Aviation Crash Map

Rans S5 COYOTE N284AH

7 July 2009 · Greeneville, Tennessee, United States · Minor injuries

Summary

On 7 July 2009 at about 16:30 local time, a Rans S5 COYOTE registered N284AH, operated by Devault David Hodges, was involved in an accident near Greeneville, Tennessee, United States. One person was on board and one had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 16:30
Classification
Accident
Location
Greeneville, Tennessee, United States
Coordinates
36.1928, -82.8150
Aircraft
Rans S5 COYOTE
Registration
N284AH
Category
Airplane
Engines
1
Operator
Devault David Hodges
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Morristown → Greeneville
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
ERA09LA383

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
1 0 0 1 0

Probable cause

The pilot's failure to maintain airspeed during a forced landing. Contributing to the accident was the loss of engine power due to fuel starvation resulting from the pilot's inadequate preflight inspection.

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

Read the full NTSB narrative

The pilot stated that he was descending through 2,500 feet mean sea level when the engine lost total power. He attempted an engine restart, but the engine started and lost power again. A forced landing was initiated towards an open field. The flaps were not extended and the airspeed was about 31 mph when the airplane stalled. The right wing dropped down, the nose pitched down, and airplane collided with the ground. Performance data for the airplane revealed it would stall at 31 mph in a clean configuration. Examination of the airframe, flight controls, the engine assembly, and accessories revealed no anomalies. The fuel selector valve, located behind the pilot seat, was found in the on position. The right main fuel tank shutoff valve was found in the on position. The left fuel tank shutoff valve was found in the off position. The left and right shutoff valves were marked correctly, manually operated, and functioned. The pilot stated both fuel valves were in the on position during his preflight inspection. First responders who responded to the accident site stated they only cut the battery cable. No other switches or buttons were disturbed.

Quoted verbatim from the NTSB record.

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