Eddie A Smith KR-2 N85ES

Summary

On 16 October 1999 at about 17:32 local time, a Eddie A Smith KR-2 registered N85ES was involved in an accident near Bell Buckle, Tennessee, United States. 2 people were on board and 2 died. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

Date

16 October 1999 at 17:32

Classification

Accident

Location

Bell Buckle, Tennessee, United States

Nearest airport

Bomar Field-Shelbyville (SYI)

Coordinates

35.5891, -86.3506

Aircraft

Eddie A Smith KR-2

Registration

N85ES

Category

Airplane

Engines

1

Operator

Not recorded

Operating rule

Part 91: General Aviation

Purpose of flight

Personal

Phase of flight

Not recorded

Route

Murfreesboro → Unknown

Aircraft damage

Destroyed

Weather

VMC

Light

Day

NTSB number

MIA00LA008

2 people died.

The poor in-flight planning decision by the pilot-in-command for continuing the flight with inadequate fuel supply and the inadvertent stall by the pilot-in-command following total loss of engine power due to fuel exhaustion. Findings in the accident were the pilot's intentional operation of the airplane with a passenger without providing a restraint system to that person, and operation of the airplane in an over gross weight condition.

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

Read the full NTSB narrative

Five gallons of fuel were added before the flight departed; after departure the flight proceeded to an airport located approximately 19 nautical miles away where a touch-and-go landing was observed. While flying northbound, northeast of the airport, witnesses heard the engine 'spittering and sputtering.' The airplane was then observed to turn to the left, followed by hearing the engine quit. They then observed the airplane in a nose low attitude, spinning and lost sight due to obstructions. Examination of the accident site by FAA inspectors revealed that the airplane descended vertical with little forward movement. A slight odor of fuel was noted in the damaged fuel tank, but no fuel was found; and no evidence of hydraulic action of the fuel tank was noted. No evidence of flight control preimpact failure or malfunction was noted. A seatbelt was not available for the right seat occupant, and replacement of the retractable main landing gear with a fixed type gear was performed but new weight and balance sheet was not located and the work performed was not documented in the aircraft maintenance records. Weight calculations performed indicate that the airplane was approximately 3 pounds over maximum design gross weight at the time of the accident.

Quoted verbatim from the NTSB record.