Casualties unknown

2004-07-24: Beech 58P (N69CL) — Fort Collins, CO

Fort Collins, CO, US

On July 24, 2004, a Beech 58P (registration N69CL) was involved in an aviation accident near Fort Collins, CO. Investigators recorded the probable cause as: the loss of engine power for undetermined reasons, and the pilot's failure to maintain adequate airspeed which resulted in a stall/spin. Clouds and the pilot's diverted attention were contributing factors. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

A pilot reported a malfunction shortly after takeoff, followed by an engine sputtering and power loss. The aircraft entered a flat spin and crashed into a residential street and driveway. Investigation found fuel selector valve discrepancies and no engine anomalies.

Background

Prior to departure, the pilot obtained a standard weather briefing and filed an instrument flight rules (IFR) flight plan. The pilot then took off.

Flight and Malfunction

Approximately four minutes after takeoff, after several routine radio communications, the air traffic controller issued a radar vector to the pilot. The pilot did not acknowledge. The controller repeated the vector. A squelch break occurred, and in the background, a noise and tone could be heard. The pilot then reported, "We have got some sort of malfunction going on here."

Accident Sequence

Witnesses reported hearing an engine sputtering and losing power. The airplane emerged from a low overcast in a flat counterclockwise spin. The airplane impacted a street and driveway in a residential subdivision.

Post-Accident Investigation

On-scene investigation disclosed that the landing gear and flaps were retracted. Both elevators were deflected up and jammed by impact. Examination of the airplane revealed the cockpit fuel selector handles were in the LEFT TANK-LEFT ENGINE/RIGHT TANK-RIGHT ENGINE positions. The left and right fuel selector valves, located in the wheel wells, were in the OFF and ON positions, respectively.

Analysis of the ATC communications tape revealed two engines operating until the pilot reported the malfunction, after which only one engine sound could be heard. A steady 1,000-hertz tone, similar to an aural stall warning system, was also heard.

Both engines, turbochargers, and propellers were later disassembled and examined. No anomalies were noted. Neither propeller was feathered.

Pilot Information

The day before the accident, the pilot had undergone recurrent ground and flight training, a flight review, and an instrument proficiency check in the airplane. Flight time totaled 5.3 hours.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20040730X01111. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.