Incident Overview
During flight, the pilot noticed a drop in manifold pressure and decided to perform a precautionary landing. While on the base leg to land, heavy smoke and fumes entered the cabin, requiring the pilot to look out of the side vent window to complete the landing. After the aircraft stopped on the runway, a fire in the engine compartment was extinguished.
Examination Findings
An examination revealed that the left intermediate exhaust pipe (Lycoming part number LW-15811) had partially separated at the flange. The engine crossover exhaust assembly had been modified in accordance with AD 89-12-04 and Textron Lycoming Service Bulletin #484, which were intended to prevent this type of failure or separation.
Conclusion
The investigation did not specify a probable cause for the incident. The modifications applied to the engine crossover exhaust assembly were designed to prevent separation of the exhaust pipe at the flange.