4 fatalities

1999-05-27: Cessna 421B Golden Eagle II (N34TM) — Robert E. Linville — Jefferson City, United States of America

Jefferson City, United States of AmericaLanding (descent or approach)

On May 27, 1999, a Cessna 421B Golden Eagle II (registration N34TM) operated by Robert E. Linville was involved in an aviation accident near Jefferson City, United States of America during landing or approach. 4 people were killed. Investigators recorded the probable cause as: The pilot failed to maintain control of the airplane. A factor was the partial loss of power due to the exhaust valve fatigue failure. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781204351Data APIEditorial standards

The airplane impacted terrain in a nose-low inverted attitude after the pilot reported a loss of power on the right engine. The probable cause was the pilot's failure to maintain control, with a factor being partial power loss from exhaust valve fatigue failure.

Accident Details

The airplane impacted the ground in a nose-low, inverted attitude. The pilot reported over the radio, 'Jeff Tower, N34TM, I've just lost power on the right engine, eh, left engine.' At the time, the airplane's altitude was approximately 200 to 400 feet when its wings wobbled back and forth. Subsequently, the wings banked approximately 90 degrees to the left, and the airplane nosed over before impacting the ground. White smoke was observed emanating from the belly of the airplane for 1 to 2 seconds, approximately 20 seconds prior to impact.

Terrain and Wreckage

The terrain consisted of a flat, hard-packed field used for growing grass sod. Both the left and right propellers were found embedded 12 to 18 inches under the hard-packed soil. Rotational paint transfer patterns from the propeller blades onto the soil were evident, and the propeller blades exhibited chordwise scratching and leading edge polishing.

Engine Examination

Examination of the left engine revealed that the #2 cylinder piston was broken, with the piston pin still attached to the piston rod. The NTSB Materials Laboratory examination determined that the fracture face of the #2 exhaust valve stem was consistent with a bending fatigue separation. Additionally, both the #2 and #6 exhaust valve guides showed heavy wear, resulting in ovalized bores.

Maintenance History

The most recent annual inspection, conducted on March 15, 1999, recorded the following compression readings for the left engine: 80/64, 50, 67, 70, 69, and 62.

Probable Cause

The official probable cause was the pilot's failure to maintain control of the airplane, with a contributing factor being the partial loss of power due to the exhaust valve fatigue failure.