1 fatality

1998-11-20: Cessna 414 Chancellor (N6820J) — Gemco — Mattapoisett, United States of America

Mattapoisett, United States of AmericaFlight

On November 20, 1998, a Cessna 414 Chancellor (registration N6820J) operated by Gemco was involved in an aviation accident near Mattapoisett, United States of America in flight. One person was killed. Investigators recorded the probable cause as: The pilot's failure to maintain control of the airplane after an undetermined failure of the airplane's attitude indicator. A factor in this accident was fog. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781204747Data APIEditorial standards

An aircraft in instrument meteorological conditions at 2,000 feet lost its attitude indicator; the pilot reported the loss before radar and communications were lost. The aircraft was found scattered in shallow water; investigation revealed a vertical speed indication and no vacuum pump malfunctions.

Accident Sequence

The aircraft was in level flight at 2,000 feet in instrument meteorological conditions when the pilot transmitted, "we've just lost our ahh artificial horizon." Approximately five minutes later, air traffic control lost radar contact and communications with the aircraft. A witness located about one mile north of the accident site reported hearing engine noise emanating from the water, describing the sound as loud and constant. The noise persisted for about 30 seconds and was followed by an "explosive collision/impact sound." The witness walked to the shore to locate the source but could not see anything due to fog.

Wreckage and Examination

The aircraft was found submerged in approximately 25 feet of water, with wreckage scattered over a 150- to 200-foot area. Recovered components included both engines, parts of the left wing, empennage, fuselage, seats, and interior. The attitude indicator was not recovered. A faint needle impression on the vertical speed indicator face indicated a descent rate between minus 2,500 and 3,000 feet per minute. Examination of the left and right vacuum pumps revealed no malfunctions or failures.

Probable Cause

The official probable cause was the pilot's failure to maintain control of the airplane after an undetermined failure of the airplane's attitude indicator. A contributing factor was fog.