Accident Overview
On November 18, 2024, at approximately 1530 eastern standard time, an experimental amateur-built Just Aircraft Highlander, registration N102XP, sustained substantial damage following a forced landing near Fountain Inn, South Carolina. The pilot, an airline transport pilot, reported minor injuries. The flight was conducted under Title 14 Code of Federal Regulations Part 91 as a personal flight.
Pilot Account
The pilot stated that the preflight inspection and ground operation were routine. After takeoff, during the initial climb, the engine suddenly lost all power. With no open areas ahead, the pilot elected to execute a forced landing into the treetops. The airplane settled into the trees, then fell to the ground, coming to rest approximately one-quarter mile past the departure end of the turf runway. The pilot secured the airplane and was met by first responders.
Wreckage Examination
Federal Aviation Administration (FAA) inspectors examined the wreckage at the accident site. The airplane came to rest upright against trees. No fire was present. Substantial damage was confirmed to the fuselage, empennage, and right wing. The wreckage was subsequently recovered to a salvage facility for further examination.
Engine and Systems Inspection
At the salvage facility, the engine was found to have sustained only minor damage. The spark plugs appeared normal in color and wear when compared to a manufacturer’s inspection chart. Internal engine continuity and compression were confirmed. Fuel was present in both carburetor bowls, and no obstructions were found in the fuel system. The oil and cooling systems were intact.
Engine Test Run
After repairing one intake manifold and reattaching the associated carburetor, the engine was prepared for a test run. Secured on a forklift, the engine started on the first attempt. A run was performed using the electric fuel pump, and then a second run using only the engine-driven pump. No anomalies were found during the engine runs that would have precluded normal operation.
Conclusion
The accident resulted in substantial damage to the aircraft, but the pilot sustained only minor injuries. The engine's sudden power loss could not be attributed to any mechanical anomaly identified during post-accident examination and testing.