aerial application takeoff, the engine lost power shortly after lift-off. The pilot landed toward the departure end, but the aircraft exited the runway into a wheat field, nosed over, and sustained damage. The pilot suffered minor injuries. Examination found a fractured rocker arm boss on the number 1…

Were there any fatalities in the 1 Jun 2006 Grumman G-164B accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 1 Jun 2006 involved a Grumman G-164B, registration N14RY, at Dighton, KS.

What was the probable cause of the accident?

A fractured rocker arm boss on the number 1 cylinder that left the exhaust valve closed, resulting in a loss of engine power.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060705X00861. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.