NTSB Issues Prelim On Valdosta KR-2 Accident
First Flight In Experimental Bird Kills Pilot
Despite a fair amount of recent experience in similar types of aircraft, the
first flight in a KR-2 homebuilt proved to be the last for one pilot. The
KR-2 (file photo) went down after declaring that he had a fire in the
cockpit, in what turned out to be the third flight for the aircraft and the
first in that specific aircraft, for the pilot. 
NTSB Identification: ERA09LA231
14 CFR Part 91: General Aviation
Accident occurred Saturday, April 04, 2009 in Valdosta, GA
Aircraft: Howard William C KR-2, registration: N456CH
Injuries: 1 Fatal.
This is preliminary information, subject to change, and may contain errors.
Any errors in this report will be corrected when the final report has been
completed.
On April 4, 2009, about 1847 eastern daylight time (EDT), an experimental
amateur-built Howard KR-2, N456CH, was destroyed by fire during an
off-airport landing. The certificated private pilot was killed. Visual
meteorological conditions prevailed, and no flight plan was filed for the
local personal flight which departed from Valdosta Regional Airport (VLD),
Valdosta, Georgia. The personal flight was conducted under the provisions of
14 Code of Federal Regulations Part 91.
The flight departed VLD approximately 1820 and was required to remain with
in 25 nautical miles of VLD until the airplane had flown at least a total of
40 hours of logged flight time. This limitation along with others had been
issued for the Phase 1 flight testing under the Experimental Operating
Limitations by the Federal Aviation Administration (FAA).
The pilot called the FAA Air Traffic Control Tower (ATCT) at VLD and
reported that he had smoke coming into the cockpit and was about 9 miles
from the airport. Subsequently the pilot reported a fire in the cockpit and
the ATCT received no further communication from the pilot.
According to a pilot friend of the accident pilot, the accident flight was
the third flight for this airplane and the first flight in this airplane for
the accident pilot. This individual helped the accident pilot install the
engine into the accident airplane and also performed the first 2 flights in
the accident airplane; the second of the two flights occurred on February
21, 2009. That flight was approximately 1.7 hours in duration and was flown
in order to verify that all the oil temperatures, pressures and controls
were "accurate and stable for an extended period of time." After that test
flight he noted two discrepancies, the first discrepancy involved the
altimeter which was locked up at 2,500 feet above mean sea level. The second
discrepancy was that the fuel valve located on the 15 gallon fuel header
tank in front of the pilot had blue staining, which was the same color as
100LL aviation fuel, when he went to close the valve. He further stated that
the accident pilot installed a radio and a cigarette lighter in the airplane
about a week prior to the accident flight. The accident pilot had received
between 10 and 15 hours of flight experience in a KR-2S.
\l ""\l ""
The airplane was examined by an FAA inspector who responded to the accident
site. The airplane was located beneath a tree along a fence row. The
airplane structure, which was comprised of wood and foam/fiberglass,
exhibited extensive fire damage. The FAA reported that a small portion of
the wingtip was located in the adjacent tree and a wheel from one of the
landing gear was located a few feet from the main wreckage. The airplane was
consumed by both an inflight and post impact fire. The inspector was unable
to confirm flight control continuity due to the extensive fire damage.
According to FAA records the accident airplane was manufactured in 2008 and
was issued a special airworthiness certificate on August 8, 2008. The
airplane was equipped with a GM Corvair, six cylinder, 100 horsepower
engine, and a Prince P-Tip wood and composite propeller.
The 1853 recorded weather observation at VLD 2 miles northeast of the
accident site, reported calm winds, clear skies, temperature 24 degrees
Celsius (C), dew point 9 degrees C, and an altimeter setting of 29.95 inches
of mercury


Paul Smith
Brisbane, AUSTRALIA
pk.sm...@bigpond.net.au
http://kr2spacemodulator.blogspot.com/

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