Beechcraft C24R N2074P

Summary

On 20 December 2015 at about 19:30 local time, a Beechcraft C24R registered N2074P was involved in an accident near Winder, Georgia, United States. One person was on board and one died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

20 December 2015 at 19:30

Classification

Accident

Location

Winder, Georgia, United States

Coordinates

33.9350, -83.6025

Aircraft

Beechcraft C24R

Registration

N2074P

Category

Airplane

Year built

1978

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Jefferson → Winder

Aircraft damage

Destroyed

Weather

VMC

Light

Day

NTSB number

ERA16FA075

1 person died.

A total loss of engine power for reasons that could not be determined because the examination of the wreckage did not reveal any mechanical anomalies that would have precluded normal operation.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The private pilot was conducting a personal cross-country flight. The pilot last fueled the airplane 10 days before the accident. Review of GPS data and fueling records revealed that between the last fueling and the accident, the airplane had been operated for nearly 4 hours. Several witnesses observed the airplane flying overhead as it neared the destination airport and then saw it impact treetops near a golf course. One of the witnesses stated that the left wing was low and that the airplane was losing altitude "very quickly" before it impacted terrain. Another witness reported hearing the engine "sputtering" before impact. The witness drove to the accident scene and saw fuel leaking from the airplane. Examination of the airframe and engine revealed no evidence of any preimpact mechanical malfunctions or abnormalities that would have precluded normal operation; however, the examination noted alack of rotational signatures on the propeller. The right fuel tank was found intact and empty. The witness's description of the engine sputtering as well as  the lack of rotational signatures on the propeller suggest that the engine had likely lost power before the impact. Although the fuel selector was found in the left fuel tank position, it could not be determined what position the selector valve was in before the loss of engine power. It is possible that the pilot exhausted the fuel in the right fuel tank and was attempting to restart the engine from the left fuel tank when the accident occurred; however, based on the available evidence, the reason for the loss of engine power could not be determined.

Quoted verbatim from the NTSB record.