On April 16, 2006, at 1318 eastern daylight time, a Piper
PA-28-140, N15507, was destroyed during a forced landing following a loss of
engine power near Avondale, Pennsylvania. The certificated private pilot was
fatally injured, and the passenger was seriously injured. Visual meteorological
conditions prevailed for the local personal flight that departed New Garden
Airport (N57), Toughkenemon, Pennsylvania, about 1315. No flight plan was filed
for the flight conducted under 14 CFR Part 91.
In a telephone interview, the passenger stated that he and the pilot performed
the preflight per the checklist. He said that he was not a pilot, and that the
pilot went over the details of the preflight with him as they moved around the
airplane.
There were no anomalies noted during the preflight, engine start, run-up, or
during taxi. The takeoff was "normal," and the airplane climbed to about 1,500
feet. The passenger said that at that point of the climb, without warning, there
was a loud metallic-sounding explosion, and oil sprayed onto the windscreen. He
said, "It sounded like someone threw a big chunk of metal in the engine, and the
engine cowling opened up like a can of sardines." At the same time, a section of
the propeller departed the airplane.
The passenger said that the pilot maneuvered the airplane toward an open area
bordered by trees, and that the airplane lacked the altitude to clear the
treetops. The airplane struck the trees, burst into flames, and then collided
with terrain. The passenger escaped the wreckage, but burned his hands in his
efforts to assist the pilot.
The pilot held a private pilot certificate with a rating for airplane single
engine land. He was issued a third-class medical certificate in April 2005.
In a telephone interview, a flight instructor acquainted with the pilot stated
that the pilot had accumulated about 160 total hours of flight experience. A
subsequent exam of the pilot's logbook revealed that the pilot had logged 155
hours of flight experience.
An examination of the airplane's maintenance records revealed the airplane was
manufactured in 1972, and had accrued approximately 4,813 total aircraft hours.
The airplane's most recent annual inspection was completed October 26, 2005, at
4,765 aircraft hours. The airplane's engine had accrued a total of about 4,700
hours of operation, and about 475 hours since overhaul.
At 1251, the weather reported at New Castle Airport (ILG), Wilmington, Delaware,
about 10 miles southeast, included clear skies with 10 miles visibility. The
winds were from 300 degrees at 10 knots, gusting to 17 knots. The temperature
was 66 degrees Fahrenheit, and the dew point was 41 degrees Fahrenheit.
The airplane was examined at the site by a Federal Aviation Administration (FAA)
inspector, and with the exception of a propeller blade, all major components
were accounted for at the scene. A nearby resident later recovered the broken
segment of propeller.
The airplane was destroyed by impact and postcrash fire. After the initial
examination, the airplane was moved to a recovery facility. The engine was
removed, and transported to an engine overhaul facility for examination. The
propeller, and the associated broken segment, were removed and transported to
the Safety Board's Materials laboratory in Washington, D.C.
The engine was examined at the Lycoming Engine Factory, Williamsport,
Pennsylvania on May 2, 2006, under the supervision of the Safety Board.
Examination revealed no preimpact anomalies or mechanical deficiencies.
The propeller and the associated broken segment were examined at the Safety
Board Materials Laboratory on July 12, 2006. Examination revealed that a large
portion of the fracture surface displayed crack arrest positions typical of
fatigue cracking. The fracture features emanated from an origin area on the
camber (forward) surface of the propeller.
Microscopic examination revealed an area of corrosion around the fatigue origin,
as well as sanding scratches and conversion (Alodine) coating.
Examination of the airplane's maintenance records revealed that on April 6,
1995, an entry stated, "Remove paint, remove damage from face of blades, correct
angles, dress, track, balance, alodine, and repaint."
A subsequent entry dated May 7, 1998 stated that the propeller was "repitched to
60" following an engine overhaul and conversion. Entries dated July 6, 2001 and
July 25, 2002, reflected annual inspections respectively, each included "filed
and inspected prop" in the text.