1 fatality

1988-07-14: Cessna 421C Golden Eagle III (N825DW) — Vadala Management Corporation — Taunton, United States of America

Taunton, United States of AmericaLanding (descent or approach)

On July 14, 1988, a Cessna 421C Golden Eagle III (registration N825DW) operated by Vadala Management Corporation was involved in an aviation accident near Taunton, United States of America during landing or approach. One person was killed. Investigators recorded the probable cause as: The accident resulted from a partial loss of engine power due to mechanical failure (fatigue of engine accessories, loose starter, oil seal loss, and oil leak), followed by a loss of control in flight due to the pilot's failure to feather the propeller,… This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781215060Data APIEditorial standards

During a landing approach, a twin-engine aircraft experienced a partial loss of power in its right engine due to starter fatigue. The pilot subsequently lost control while maneuvering, leading to a collision with terrain northeast of the runway.

Accident Overview

While en route, the pilot notified approach control that the right engine was emitting smoke and losing oil pressure. Vectors were provided for a visual approach, but low clouds and haze reduced visibility. Upon reaching the airport area, the pilot reported the runway in sight and entered a left downwind for runway 30.

Timeline of Events

Witnesses observed the aircraft on a left downwind but noted it overshot the first turn toward final approach. As the pilot maneuvered to land, the aircraft crashed approximately 2,500 feet northeast of the runway in a wooded area. Witnesses reported the aircraft was flying slowly in a steep right turn with the landing gear extended before it descended steeply and caught fire.

Examination Findings

Post-accident examination revealed that the starter on the right engine had loosened. Three starter bolts had fractured through the threaded area, exhibiting signs of fatigue cracking. Wear marks on the starter gear and engine gear ring indicated the starter motor had shifted approximately three-quarters of an inch rearward. Additionally, the torsional damper was found to have been loose on its shaft before the accident, and both propellers were operating at low pitch during initial impact.

Probable Cause

The official findings identified three occurrences. The first was a partial loss of engine power due to mechanical failure, specifically fatigue of engine accessories, a loose starter, partial loss of the oil seal, and an oil leak. The second occurrence was a loss of in-flight control attributed to the pilot's failure to feather the propeller, an improper planned approach, failure to maintain minimum control airspeed (Vmc), and failure to maintain aircraft control. The third occurrence was an in-flight collision with terrain during an uncontrolled descent.