Friday, January 23, 2026

Evektor-Aerotechnik SportStar Max, N2312T, accident occurred on December 27, 2025, at Needles Airport (EED/KEED), Needles, California

  • Location: Needles, CA 
  • Accident Number: WPR26LA073 
  • Date & Time: December 27, 2025, 11:09 Local 
  • Registration: N2312T 
  • Aircraft: EVEKTOR - AEROTECHNIK A S SPORTSTAR MAX 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202222/pdf

http://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N2312T

On December 27, 2025, about 1109 Pacific standard time, an Evektor-Aerotechnik AS Sportstar Max LSA airplane, N2312T, was substantially damaged when it was involved in an accident near Needles, California. The pilot and pilot rated passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that while operating in cruise flight about 6,500 ft mean sea level (msl) to Lake Havasu City Airport (HII), Lake Havasu City, Arizona, all flight instruments and engine parameters were within normal operating ranges. Without warning, the airplane began vibrating violently and the control sticks moved rapidly to their forward and aft limits several. The engine RPM decreased, the vibrations simultaneously subsided and after about 15 seconds the pilot regained the ability to manipulate the control stick. The passenger observed that one of the three propeller blades had departed the propeller hub, and the pilot initiated a forced landing on runway 02 at Needles Airport (EED), Needles, California.

Post-flight inspection of the engine revealed substantial damage to the upper left engine mount which separated from the firewall. The propeller hub was fracture-separated at the blade grip. The blade grip material and the four blade retention bolts were liberated from the hub.

The airplane was recovered to a secure area for further examination.

Piper PA-28-181 Pilot 100i, N505AF, incident occurred on January 21, 2026, at Scottsdale Airport (SDL/KSDL), Scottsdale, Arizona

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N505AF

- History of Flight:
On January 21, 2026, at about 1715 local time, a Piper PA-28-181 Pilot 100i, N505AF, registered to Ameriflyers of Texas Inc and being operated as American Flyers, sustained unknown damage when it was involved in an incident at Scottsdale Airport (SDL/KSDL), Scottsdale, Arizona. The pilot was not injured.

The FAA reported: "Aircraft warming up and inadvertently started to move and struck two parked vehicles." ADS-B data showed a single ping on the far northeast side of the ramp as seen in the figure.

Figure 1: Single ping by ADS-B data recorded at 1820 LT, note close location to parked vehicles.

CubCrafters Carbon Cub FX-3, N972WY, accident occurred on January 21, 2026, near Powder River, Wyoming

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N972WY

- History of Flight:
On January 21, 2026, at about 1512 local time, a privately-registered CubCrafters Carbon Cub FX-3, N972WY, sustained substantial damage when it lost control on landing near Powder River, Wyoming. The sole pilot onboard was not injured.

Cessna 560XL Citation Excel, N802TD, accident occurred on August 14, 2025, near Oakland Park, Florida

  • Location: Oakland Park, FL 
  • Accident Number: ERA25LA301 
  • Date & Time: August 14, 2025, 17:15 Local 
  • Registration: N802TD 
  • Aircraft: Cessna 560XL 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Business 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200796/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N802TD

On August 14, 2025, about 1715 eastern daylight time, a Cessna 560XL, N802TD, was substantially damaged when it was involved in an accident near Oakland Park, Florida. The airline transport pilot and commercial pilot were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 business flight.

The pilot and the commercial pilot arrived at Fort Lauderdale Executive Airport (KFXE), Fort Lauderdale, Florida, about 1100, with the intent to fly the airplane to Orlando Executive Airport (ORL), Orlando, Florida, with an estimated departure time of 1400. The airplane was at FXE to be painted; however, shop personnel informed them upon their arrival that the airplane was not ready to be released, and their 1400 departure time would have to be pushed back. The pilot said he utilized this time to perform a quick walk around the airplane, he adjusted the seat and rudder pedals and made plans to do a final operational check once the airplane was towed to a different location on the airport to be fueled.

The pilot said that when the airplane was ready, he performed an external pre-flight check of the airplane and arranged to add 3,500 pounds of fuel. Personnel from the paint shop arrived at the airplane, and he and the commercial pilot assisted them with multiple operational checks which included engine runs, manipulation of the control column to check flight control positioning, and cycling of the flaps from 0 to 35 degrees (five cycles). During this time, the pilot noticed that the control column seemed a bit closer than he remembered when it was full forward as compared to a different airplane of the same make and model. Otherwise, the controls seemed to move as normal with no unusual binding or limitations.

The pilot said that he and the commercial pilot completed normal pre-engine start checks, started the engines and taxied to the active runway, held short, then taxied onto the runway after receiving takeoff clearance. After taxiing onto the runway, the pilot gave the controls to the commercial pilot. The pilot said the takeoff roll was uneventful but once he retracted the landing gear, he noticed that the airplane was at an unusually high pitch and requested that the  ommercial pilot to lower the nose. He said, it became immediately obvious that she was unable to do this, so he assumed command of the airplane and placed full available forward pressure on the control column. An emergency was declared and a 180° left turn was made in an attempt to return, but both pilots were unable to arrest the climb, climbing to 9,500 ft, which was well above their assigned altitude of 2000 ft mean sea level. The tower controller asked them if they could see the runway and we were unable to see it due to the uncommanded steep climb. The tower controller then asked them to change to a Miami Air Route Traffic Control Center frequency, but he and the commercial pilot had both arms pressing forward on the control column in an attempt to prevent a stall.

Over the next several minutes, the crew attempted to maintain control of the airplane during a series of radical pitch up events into one or more stalls followed by an uncommaded steep pitch down event. The flight then proceeded towards Fort Lauderdale/Hollywood International Airport for landing on runway 10L, where the pilot performed a 360° turn to reduce airspeed. With the throttles at idle power and the speed brakes deployed, he was able to lose about 120 kts of airspeed in the 360° turn but was still about 30 knots above normal approach speed. The pilot continued towards the runway and when in ground effect, the airplane pitched up again uncommanded. The pilot was able to correct that condition and landed on the last 1/4 of the runway before he brought the airplane to a full stop. The pilots then taxied the airplane after receiving approval from emergency personnel.

Postaccident examination of the airplane revealed an elevator pushrod was bent with evidence of contact with an adjacent structural member.