No fatalities

5 Jul 2013: PIPER PA 46-350P (N502EU) — Pilot — Nappanee, IN

Nappanee, IN, United States

On 5 Jul 2013, a PIPER PA 46-350P (registration N502EU) operated by Pilot was involved in an aviation accident near Nappanee, IN. No fatalities were reported. Investigators recorded the probable cause as: The failure of the No. 6 piston due to detonation and the subsequent interruption of the engine oil flow that resulted from the piston fragments. This summary draws on records from NTSB; 17 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

A Piper PA-46-350P with registration N502EU made a forced landing after an engine failure during cruise flight near Nappanee, Indiana. The pilot was not injured, and the right wing sustained substantial damage.

Incident

On July 5, 2013, about 1230 eastern daylight time, a Piper PA-46-350P airplane, registration N502EU, was substantially damaged during a forced landing following a loss of engine power during cruise flight near Nappanee, Indiana. The pilot was not injured. The aircraft was registered to GTG LLC and operated by the pilot under 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed, and the flight was operated on an instrument flight rules flight plan. The flight departed from Elkhart Municipal Airport (EKM), Elkhart, Indiana, about 1210, with an intended destination of Indianapolis Executive Airport (TYQ), Indianapolis, Indiana.

The pilot reported that the takeoff and climb out were uneventful. Upon leveling at the assigned cruise altitude of 8,000 feet mean sea level, he heard three loud "bangs." The engine oil pressure and temperature indications exceeded the gauge limit. He was unable to maintain altitude and ultimately executed a forced landing to a field located about 4 miles north-northwest of Nappanee, Indiana. The airplane came to rest upright, with substantial damage to the right wing.

Aircraft and Engine Examination

A postaccident engine examination was conducted under the direct supervision of a Federal Aviation Administration inspector. The examination revealed that a portion of the no. 6 piston face had separated along the perimeter. The damage appeared consistent with exposure to detonation within the cylinder during operation. The no. 5 connecting rod separated near the crankshaft journal. The lower portion of the engine crankcase exhibited a hole immediately above the oil sump. Metallic fragments were recovered from the oil sump, the oil sump screen, and the oil filter.

The accident airplane was powered by a 350-horsepower Lycoming TIO-540-AE2A engine, serial number L-9578-61A.

Maintenance History

The pilot reported that the airframe and engine had accumulated 1,584.3 hours total time at the time of the accident. Maintenance records indicated that on October 19, 2012, the no. 6 cylinder was removed and a new piston, new rings, and new gaskets were installed due to excessive oil consumption. The engine had accumulated 39.5 hours since the work was performed. The records noted that 8 days earlier, on October 11, 2012, the no. 4 cylinder was removed and new rings and gaskets were installed due to excessive oil consumption. The most recent annual inspection was performed on September 11, 2012, at 1,535.4 hours total airframe/engine time. The engine maintenance logbook did not contain any entries subsequent to the October 19th cylinder replacement.

Contributing factors

Recip eng cyl section — FailureDamaged/degraded