Thursday, November 06, 2025

Bombardier CRJ-900LR, N902XJ, and Bombardier CRJ-900LR, N480PX, accident occurred on October 1, 2025, at New York-La Guardia Airport (LGA/KLGA), New York, New York

  • Location: New York, NY 
  • Accident Number: DCA26FA001 
  • Date & Time: October 1, 2025, 21:56 Local 
  • Registration: N902XJ (A1); N480PX (A2) 
  • Aircraft: BOMBARDIER INC CL-600-2D24 (A1); BOMBARDIER INC CL-600- 2D24 (A2) 
  • Injuries: 1 Minor, 31 None (A1); 61 None (A2) 
  • Flight Conducted Under: Part 121: Air carrier - Scheduled (A1); Part 121: Air carrier - Scheduled (A2)

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201766/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N902XJ

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N480PX

On October 1, 2025, about 2156 eastern daylight time (EDT), Endeavor Air dba Delta Connection flight 5155, a Mitsubishi Heavy Industries (MHI) RJ CL-600-2D24 (CRJ-900), N902XJ, collided with Endeavor Air dba Delta Connection flight 5047, a MHI RJ CL-600-2D24 (CRJ-900), N480PX, at the intersection of taxiways M and A at LaGuardia Airport (LGA), New York, New York. There were 2 pilots, 2 flight attendants, and 28 passengers on board flight 5155; 1 flight attendant sustained minor injuries. There were no injuries to the 2 pilots, 2 flight attendants, and 57 passengers on board flight 5047. The crew and passengers of both airplanes were deplaned via the main cabin stairs and bussed to the terminal.

Flight 5155 was a scheduled domestic passenger flight operating under the provisions of Title 14 Code of Federal Regulations Part 121 from LGA to Roanoke-Blacksburg Regional Airport (ROA), Roanoke, Virginia. Flight 5047 was a scheduled domestic passenger flight operating under the provisions of Title 14 Code of Federal Regulations Part 121 from Charlotte Douglas International Airport (CLT), Charlotte, North Carolina. Flight 5047 landed at LGA and was taxiing to the terminal on taxiway B. Flight 5155 had pushed back from the gate at LGA and was taxiing on taxiway A. Flight 5047 exited taxiway B and had turned onto taxiway M when it was struck by the right wing of flight 5155 at the intersection of taxiways M and A.

In response to the accident, the NTSB launched a go-team to LGA. As part of the investigation, the NTSB also invited qualified parties to participate in the investigation. Parties named to the investigation included the Federal Aviation Administration (FAA), Endeavor Air, the Air Line Pilots Association (ALPA), and the National Air Traffic Controllers Association (NATCA). The Transportation Safety Board of Canada (TSB Canada), representing the State of Design and State of Manufacture for the airplanes, assigned an Accredited Representative. MHI was named as a technical advisor by the Canadian Accredited Representative.

The parties were formed into specialized investigative groups led by NTSB group chairs in the areas of Operations, Human Performance, Air Traffic Control (ATC), and Structures. Additionally, NTSB specialists in the areas of Survival Factors, Airport Operations, Cockpit Voice Recorder (CVR), and Flight Data Recorder (FDR) were assigned.

History of Flight

The following timeline (table 1) was constructed from certified ATC audio recordings and Automatic Dependent Surveillance-Broadcast (ADS-B) data provided by the FAA. All times are in EDT. Graphical depictions of the movements of flights 5047 and 5155 leading up to the collision are shown in figure 1. 

Flight 5047 landed on runway 4 and exited the runway on taxiway G. The LGA ground controller instructed flight 5047 to taxi on taxiway B to taxiway M and on to lane 12 in the gate area, which would require flight 5047 to cross taxiway A from M. The crew of flight 5047 subsequently read back the ground controller’s instructions. 

The crew of flight 5155 contacted the ground controller and stated they were in lane 17 of the gate area. The ground controller subsequently instructed flight 5155 to runway 13 via taxiways A to E, to hold short of runway 4, and to “give way” to another Endeavor Air airplane at taxiway M. The crew of flight 5155 read back the ground controller’s instructions. At this time flight 5047 was on taxiway B at the intersection with taxiway L, and moving towards taxiway M. Subsequently, the ground controller provided the crew of flight 5155 a new departure frequency, which the crew of flight 5155 confirmed, while they were still located in the gate area. 

Airport surveillance camera videos that captured the collision showed flight 5047 had turned onto taxiway M moving south, and flight 5155 moving east on taxiway A. Flight 5047 abruptly stopped as it approached the intersection with taxiway A, and about 2 seconds later the right wing of flight 5155 collided with the nose of flight 5047. Flight 5047 appeared to turn to the left about 1 second prior to the collision.

The CVR and FDR from both airplanes were recovered and sent to the NTSB’s Vehicle Recorder Laboratory in Washington, DC for analysis. All four recorders were successfully downloaded and captured the accident. 

Postaccident examination of N480PX (flight 5047) found substantial damage to the nose and the captain’s windshield (see figure 2). Postaccident examination of N902XJ (flight 5155) found substantial damage to the outboard section of the right wing, including separation of the outboard slat, aileron, and wing tip (see figure 3).

The meteorological aerodrome report (METAR) from LGA, issued on October 1, 2025, at 2151 EDT, showed clear skies and visibility of 10 statute miles.

Postaccident interviews of the flight crew of flight 5047 revealed that the arrival into LGA was uneventful. The captain of flight 5047 estimated their taxi speed on taxiway B was about 9 knots. The flight crew recalled nothing unusual about the taxi instructions from the LGA ground controller. The captain slowed the airplane to turn onto taxiway M. The first officer leaned forward to clear the right side of the airplane at that time. As they made the turn onto taxiway M, the captain was focused on clearing lane 12 but saw another airplane to his left and brought the airplane to a stop. A few seconds later the right wing of flight 5155 impacted the nose and windshield of flight 5047, causing substantial damage to both airplanes.

Postaccident interviews of the flight crew of flight 5155 revealed that, after pushback from the gate at LGA, both engines were turned on for taxi. The first officer of flight 5155 recalled hearing the full taxi clearance and recalled it was not confusing. The captain of flight 5155 recalled hearing the taxi clearance up to holding short of runway 4 and did not recall hearing the instruction to give way to another Endeavor Air airplane. The captain stated he was focused on calculating performance numbers for the landing at ROA. 

Flight 5155 started its taxi, and while taxiing on taxiway A, the flight crew accomplished the taxi checklist, with the first officer calling out the checklist step and the captain verifying the step. The captain recalled he was looking down into the cockpit to visually verify the airplane trim setting as part of the checklist, and when he looked up he saw flight 5047 to the right. The captain of flight 5155 stated he attempted to veer left to avoid the other aircraft, and the captain of flight 5047 stated that he applied brakes immediately before the collision. 

The investigation continues.

Denney Kitfox 2, N8610X, fatal accident occurred on October 17, 2025, at Avery County Airport/Morrison Field (7A8), Spruce Pine, North Carolina

  • Location: Spruce Pine, NC 
  • Accident Number: CEN26FA022 
  • Date & Time: October 17, 2025, 11:54 Local 
  • Registration: N8610X 
  • Aircraft: KITFOX II 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201880/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?NNumberTxt=N8610X

On October 17, 2025, about 1154 eastern daylight time, a Kitfox II airplane, N8610X was destroyed when it was involved in an accident near Spruce Pine, North Carolina. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Witness 1 reported that the pilot completed one takeoff and landing on grass runway 17 at the Avery County Airport-Morrison. Later, two witnesses saw the airplane taxiing on the grass east of the asphalt runway near the windsock. Witness 1 reported that he briefly observed what appeared to be the accident airplane executing a takeoff roll from the east side of the airport, parallel to runway 17 (Figure 1).


The accident site was located about 60 ft below airport field elevation on the side of a brush-covered embankment southeast of the approach end of runway 35. Examination of the accident site revealed that the airplane impacted the terrain in a nose-low attitude on a northwesterly heading (See Figure 2).

The airframe fabric was consumed by the post impact fire, and the underlying tubular structure exhibited aft crushing consistent with impact damage. Both wings remained partially attached to the fuselage, with both flaperons found separated near their respective wings. Flight control continuity was established from the cockpit to the center fuselage near the wing roots for flaperon controls. The empennage, to include the horizontal and vertical stabilizer, elevator, and rudder, remained attached to the airframe. The rudder and elevator controls were continuous from the cockpit to their respective control surfaces.

The engine was found partially attached to the airframe, with the propeller separated from the engine at the gearbox. The main wreckage was partially embedded in the ground. All three composite propeller blades were found to be thermally damaged and relatively straight. Blade A was separated near the propeller hub, blade B was partially cracked near the propeller hub,and blade C was unremarkable.

Initial examination of the engine revealed damage to the engine assembly consistent with impact and the post impact fire. The crankshaft could not be rotated due to damage consistent with the impact sequence. The cylinder head and cylinders were removed, and no anomalies were observed to the engine that would have precluded normal operation.

Beechcraft V35A Bonanza, C-FETM, fatal accident occurred on October 15, 2025, near Austin, Nevada

  • Location: Austin, NV 
  • Accident Number: WPR26FA019 
  • Date & Time: October 15, 2025, 14:47 Local 
  • Registration: CFETM 
  • Aircraft: Beech V35 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201879/pdf

On October 15, 2025, about 1447 Pacific daylight time, a Beech V35, C-FETM, was substantially damaged when it was involved in an accident near Austin, Nevada. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Preliminary ADS-B data showed that the airplane departed West Kootenay Regional Airport (YCG), Castlegar, British Columbia, Canada, about 0903, flew southwest, and arrived at Grant County International Airport (MWH), Moses Lake, Washington, about 1003. The airplane departed MWH about 1149, flew south/southeast and climbed to an altitude of 9,300 ft mean sea level (msl). About 1345, the airplane initiated a climb to 12,000 ft msl, then flew between 11,100 ft msl and 12,400 ft msl for the remainder of the flight track data. About 1414, the airplane turned to the southwest. About 1419, the airplane began a turn toward the southeast and remained on a southeasterly heading until the end of the flight track data. The data ended about 7 miles northwest of the accident site and showed the airplane at an altitude of 11,100 ft msl.

On October 16, 2025, at 1331, an Alert Notice (ALNOT) was issued, following reports from family members, that the airplane was overdue. The wreckage was subsequently located later that day by a private citizen who volunteered to search by air, about 16 miles northeast of Austin, Nevada, at an elevation of 10,195 ft msl.

Examination of the accident site revealed that the airplane impacted mountainous terrain near the top of Mt. Callaghan, on the western slope of the mountain near the peak. The debris field was about 992 ft in length and was oriented on a magnetic heading of 147° from the first identified point of contact (FIPC) to the main wreckage, and a magnetic heading of 172° from the main wreckage to the end of the debris field. The main wreckage was located about 574 ft from the FIPC and came to rest inverted on a magnetic heading of about 270°, on the eastern slope of the mountain. All major structural components of the airplane were observed throughout the debris field. (See figure 1.)

The wreckage was recovered to a secure facility for further examination.

Piper PA-24-250 Comanche, N7412P, accident occurred on August 28, 2025, near Richmond Field Airport (69G), Gregory, Michigan

  • Location: Gregory, MI 
  • Accident Number: CEN25LA357 
  • Date & Time: August 28, 2025, 15:50 Local 
  • Registration: N7412P 
  • Aircraft: Piper PA-24-250 
  • Injuries: 1 Serious
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200924/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N7412P

On August 28, 2025, at about 1550 eastern daylight time, a Piper PA-24-250 airplane, N7412P, was substantially damaged when it was involved in an accident near Gregory, Michigan. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

The pilot reported that he and the airplane owner flew the airplane from the Toledo Suburban Airport (DUH), Lambertville, Michigan, to the Charlevoix Municipal Airport (CVX), Charlevoix, Michigan, where he dropped off the airplane owner. He then re-boarded the airplane to return to DUH alone. He reported that the flight from DUH to CVX was uneventful, as was the flight from CVX toward DUH, until about 1:20 into the flight. At this time the engine suddenly stopped producing power. The pilot was in communication with air traffic control (ATC) and reported the power loss. The controller provided the pilot with options for nearby airports and the pilot elected to attempt a landing at the Richmond Field Airport (69G), near Gregory, Michigan. The airplane came to rest in a field just south of 69G and a post-impact fire ensued which consumed the cabin portion of the airplane.

Postaccident examination of the engine revealed extensive fire damage. Initially the engine could not be rotated; however, after removal of the fire damaged accessories and accessory housing on the back of the engine, the remainder of the engine was free to rotate. Thumb compression was verified on all cylinder and valve continuity was verified. All of the accessory case gears were intact. The engine still had an unknown amount of oil that drained out of the broken crankcase during the examination. Examination of the accessory case components revealed that the vacuum pump drive shaft, the tachometer drive shaft, and the oil pump drive shaft were seized in their bores. Disassembly of the accessory case components did not reveal any anomalies and the seizures were consistent with the fire damage. The rear mounted magnetos were extensively damaged by the postimpact fire and were unable to be tested.

Beechcraft 58P Baron, N121GJ, fatal accident occurred on October 5, 2025, near Williston Regional Airport (X60), Williston, Florida

  • Location: Williston, FL 
  • Accident Number: CEN26FA005 
  • Date & Time: October 5, 2025, 16:10 Local 
  • Registration: N121GJ
  • Aircraft: Beech 58P 
  • Injuries: 3 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201781/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N121GJ

On October 5, 2025, at 1610 eastern daylight time, a Beech 58P airplane, N121GJ, was destroyed when it was involved in an accident near Williston, Florida. The pilot and two passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to people familiar with the flight, the pilot intended to fly the two passengers back to Florida after their hunting trip in Kentucky. The airplane departed Lebanon Springfield Airport (6I2), Springfield, Kentucky, about 1318 and climbed to about 17,000 ft mean sea level. The pilot was receiving radar services from air traffic control (ATC) and was operating under visual flight rules. About 50 miles northwest of the intended destination, Williston Regional Airport (X60), Williston, Florida, the airplane began to descend. About 10 miles northwest of X60 the airplane was level about 1,300 ft msl and 180 kts ground speed, when ATC terminated radar services and transferred communications to the X60 common traffic advisory frequency. About 4 miles northwest of X60, the airplane turned right, and the ground speed increased from 158 kts to 168 kts. In the final 18 seconds of the flight the airplane made a steep descent about 4,000 ft per minute. A pilot witness who was flying about one mile to the west, observed the accident airplane in a steep descent with a 90° bank angle before it impacted the ground and exploded.

The airplane impacted a peanut field on a 200° heading, and the debris field extended about 765 ft. The main wreckage came to rest 1.76 nm northwest of the approach end of runway 5 at X60. The airplane was highly fragmented and exhibited thermal damage in many areas. The initial impact area contained pieces of the right wing tip. The debris field contained all major components of the airplane. The fuselage was mostly consumed by the post-impact fire and the empennage remained relatively intact with minimal fire damage. The landing gear and flaps were both found retracted. The left and right engines were separated from the airplane and sustained impact damage. The propeller blades from each engine were all separated from their respective propeller hubs and found in the debris field. The airplane was equipped with multiple avionics devices with recording capability, which were sent to the NTSB Vehicle Recorder Laboratory for data extraction.

The airplane was retained for further examination.

Bell 222SP, N222EX, accident occurred on October 11, 2025, in Huntington Beach, California

  • Location: Huntington Beach, CA 
  • Accident Number: CEN26FA015 
  • Date & Time: October 11, 2025, 14:01 Local 
  • Registration: N222EX 
  • Aircraft: Bell 222 
  • Injuries: 3 Serious, 2 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201834/pdf

http://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N222EX

On October 11, 2025, at 1401 Pacific daylight time, a Bell 222 helicopter, N222EX, was substantially damaged when it was involved in an accident near Huntington Beach, California. The pilot and passenger received serious injuries. One person on the ground received serious injuries and two others received minor injuries. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he and the passenger departed from Redlands, California, and intended to land in a Huntington Beach parking lot for a large public event. The pilot approached Huntington Beach from north, then circled for a high-speed pass above Pacific Coast Highway headed northwest. The pilot circled again and completed a slow pass above the highway, then approached the parking lot from southeast. As the helicopter descended above the parking lot, he made a small right pedal input to straighten the helicopter, then the nose veered left, and he heard a loud noise from the back left side. The pilot turned right and increased the power to fly away from the confined landing area. As the right turn rate increased, the pilot was unable to maintain control of the helicopter.

Witness photos and videos revealed that during the high-speed pass, there were no apparent anomalies with the helicopter. During the slow pass, one of the tail rotor pitch links was disconnected from a tail rotor blade. As the helicopter approached the parking lot for landing, the pitch link remained disconnected (see figure 1).

The helicopter turned right and ascended as pieces of the tail rotor assembly began to separate. The tail rotor gearbox separated in half and the output side remained attached to the tail rotor assembly, then landed in the parking lot. The helicopter continued to spin right then impacted a staircase at the end of a pedestrian bridge.

Postaccident examination of the separated tail rotor assembly revealed that both pitch horns were fractured in half. All pitch horn bolts and associated hardware remained installed and secure.

The helicopter was retained for further examination. 

Airbus Helicopters H130, N414RX, fatal accident occurred on October 6, 2025, in Sacramento, California

  • Location: Sacramento, CA 
  • Accident Number: WPR26FA008 
  • Date & Time: October 6, 2025, 19:05 Local 
  • Registration: N414RX 
  • Aircraft: Airbus Helicopters EC 130 T2 
  • Injuries: 3 Serious 
  • Flight Conducted Under: Part 135: Air taxi & commuter - Non-scheduled - Air Medical (Discretionary)
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201802/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N414RX

On October 6, 2025, about 1905 Pacific daylight time, an Airbus Helicopters EC-130 T-2, N414RX, was substantially damaged when it was involved in an accident in Sacramento, California. The pilot, flight paramedic and flight nurse sustained serious injuries. Subsequently, the flight nurse succumbed to her injures four days after the accident The helicopter was operated as a Title 14 Code of Federal Regulations Part 135 air medical flight.

The helicopter had just departed UC Davis Medical Center Tower II Heliport (3CLO), Sacramento, California, with a planned destination of Mc Clellan Airfield (MCC), Sacramento, California. The flight paramedic reported that shortly after takeoff she noticed the power had gone out and the helicopter was autorotating towards U.S. Route 50. She made a mayday call on the company Flight Guard frequency.

Subsequently, the helicopter came to rest on its left side in the eastbound lanes of U.S. Route 50, about 1,600 ft north from 3CLO. A main rotor blade strike impression was observed on the residential side of the fence that enclosed the highway. Furthermore, a section of the outer portion of the main rotor blade was discovered embedded in the roof of a detached garage on a residential home located next to the highway.

A review of ADS-B data revealed that the helicopter took off and climbed to a maximum altitude of about 500 ft mean sea level. Shortly thereafter, the helicopter was in descent for about the final 11 seconds of the flight.

Postaccident examination revealed that the helicopter’s fuselage and main rotor blades sustained substantial damage. The helicopter was recovered and retained for further examination.

Cessna 172G Skyhawk, N4390L, accident occurred on October 10, 2025, near Kaolin Field Airport (OKZ/KOKZ), Sandersville, Georgia

  • Location: Sandersville, GA 
  • Accident Number: ERA26LA012 
  • Date & Time: October 10, 2025, 20:15 Local 
  • Registration: N4390L 
  • Aircraft: Cessna 172 
  • Injuries: 1 Minor, 1 None 
  • Flight Conducted Under: Part 91: General aviation - Positioning

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201843/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N4390L

On October 10, 2025, about 2015 eastern daylight time, a Cessna 172G, N4390L, was substantially damaged when it was involved in an accident near Sandersville, Geogia. The pilot was not injured and the passenger sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 positioning flight.

According to the pilot, maintenance had just been completed on the airplane, and the purpose of this flight was to take it back to the airport where the airplane was based. He performed a normal preflight inspection of the airplane and stated that the engine run-up was normal. The pilot also confirmed that he had used a measuring stick to check the fuel quantity. During the departure, he reported that the airplane left the ground, but about 250 ft above ground level, the engine rpm began to drop. The pilot attempted to quickly troubleshoot by “pumping” the throttle lever and verifying the fuel selector position. The airplane was unable to maintain altitude and impacted the tops of trees.

A postaccident examination of the wreckage by a Federal Aviation Administration inspector revealed that the wing fuel tanks contained fluid that smelled and appeared visually consistent with automotive fuel. The airplane sustained substantial damage to both wings, fuselage, and empennage.

The airplane contained avionics that were capable of recording airframe and engine data. These were retained for further examination and data download.

The wreckage was retained for further examination.

Cessna 210A Centurion, N911MC, accident occurred on September 12, 2025, near Gore Springs, Mississippi

  • Location: Gore Springs, MS
  • Accident Number: CEN25LA384
  • Date & Time: September 12, 2025, 17:39 Local
  • Registration: N911MC
  • Aircraft: Cessna 210A
  • Injuries: 1 Minor
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201026/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N46CR

On September 12, 2025, about 1739 central daylight time, a Cessna 210A airplane, N911MC, was substantially damaged when it was involved in an accident near Gore Springs, Mississippi. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported a loss of engine power during cruise flight. He subsequently executed a forced landing on a two-land road. The wings struck trees and a road sign during the landing. Both wings sustained leading-edge impact damage to the outboard 2 -3 feet and near midspan.

ADS-B data revealed the flight departed from the Gulfport-Biloxi International Airport (GPT) at 1550 and climbed to a cruise altitude of about 4,500 ft mean seal level (msl). About 1731, the airplane entered a descent that continued until the final data point which was consistent with the reported loss of engine power. The final ADS-B data point was recorded at 1738:17, with an associated altitude of 1,000 ft msl.

An engine examination is planned following recovery of the airplane to an appropriate facility.

Piper PA-46-310P Malibu, N46CR, accident occurred on October 26, 2025, near El Paso, Texas

  • Location: El Paso, TX 
  • Accident Number: CEN26LA030 
  • Date & Time: October 26, 2025, 09:18 Local
  • Registration: N46CR 
  • Aircraft: Piper PA-46-310P 
  • Injuries: 3 None 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201923/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N46CR

On October 26, 2025, about 918 mountain daylight time, a Piper PA46-310P, N46CR, was substantially damaged when it was involved in an accident near El Paso, Texas. The pilot and two passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported he was climbing to his enroute cruise altitude when the engine made a loud bang, followed by decreasing temperature readings and a low oil pressure warning. The pilot declared an emergency, requested vectors to the nearest airport, and performed the engine failure emergency checklist. The pilot assessed different landing options before deciding on a north-south dirt road. The airplane touched down about 500 feet before a steep incline in the road. The pilot applied heavy braking until he spotted a 3 foot hole in the road, at which time he released the brakes and applied full aft elevator. All three landing gear separated from the airplane as the airplane went into and past the hole in the road. The wings and fuselage were substantially damaged. Once the airplane came to rest, the pilot shut down the electrical systems and began evacuation of the occupants through the emergency exit. The main door had become blocked by a tree and some brush.

Post accident examination of the airplane revealed a hole in the top of the crankcase by the number two cylinder. The magneto above the hole was dislodged from its mounting point. Clean looking oil was present on the dipstick. The airplane was retained for further examination.

Denney Kitfox 3, N5241N, accident occurred on October 27, 2025, near Chilton, Texas

  • Location: Chilton, TX 
  • Accident Number: CEN26LA031 
  • Date & Time: October 27, 2025, 05:30 Local 
  • Registration: N5241N 
  • Aircraft: Denney Kitfox 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201928/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N5241N

On October 27, 2025, about 0530 central daylight time, a Denney Kitfox III airplane, N5241N, was substantially damaged when it was involved in an accident near Chilton, Texas. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The flight departed from the Easterwood Field Airport (KCLL), College Station, Texas, about 0445 and was en route to the McGregor Executive Airport (KPWG), Waco, Texas. About 20 nautical miles from KPWG, the engine briefly sputtered. The pilot verified all switches and fuel selectors were in the proper positions. The engine began to violently shudder, and engine power began to degrade. The pilot pitched for best glide and flew towards a nearby airfield. Shortly after, the engine completely lost power, and the pilot set up for a forced landing to a field. Avoiding a power line pole, the airplane touched down hard in a field. Due to an unseen fence line, the pilot applied the wheel brake hard to nose the airplane over and avoid a collision with the fence. The airplane nose over and came to rest inverted.

Substantial damage was sustained to the fuselage and wings. The airplane was retained for further examination.

SIAI-Marchetti SM.1019, N3172U, accident occurred on October 2, 2025, at Richland Airport (RLD/KRLD), Richland, Washington

  • Location: Richland, WA 
  • Accident Number: WPR26LA006 
  • Date & Time: October 2, 2025, 10:50 Local 
  • Registration: N3172U 
  • Aircraft: SIAI-MARCHETTI SM 1019 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201797/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N3172U

On October 2, 2025, about 1050 Pacific daylight time, a Siai-Marchetti SM 1019, N3172U, sustained substantial damage when it was involved in an accident near Richland, Washington. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he departed Tri-Cities Airport (PSC), Pasco, Washington, on a local flight. About 45 minutes into the flight, he observed uncommanded engine rpm oscillations and decided to make a precautionary landing at Richland Airport (RLD), Richland, Washington. While on the downwind leg for runway 19, as the pilot moved the condition lever forward, it felt like the propeller was moving unsolicited, from beta to flight idle. He recalled that when he tried to return the propeller from beta, to flight idle, the engine rpm oscillations increased significantly.

As the pilot turned onto final for runway 19, he noticed that the engine rpm oscillations became more erratic. The pilot stated that when the propeller felt like it had entered beta, the airspeed decreased below the airplane’s stall speed and thrusted the occupants forward in their seats. Subsequently, the pilot lowered the nose added power and noted that the slightest increase of the power control lever resulted in an extreme engine rpm increase followed by the nose of the airplane pitching upward. He applied 15° flaps and slowed the airplane to about 50 knots.

The pilot stated that after touchdown, the landing roll was normal for about 50 ft. As he applied brakes, the engine rpm increased and the airplane became airborne. Subsequently, the airplane turned left, touched down hard on the runway, and the right main landing gear collapsed. Subsequently, the airplane exited the left side of the runway and came to rest upright. 

Postaccident examination of the airplane revealed that the right wing was substantially damaged. The airplane was recovered to a secure location for further examination.

Cirrus SR22 G2, N812SE, accident occurred on October 2, 2025, near Talladega, Alabama

  • Location: Talladega, AL 
  • Accident Number: ERA26LA001 
  • Date & Time: October 2, 2025, 11:26 Local 
  • Registration: N812SE 
  • Aircraft: CIRRUS DESIGN CORP SR22 
  • Injuries: 1 Minor, 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201776/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N812SE

On October 2, 2025, at 1126 central daylight time, a Cirrus SR22, N812SE, was substantially damaged when it was involved in an accident near Talladega, Alabama. The commercial pilot sustained minor injuries, and the two passengers were not injured. The airplane was being operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The flight originated from Birmingham–Shuttlesworth International Airport, Birmingham, Alabama, and was destined for Talladega Municipal Airport (ASN), Talladega, Alabama. According to the pilot, after departure he climbed to 3,500 ft., mean sea level (msl). While descending toward ASN, he advanced the throttle, but the engine did not respond. He attempted to restore power; however, engine power did not increase. The pilot reported that the airplane’s altitude was below the minimum required for Cirrus Airframe Parachute System (CAPS) deployment, so he configured the airplane for a glide and performed a forced landing to an open field about 7 nautical miles west of ASN. During the landing roll, the airplane struck an agricultural irrigation pivot, which resulted in substantial damage to the right wing and right engine cowling.

The airplane was recovered and retained for further examination.

Progressive Aerodyne SeaRey, N2090S, accident occurred on September 28, 2025, near Rotonda West, Florida

  • Location: Rotonda West, FL 
  • Accident Number: ERA25LA368 
  • Date & Time: September 28, 2025, 11:26 Local 
  • Registration: N2090S 
  • Aircraft: ELMORE TRAVIS C SEAREY 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201737/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N2090S

On September 28, 2025, at 1126 eastern daylight time, an experimental, amateur-built Searey, N2090S, was substantially damaged when it was involved in an accident near Stump Pass, Florida. The private pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that the preflight, taxi, and takeoff were all normal with no observed anomalies. After departing from Manatee Airport, Palmetto, Florida, the pilot stated he flew for about an hour and a half in the local area. While flying north along the beach at about 300 ft above ground level, the pilot reported that the engine RPM dropped to about idle. The pilot pushed the nose down, pushed the throttle to maximum, and turned on the second fuel boost pump. The pilot reported there was no change in RPM and the engine continued to operate at idle. The pilot determined he would be unable to make it back to an airport and so he performed a forced landing in choppy water. During the landing, the airplane’s nose impacted a wave. A postaccident examination revealed that the airplane sustained substantial damage to the fuselage and to the horizontal stabilizer.

The wreckage was retained for further examination.

SIAI-Marchetti SF.260B, N272C, accident occurred on September 26, 2025, at Billings-Logan International Airport (BIL/KBIL), Billings, Montana

  • Location: Billings, MT 
  • Accident Number: WPR25LA295 
  • Date & Time: September 26, 2025, 10:40 Local 
  • Registration: N272C 
  • Aircraft: SIAI-MARCHETTI SF260B 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201730/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N272C

On September 26, 2025, about 1040 mountain daylight time, a SIAI-MARCHETTI SF 260B, N272C, was substantially damaged when it was involved in an accident near Billings, Montana. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations part 91 flight.

The pilot reported that shortly after rotation from runway 28R, the airplane began to drift left. He applied corrective control inputs and was able to maintain control while in ground effect, but the airplane would not climb. The airplane then drifted away from the runway to the right, and began to settle, after which it struck the ground. The landing gear collapsed during the impact sequence, and the airplane sustained substantial damage to the left wing and aft cabin structure.

The airplane was recovered for further examination. 

Wind Speed/Gusts, Direction: 20 knots / 28 knots, 320°
Temperature/Dew Point: 23°C /-3°C

Consolidated PBY-5A Catalina, N222FT, accident occurred on October 31, 2025, at Mark Anton Airport (2A0), Dayton, Tennessee

This is preliminary information, subject to change, and may contain errors. Any errors in this post will be corrected when the preliminary report is released.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N222FT

- History of Flight:
On October 31, 2025, at about 1818 local time, a 
Consolidated PBY-5A Catalina, N222FT, registered to PBY LLC out of Wilmington, Delaware, sustained substantial damage when it was involved in an accident at Mark Anton Airport (2A0), Dayton, Tennessee. There were no injuries. The local flight originated from 2A0.

According to available information, the vintage 1945 airplane suffered a landing gear collapse and is being investigated by the NTSB as an accident, case number ERA26LA028.

The airplane was undergoing maintenance at the airport and had not flown in a while. The accident occurred during the first post maintenance test flight (as per a social media post and flight tracking history).