5 fatalities

2004-12-02: Cessna 421B Golden Eagle II (N421SD) — Georgia-Cumberland Conference of Seventh-Day Adventists — Collegedale, United States of America

Collegedale, United States of AmericaTakeoff (climb)

On December 2, 2004, a Cessna 421B Golden Eagle II (registration N421SD) operated by Georgia-Cumberland Conference of Seventh-Day Adventists was involved in an aviation accident near Collegedale, United States of America during takeoff. 5 people were killed. Investigators recorded the probable cause as: The pilot's improper identification of a partial loss of engine power on initial takeoff climb resulting in a collision with trees and the ground. A factor was a partial failure of the left engine starter adapter due to overload. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199974Data APIEditorial standards

During takeoff climb, the pilot mishandled a partial power loss, failing to feather the right engine and misidentifying the problem. The left engine's starter adapter failed due to overload.

Accident Overview

An airline transport pilot (ATP) stated that the airplane was between 200 and 300 feet on initial takeoff climb when the right engine lost power, causing the airplane to yaw to the right. The pilot lowered the nose to gain airspeed and pulled the right power lever rearward, but nothing happened. The pilot did not feather the right propeller and began moving switches near the boost pump switches.

Passenger Observations

An ATP passenger reported that he did not think the left engine was producing full power. He scanned the manifold pressure gauges, noting one needle at zero and the other at 25 inches, while the expected manifold pressure should have been 39 inches. The passenger observed trees ahead and believed the pilot was attempting a forced landing in an open field to the left. He realized the airplane would collide with the trees. Just before impact, the pilot feathered the right engine; the passenger saw the right propeller go into feather position and come to a complete stop.

Examination Findings

Examination of the right engine revealed no anomalies. Examination of the left engine found that the starter adapter gear teeth had failed due to overload.

Probable Cause

The probable cause was the pilot's improper identification of a partial loss of engine power on initial takeoff climb, resulting in a collision with trees and the ground. A contributing factor was a partial failure of the left engine starter adapter due to overload.