Probable cause
A fatigue crack of the crankshaft at the No. 4 main bearing journal.
NTSB analysis
While the private pilot was conducting a cross-country flight, the airplane's engine started running roughly when the airplane was about 5,500 ft. The pilot pushed the mixture, propeller, and throttle controls to the full forward position, but the engine continued to run roughly. The pilot then decided to return to the departure airport. During the turn back to the airport, oil covered the windscreen. The pilot declared an emergency and asked air traffic control for radar vectors to a closer airport. The pilot was having trouble controlling the airplane, so he asked for vectors to another airport. Seconds later, he saw parts, which he thought were from the propeller, separate from the airplane. The engine then lost total power, and the pilot ditched the airplane into the water below. Postaccident examination of the engine revealed that the crankshaft was fatigue fractured at the No. 4 main bearing journal. The origin surface area of the fatigue crack was obliterated due to relative movement between the mating fracture faces; thus, the investigation could not determine the cause of the fatigue crack.
Text from the NTSB. Open the NTSB docket for ERA17LA069 for the full record.
Event
- Date
- Dec 11, 2016
- Type
- Accident
- Place
- Shoreham, New York
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Beech A36
- N-number
- N69286
- Category
- Airplane
- Year built
- 1984
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.