Forced Landing
The airplane made an off-airport forced landing following a loss of engine power. According to the pilot, approximately 20 minutes after takeoff, the engine stopped, and he performed a forced landing in a dirt field. During the landing roll, the nose wheel dropped into a culvert, causing substantial damage to airframe structural members.
Previous Maintenance
The day before the accident, another pilot reported an "rpm bump" to maintenance personnel. Technicians discovered a leak in the oil cooler return line and repaired it.
Engine Examination
After the accident, examination of the engine determined that the rpm topped out at over 3,000 rpm. The maximum rated speed for the engine was 2,970 rpm. Textron Lycoming Service Bulletin (SB) 3691 defines an overspeed as an increase of no more than 10 percent of rated engine rpm for a period not exceeding 3 seconds. The overspeed observed exceeded 10 percent, which, according to Chart 11 of SB 3691, requires engine disassembly and inspection in accordance with the applicable overhaul manual. Further inspection revealed that the rod cap separated from the rod on the number 3 cylinder, and pieces of metal were found throughout the interior of the engine.