Incident Overview
While cruising at 6,500 feet, the engine lost power and the propeller stopped windmilling. The pilot elected to land on a highway. During the landing, the right wing struck overhanging tree limbs, which yawed the aircraft off the right side of the road and down an embankment.
Engine Examination
The engine was removed and disassembled. Examination revealed that the crankshaft had failed due to fatigue at the #2 crank cheek. The fatigue crack originated at the front corner of the #2 cheek lightening hole.
Crankshaft History
The engine was manufactured in 1961. In 1962, the manufacturer redesigned the crankshaft for this model of engine by eliminating the lightening hole. In May 1962, Continental Service Bulletin M62-8 advised of the availability of the improved crankshaft.
Maintenance History
The engine of N5021P was overhauled on July 21, 1975, at 1,486 hours total time. At that time, the crankshaft was removed, magnafluxed, and reinstalled. Time since overhaul was 695 hours. Total engine time was 2,181 hours.