Casualties unknown

Engine Loss During Touch and Go Results in Forced Landing and Nose-Over (N5196W)

Cartersville, GA, US

On March 5, 2006, a Joel H Johnson RANS S-6ES COYOTE II (registration N5196W) was involved in an aviation accident near Cartersville, GA. Investigators recorded the probable cause as: The loss of engine power during cruise flight for undetermined reasons, which resulted in an forced landing, on ground collision with a ditch, and nose over. 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 2026-06-10Data APIEditorial standards

During pattern work, a CFI and student pilot experienced engine sputtering after a touch and go. The engine lost power, leading to a forced landing in a field, where the aircraft hit a ditch and nosed over. Post-accident inspection found no anomalies.

Accident Overview

A certified flight instructor (CFI) and a student pilot were conducting takeoff training, pattern work, and approach-to-landing instruction at an airport. During a touch-and-go landing, the engine began to sputter and lose power. The aircraft was at an altitude of 300 to 400 feet above ground level and approximately two-thirds down Runway 01 when the power loss occurred.

Actions Taken

The CFI assumed control of the airplane and leveled it, hoping the engine would regain power. However, the engine subsequently stopped, forcing the CFI to execute a forced landing in a field adjacent to the airport. On landing, the aircraft collided with a ditch and nosed over.

Post-Accident Examination

The registered owner of the aircraft conducted an examination of the engine assembly after removal from the airframe. The top spark plugs were removed and found to have normal electrodes with the proper gap, as per the Rotax Maintenance Manual. The oil and fuel lines were intact and not breached. A visual fuel sample showed no contaminants, and the fuel system remained full and intact. The in-line fuel filters were free of contaminants. The carburetors were inspected and no contaminants were observed. The electrical system, including coils and lighting coils, functioned normally with no anomalies. The gearbox, checked by manual rotation of the engine, was functional. Rotary valves operated correctly, and compression appeared normal when the engine was turned by hand. The engine head was removed, revealing no damage to the pistons, sleeves, or rings.

Investigation Outcome

Despite the thorough examination, no determination was made regarding the cause of the loss of engine power.

Safety Information

No specific safety recommendations or conclusions were provided in the source material.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20060323X00334. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.