Two Injured In Cirrus SR22 Crash In Georgia

During the descent from 17,500 ft mean sea level (msl), as the airplane was passing through about 7,500 ft msl, the pilot felt a jolt from the engine and subsequently received a low oil pressure alert. The pilot diverted to a closer airport and continued the descent. When the airplane was about 2,000 ft msl, the pilot felt additional jolts and observed sparks emanating from the engine cowling area. Shortly thereafter, the engine lost total power. With no clear landing area available in nighttime conditions over an urban area, he activated the whole-airframe parachute system, and the airplane impacted trees and terrain with the parachute deployed. The fuselage, wings, and empennage sustained substantial damage. Examination of the engine crankcase revealed a fracture hole at the No. 6 cylinder, and the connecting rod had sheared from the upper crankshaft bearing. Disassembly of the engine and its components revealed that the left turbocharger had seized; rub marks were observed inside the turbine housing; metal contaminants were found inside the oil filter; and the oil sump contained damaged connecting rod ends, valve lifters, and engine bearings. The damage is consistent with an oil circulation interruption and catastrophic engine failure. The source of the interruption of oil circulation to the engine could not be determined after engine disassembly.

Probable Cause(s): The total loss of engine power due to the interruption of oil circulation for reasons that could not be determined based on the available evidence.

Note: The report republished here is from the NTSB and is printed verbatim and in its complete form.