4 fatalities

2006-01-30: Cessna 421B Golden Eagle II (N920MC) — H K Golden Eagle Inc. — Chicago-Executive (Palwaukee), United States of America

Chicago-Executive (Palwaukee), United States of AmericaLanding (descent or approach)

On January 30, 2006, a Cessna 421B Golden Eagle II (registration N920MC) operated by H K Golden Eagle Inc. was involved in an aviation accident near Chicago-Executive (Palwaukee), United States of America during landing or approach. 4 people were killed. Investigators recorded the probable cause as: The pilot's failure to maintain airspeed during the landing approach which led to an inadvertent stall and subsequent uncontrolled descent and impact with the ground. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A).

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199088Data APIEditorial standards

An airplane was destroyed and its occupants fatally injured when it stalled during approach to landing in visual meteorological conditions. The pilot failed to maintain airspeed, leading to an inadvertent stall and uncontrolled descent.

Accident Overview

The accident occurred during approach to landing when the airplane impacted the ground and was destroyed. The occupants sustained fatal injuries. Examination of the airplane, its engines, and propellers revealed no anomalies that were determined to have existed prior to impact. The propellers were found to have been in their normal operating range, and neither propeller was in a feathered position. The quill shafts of both engines showed evidence of damage due to the production of torque. A sound spectrum examination of audio transmissions showed signatures that both engines were operating during the last two radio transmissions from the airplane.

Flight Path and Conditions

Based on radar data, communications, and meteorological information, the airplane was operating in visual meteorological conditions below an overcast layer of clouds. Radar data showed the airplane as it approached the airport and as it entered a left-hand traffic pattern for runway 34. Radio communications confirmed that the airplane had been cleared for a left-hand traffic pattern to runway 34. The radar data showed the airplane as it made a turn to the left while its speed decreased to about 82 knots calibrated airspeed as of the last received radar return. This radar return was about 0.1 nautical miles from the accident site and 0.8 nautical miles at 216 degrees from the approach end of runway 34.

Performance and Configuration

The airplane owner's manual listed stall speeds ranging from 81 to 94 knots calibrated airspeed for airplane configurations including gear and flaps up to gear down and flaps 15 degrees, and bank angles from 0 to 40 degrees. Flap position could not be determined because the flap chain had separated from the flap drive motor. The owner's manual also listed an approach speed of 103 knots.

Probable Cause

The probable cause of the accident was the pilot's failure to maintain airspeed during the landing approach, which led to an inadvertent stall and subsequent uncontrolled descent and impact with the ground.