5 fatalities

2005-01-21: Cessna 421C Golden Eagle III (N844JK) — Riley Rocket — Olathe, United States of America

Olathe, United States of AmericaTakeoff (climb)

On January 21, 2005, a Cessna 421C Golden Eagle III (registration N844JK) operated by Riley Rocket was involved in an aviation accident near Olathe, United States of America during takeoff. 5 people were killed. Investigators recorded the probable cause as: The pilot's failure to maintain adequate altitude/clearance during cruise flight, resulting in collision with trees. Contributing factors were the low altitude and low ceiling. This summary draws on records from the Bureau of Aircraft Accidents Archives (B3A); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Bureau of Aircraft Accidents Archives (B3A)Primary reportUpdated 1781199860Data APIEditorial standards

A personal flight operating under IFR with an uncertified GPS exceeded maximum gross weight and struck trees, terrain, and a residence in instrument conditions, causing substantial damage.

Accident Overview

According to official records, a personal flight departing from an airport at an elevation of 1,096 feet mean sea level sustained substantial damage after impacting trees, terrain, and a residence approximately one mile from the departure airport. The accident occurred during instrument meteorological conditions.

Flight Details

The flight was operating under an instrument flight rules (IFR) flight plan. The flight plan included an equipment suffix indicating the aircraft was equipped with a Global Positioning System (GPS). However, aircraft records show that while a GPS was installed, it was not approved for IFR navigation.

Departure and Radar Data

The pilot received a departure clearance to 3,000 feet with a heading of 130 degrees. Radar data indicates that the airplane leveled off at approximately 2,000 feet for a 32-second period while executing a right turn toward the assigned heading.

Impact and Wreckage

Witnesses reported that the airplane impacted terrain in a right-wing, nose-low attitude. The wreckage distribution and ground scarring were consistent with a high-speed impact. No anomalies were found that would have precluded normal operation of the airplane.

Weight and Loading

Calculations showed that the airplane's weight at the time of the accident was approximately 597 pounds above its maximum gross weight.

Probable Cause

The probable cause of the accident was the pilot's failure to maintain adequate altitude/clearance during cruise flight, resulting in a collision with trees. Contributing factors were the low altitude and low ceiling.