Aviation Crash Map

Klasing BRADLEY BA100 N53SK

29 May 2005 · Xenia, Ohio, United States · Fatal

Summary

On 29 May 2005 at about 13:02 local time, a Klasing BRADLEY BA100 registered N53SK was involved in an accident near Xenia, Ohio, United States. One person was on board and one died. 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 13:02
Classification
Accident
Location
Xenia, Ohio, United States
Nearest airport
Greene County Airport (I19)
Coordinates
39.6969, -83.9758
Aircraft
Klasing BRADLEY BA100
Registration
N53SK
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Dayton → Unknown
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
NYC05LA088

People

1 person died.

On board Died Serious Minor Uninjured
1 1 0 0 0

Probable cause

A loss of engine power for undetermined reasons, and the pilot's failure to maintain aircraft control, which resulted in an inadvertent stall and uncontrolled descent into terrain.

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

Read the full NTSB narrative

The amateur built airplane was equipped with a Revmaster 2100D, 75-horsepower engine; which was a conversion of a Volkswagen engine. The pilot had completed the first flight in the airplane several weeks prior to the accident. During that flight, the pilot had difficulty controlling the airplane. The pilot subsequently made modifications to the airplane in an effort to increase the controllability. The accident flight was the pilot's second flight in the airplane. After approximately 15 minutes of flight, the airplane appeared to be entering a base leg for runway 25 at the pilot's home airport. Witnesses heard the engine sputter, followed by a lack of engine noise. The airplane then slowed, descended in a nose down attitude, and impacted a quarry. Examination of the wreckage did not reveal any pre-impact mechanical malfunctions. The engine was not equipped with magnetos as it had a battery-powered ignition system. The battery-powered ignition system was not tested due to impact damage. In addition, according to an FAA Carburetor Icing Probability Chart, moderate icing at cruise power or serious icing at glide power range was predicted for the prevailing temperature and dew point.

Quoted verbatim from the NTSB record.

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