Friday, February 06, 2026

Piper PA-28-180 Cherokee D, N6516J, accident occurred on January 10, 2026, near Port St. Lucie, Florida

  • Location: Port St. Lucie, FL 
  • Accident Number: ERA26LA091 
  • Date & Time: January 10, 2026, 19:25 Local 
  • Registration: N6516J 
  • Aircraft: Piper PA-28-180 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202282/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N6516J

On January 10, 2026, about 1925 eastern standard time, a Piper PA-28-180, N6516J was substantially damaged when it was involved in an accident near Port St. Lucie, Florida. The pilot and passenger sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, prior to takeoff from Okeechobee County Airport (OBE), Okeechobee, Florida, he “topped off” the fuel tanks with about 40 gallons of 100LL aviation fuel. As the pilot was preparing to start the airplane’s engine, he turned on the master switch, observed that the cockpit and cabin lights were dim, and could not start the engine.

The pilot requested a “jump start,” which started the engine and he subsequently taxied to the runway and took off, but during the initial climb, the engine was not producing adequate power to maintain a good climb rate. The airplane climbed past 2,000 ft mean sea level, and the pilot began to troubleshoot the “problem,” but shortly after, the airplane experienced a total loss of engine power. The pilot attempted to restart the engine several times using the loss of engine power checklists, but was unsuccessful.

The pilot conducted a descending 180° right turn toward OBE but was too far (10 nautical miles) to reach the airport, and he attempted a forced landing to a field. The airplane impacted trees during the approach, both wings separated and the fuselage impacted terrain in a nose down inverted attitude about 100 ft from the initial tree impact.

After the accident, the pilot stated that he recently purchased the airplane which had been ferried from California to Florida. The airplane’s magnetos had been recently overhauled, and a new wiring harness was installed prior to the purchase. The airplane’s most recent annual inspection was performed on December 9, 2025, which was about 5 years after the previous annual inspection. The ferry pilot who transported the airplane to the pilot informed him that the  alternator was experiencing intermittent drops during the four-day ferry flight, and that each flight leg was about 8 hours per day. No other issues were noted by the ferry pilot.

The airplane was recovered and retained for further examination.

Quicksilver MX II Sprint, N4NH, incident occurred on January 20, 2026, at David Wayne Hooks Memorial Airport (DWH/KDWH), Houston, Texas

  • Location: Spring, TX 
  • Accident Number: CEN26LA097 
  • Date & Time: January 20, 2026, 16:58 Local 
  • Registration: N4NH 
  • Aircraft: Quicksilver II 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202331/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N4NH

On January 20,2026, 1658 central standard time, a Quicksilver II, N4NH, sustained substantial damage when it was involved in an accident at David Wayne Hooks Memorial Airport, DWH, in Spring, Texas. The pilot, sole occupant, sustained no injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot departed runway 17L with intentions of staying in the traffic pattern and making a water landing at the adjacent water runway at the airport. After retracting the landing gear, the engine ran very rough and lost power from the normal 6,500 rpm to about 1,800 rpm. The airplane was about 100 ft above ground level (agl) as the pilot lowered the nose and prepared for landing on the remaining runway. The airplane landed hard on the left side of the runway with the wings level and the landing gear still retracted. The airplane continued into the grass on the left side of runway 17L and came to rest near taxiway H. Just before touchdown, the engine power began to recover, and the engine returned to full power as the airplane was sliding on its floats. The pilot closed the throttle to idle, turned off the engine, and exited the airplane.

During the hard landing the aluminum tubes from the rear engine area to the main landing gear were bent. The engine was displaced aft and the propeller contacted the elevator control tube and severed it. The elevator control horn was fractured and the elevator trim cable was damaged by contact with the propeller. The pilot also reported that several aluminum structural tubes were bent. He stated that there was no other damage to the airplane.

The pilot, with the help of ground personnel, lowered the landing gear, and returned the airplane to the hangar for further inspection.