N6868D is a 1969 Piper PA-32-300. It is a fixed-wing single-engine aircraft with 6 seats, powered by a Lycoming TI0-540 SER rated at 310 horsepower. The registration is active, with the registrant based in Cincinnati, OH. Its standard airworthiness certificate was issued in Feb 1969. It has been registered to its current owner since Apr 2005. This page also carries 1 NTSB event.
- 57 years old
- 1 of 1,040 Piper PA-32-300
2005
1969
That's everything on file so far — TailWiki checks the FAA registry daily and adds new entries as N6868D's record changes.
On September 1, 2023, about 2038 eastern daylight time, a Piper PA-32-300, N6868D, was substantially damaged when it was involved in accident near Cincinnati, Ohio. The pilot received minor injuries and the three passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
According to the pilot, she departed Cincinnati Municipal Airport/Lunken Field (LUK), Cincinnati, Ohio, about 2010 for a local flight with friends. During cruise flight, at an altitude of 4,500 ft mean sea level, the engine started “sputter” and there was a smell of “burning and avgas.” The pilot made the decision to return to LUK. She contacted the LUK tower about 10 miles away and informed them of the engine trouble. She called the tower again 5 miles from the airport, stated that she experienced complete engine failure, and was heading for the river for a forced landing. She subsequently contacted the tower again and stated that she was unable to reach the river and would be going down in trees about 5 miles from the airport. She secured the engine and the airplane collided with trees and came to rest on its tail section, resulting in substantial damage to the empennage, tail section, and wings.
The pilot stated that after the engine started to sputter, she switched from the right tip tank to the left main tank, then the right main tank, and subsequently the left tip tank during her troubleshooting attempts.
Postaccident examination of the engine established compression in each of the cylinders and continuity to the accessory drive section, as the magnetos’ impulse couplings could be heard when the propeller was rotated by hand. The spark plug wires appeared new and in good condition. The fuel flow divider, nor injectors showed any signs of fuel leakage. The propeller blades were straight and not damaged. The spinner dome was impact damaged on one side. There were no signs of oil leakage around the engine. No anomalies were noted with the engine that would have precluded normal operation.
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