- Location: Maricopa, Arizona
- Accident Number: WPR24LA086
- Date & Time: February 11, 2024, 10:30 Local
- Registration: N691B
- Aircraft: Beech A35
- Aircraft Damage: Substantial
- Defining Event: Landing gear not configured
- Injuries: 3 None
- Flight Conducted Under: Part 91: General aviation - Personal
Wednesday, June 18, 2025
Landing gear not configured: Beechcraft A35 Bonanza, N691B, accident occurred on February 11, 2024, at Ak-Chin Regional Airport (A39), Maricopa, Arizona:
Dynamic rollover: Bell 505 Jet Ranger X, N9TV, accident occurred on April 30, 2025, at Wiley Post Airport (PWA/KPWA), Oklahoma City, Oklahoma
- Location: Bethany, Oklahoma
- Accident Number: CEN25LA167
- Date & Time: April 30, 2025, 17:52 Local
- Registration: N9TV
- Aircraft: BELL HELICOPTER TEXTRON CANADA 505
- Aircraft Damage: Substantial
- Defining Event: Dynamic rollover
- Injuries: 1 Minor, 1 None
- Flight Conducted Under: Part 91: General aviation - Business
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200106/pdf
https://data.ntsb.gov/Docket?ProjectID=200106
After completing a two-hour news gathering flight, the pilot returned to the airport and attempted to land on a dolly landing platform. The pilot stated that he landed off-center on the platform, then attempted to back out and straighten the helicopter. The helicopter’s right skid got caught in the middle of the platform, and the helicopter rolled right and experienced a dynamic rollover, which resulted in substantial damage. The pilot reported that there were no preaccident mechanical malfunctions or failures of the helicopter that would have precluded normal operation.
- Probable Cause: The pilot’s improper landing technique that allowed the helicopter’s right skid to get caught on the landing platform, which resulted in a dynamic rollover.
Landing gear not configured: Beechcraft B95A Travel Air, N755RP, accident occurred on December 19, 2024, at Murray-Calloway County Airport (CEY/KCEY), Murray, Kentucky
- Location: Murray, Kentucky
- Accident Number: ERA25LA083
- Date & Time: December 19, 2024, 15:50 Local
- Registration: N755RP
- Aircraft: Beech B95A
- Aircraft Damage: Substantial
- Defining Event: Landing gear not configured
- Injuries: 2 None
- Flight Conducted Under: Part 91: General aviation - Instructional
The pilot was completing his multi-engine checkride with a Designated Pilot Examiner (DPE). The DPE had configured the airplane for a simulated single-engine landing. The DPE recalled the pilot calling out an extension of the landing gear, but the pilot did not remember putting the landing gear down and nor verifying that it was extended. Neither pilot nor DPE recalled hearing the landing gear position warning horn before touchdown. The airplane touched down on the runway with the landing gear retracted and slid down the runway on the underside of the fuselage, substantially damaging it.
A postaccident examination of the landing gear system revealed that the landing gear position warning horn was functioning normally. Neither pilot reported that there were any preimpact mechanical malfunctions or failures with the airplane were reported that would have precluded normal operation.
- Probable Cause: The pilot’s failure to lower the landing gear before touchdown, which resulted in a gear-up landing. Contributing was the designated pilot examiner’s inadequate monitoring and lack of remedial action.
Robinson R22 Mariner, N178EP, accident occurred on November 13, 2025, near Parrottsville, Tennessee
- Location: Parrottsville, Tennessee
- Accident Number: ERA25LA046
- Date & Time: November 13, 2024, 11:30 Local
- Registration: N178EP
- Aircraft: ROBINSON HELICOPTER COMPANY R22 MARINER
- Aircraft Damage: Substantial
- Defining Event: Loss of control in flight
- Injuries: 1 Minor
- Flight Conducted Under: Part 91: General aviation - Instructional
https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?NNumberTxt=178EP
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/195496/pdf
https://data.ntsb.gov/Docket?ProjectID=195496
The student pilot of the helicopter stated she was flying on her first solo cross-county flight. She flew to the first destination airport, which was about 30 minutes away, and made three uneventful approaches to land before departing the airspace and fly to another airport and practice some more approaches. She stated that about 15 minutes out from the next airport, she was having problems getting the correct frequency dialed into the radio and the helicopter felt “light” on the controls. She further described that the engine was running normally and all engine controls were functioning as expected. She then decided to make a precautionary landing in a field. During landing, she was focused on the helicopter’s instruments, did not look outside at the ground, and did not notice the field was slopped. One of the helicopter’s skids contacted the ground with a sideways motion, and the helicopter began to spin. The tail rotor subsequently contacted the ground and the helicopter rolled over on its left side resulting in substantial damage to the tail rotor and tail boom. The pilot stated that there were no preimpact mechanical malfunctions or failures of the helicopter that would have precluded normal operation.
- Probable Cause: The pilot’s failure to maintain control of the helicopter during a precautionary, off-airport landing to sloping terrain.
AC/prop/rotor contact w person: Aero AT-4 LSA, N401G, accident occurred on October 25, 2024, at Mallory Airport (WV12), South Charleston, West Virginia
- Location: South Charleston, West Virginia
- Accident Number: ERA25LA032
- Date & Time: October 25, 2024, 11:30 Local
- Registration: N401G
- Aircraft: AERO SP Z O O AT-4 LSA
- Aircraft Damage: Minor
- Defining Event: AC/prop/rotor contact w person
- Injuries: 1 Serious, 2 None
- Flight Conducted Under: Part 91: General aviation - Instructional
At the conclusion of a short cross-country flight, the flight instructor and student pilot elected to a perform takeoff and landings at their destination airport. The airport was privately owned, the single asphalt runway was 1,900 ft-long by 24 ft-wide, and there was no taxiway parallel to the runway. The flight instructor stated that, he scanned the runway for obstructions and announced over the airport’s Common Traffic Advisory Frequency the airplane’s position in the traffic pattern and their intent to land. No obstructions were observed during the landing. As the pilots taxied the airplane down the recently-paved runway, a person wearing dark-colored clothing “suddenly” came into view. The person was walking along the runway with his back toward the approaching airplane. The airplane’s left wingtip contacted the pedestrian and knocked him forcefully to the ground, resulting in serious injuries. The airplane’s wingtip incurred minor damage. The flight instructor then stopped the airplane, and he and the student rendered aid to the pedestrian until emergency responders arrived. The flight instructor reported that the pedestrian typically carried a hand-held radio that he would use to listen for traffic calls, but he was not carrying it with him on the day of the accident.
- Probable Cause: The pedestrian’s inadequate visual lookout while walking next to an active runway, which resulted in the airplane striking him during taxi.
Cessna S550 Citation S/II, N666DS, fatal accident occurred on May 22, 2025, near Montgomery-Gibbs Executive Airport (MYF/KMYF), San Diego, California
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.
- Location: San Diego, CA
- Accident Number: WPR25FA161
- Date & Time: May 22, 2025, 03:47 Local
- Registration: N666DS
- Aircraft: Cessna S550
- Injuries: 6 Fatal, 8 Minor
- Flight Conducted Under: Part 91: General aviation - Business
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200192/pdf
https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N666DS
Daviator LLC
On May 22, 2025, at 0347 Pacific daylight time (PDT), a Cessna Citation S550, N666DS, was destroyed when it was involved in an accident near San Diego, California. The pilot and five passengers were fatally injured. Eight people on the ground received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
The airplane departed Teterboro Airport (TEB), Teterboro, New Jersey, on May 21, about 2309 eastern daylight time (2009 PDT) and arrived at Colonel James Jabara Airport (AAO), Wichita, Kansas, about 0148 central daylight time (2348 PDT). The airplane was refueled with 548 gallons of Jet-A fuel before departing about 0236 central daylight time (0036 PDT) with a destination of Montgomery-Gibbs Executive Airport (MYF), San Diego, California. MYF is a tower-controlled airport between the hours of 0700 and 1800 and operates as an uncontrolled airport during the remaining hours of the day.
As the airplane neared MYF, the pilot checked in on frequency with the Southern California Terminal Radar Approach Control (SOCAL TRACON) controller while at 17,000 ft mean sea level (msl). The controller informed the pilot that the Automated Surface Observing System (ASOS) at MYF was out of service and the pilot acknowledged that he was aware of that. The controller asked the pilot what approach he would like to fly into MYF and the pilot responded that he would like to fly the RNAV (GPS) instrument approach to runway 28R. The pilot did not specify whether he would fly the localizer performance with vertical guidance (LPV) approach or the lateral navigation (LNAV) approach. The pilot was then cleared direct to the NESTY approach fix and instructed to descend to 9,000 ft. The pilot subsequently asked the controller if they could assist in determining the weather conditions at MYF. The controller provided the pilot the weather conditions at Marine Corp Air Station Miramar (NKS), located about 4 miles north of MYF, which was briefed as wind calm, ½ mile visibility, and an indefinite 200 ft ceiling.
The pilot then discussed alternate airport weather conditions with the controller in the event he had to perform a missed approach. He stated he would notify SoCal TRACON of his selection of an alternate airport, but did not do so during the remainder of the flight.
When the airplane was about 10 mi northeast of NESTY, the controller asked the pilot if he was going to “make your descent” and asked if he would like vectors to the south. The pilot replied, “I think we’ll be alright.” The airplane was at about 8,000 ft msl and 270 knots ground speed at that time. The controller informed the pilot that he was 5 miles from NESTY and instructed them to cross NESTY at or above 3,800 ft msl, and that he was cleared the RNAV approach to runway 28R at MYF, which the pilot acknowledged.
ADS-B data showed the airplane subsequently turned abeam NESTY at about 3,750 ft msl and a ground speed of 200 knots, or 191 knots calibrated airspeed (KCAS). The airplane continued to slow and descend and as it crossed PENYY, the final approach fix, at 0344:50 and about an altitude of 2,450 ft msl and ground speed of about 175 knots (167 KCAS).
The pilot made a position call on the MYF common traffic advisory frequency that he was at 3 miles on the approach, followed by the sound of the microphone button being keyed 7 times, consistent with an attempt to activate the pilot-controlled runway lighting.
The airplane crossed PALOS, located 2.9 nm from the runway 28R displaced threshold, at 0346:12, at an altitude of about 1,190 ft msl, and ground speed of about 120 knots (117 KCAS). PALOS has a published minimum crossing altitude at or above 1,380 ft msl. The airplane continued to descend until the ADS-B data ended at 0346:47, at an altitude of about 464 ft msl (about 60 ft agl).
The first identified point of contact (FIPC) was damaged power transmission lines about 90-95 ft above the ground (about 500 ft msl), located about 1.8 nm from the runway 28R displaced threshold. Portions of the left horizontal stabilizer, left elevator, and the vertical stabilizer were located about 200 ft downrange of the lines. The debris field was about 1,200 ft in length and on a magnetic heading of about 300° from the FIPC. The debris field spanned brush-covered terrain and a residential neighborhood.
The main wreckage, which consisted of thermally damaged remnants of the cabin, engines, and left wing, were located on a residential street about 1.6 nm from the runway 28R displaced threshold. The airplane impacted one residential structure and 20 vehicles, which were damaged or destroyed by impact or post impact fire. The wreckage was moved to a secure location for additional examination.
A cockpit voice recorder (CVR) was recovered from the wreckage and was sent to the NTSB Vehicle Recorders Laboratory for examination and audio extraction. The left and right engine Full Authority Digital Engine Control (FADEC) units were recovered and retained for data download. The airplane was not equipped with a flight data recorder (FDR).
The RNAV (GPS) RWY 28 approach allowed for instrument approaches for Category A and B aircraft only (figure 1).
The Flight Standardization Board Report, Rev.2, for the CE-500 series airplanes states:
“13.2 Aircraft Approach Category. The CE-500 Series aircraft are considered a Category B aircraft for the purposes of determining the appropriate instrument approach procedure category in accordance with § 97.3.”
There was a notice to airmen (NOTAM) in effect at the time of the accident informing pilots that the Runway Alignment Indicator (RAI) lights were out of service at MYF and had been so since March 28, 2022. The repairs of the affected RAI lighting components and replacement of the light system have been delayed awaiting completion of an environmental study. All other runway lighting was operable at the time of the accident.
The pilot was based at MYF and underwent a flight evaluation and received an exemption to fly the Cessna S550 single-pilot on December 15, 2024.
Mooney M20TN Acclaim, N242RE, fatal accident occurred on April 26, 2025, near Sparta-Upper Cumberland Regional Airport (SRB/KSRB), Sparta, Tennessee
- Location: Sparta, TN
- Accident Number: ERA25FA187
- Date & Time: April 26, 2025, 11:47 Local
- Registration: N242RE
- Aircraft: Mooney M20TN
- Injuries: 3 Fatal
- Flight Conducted Under: Part 91: General aviation - Personal
Lancair 360, N77LH, accident occurred on June 11, 2025, at Fort Stockton–Pecos County Airport (FST/KFST), Fort Stockton, Texas
- Location: Fort Stockton, TX
- Accident Number: CEN25LA205
- Date & Time: June 11, 2025, 21:45 Local
- Registration: N77LH
- Aircraft: Lancair 360
- Injuries: 1 None
- Flight Conducted Under: Part 91: General aviation - Personal
On June 11, 2025, about 2145 central daylight time, a Lancair 360 airplane, N77LH, was destroyed when it was involved in an accident near Fort Stockton, Texas. The airline transport pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
According to the pilot, he had recently purchased the airplane in California, and he was performing a cross-country flight to his home base in Florida. The airplane stopped at the El Paso International Airport (ELP), El Paso, Texas to refuel. The airplane departed from ELP about 1940 mountain daylight time. While enroute to the San Antonio International Airport, San Antonio, Texas, the pilot smelled smoke in the cockpit. The pilot contacted air traffic control and changed his destination airport to the Fort Stockton-Pecos County Airport, Fort Stockton, Texas, due to the emergency. Once the pilot maneuvered the airplane for landing on runway 12, the cockpit was filled with smoke, and flames were emitting from underneath the instrument panel.
During the landing, the pilot reported he did not have brake authority, and the airplane departed the runway to the left. The airplane came to rest upright against a barbed wire fence along the airport perimeter. The pilot was able to egress from the airplane without further incident.
The fire consumed the engine compartment, part of the fuselage, and the left wing. The wreckage was recovered from the accident site, and it was transported to a secure location for future examination.
The experimental airplane was built from a kit in 1999. The composite construction airplane was equipped with a Lycoming Engines O-360-A1A reciprocating engine. The airplane had a condition inspection performed by a mechanic on the airframe and the engine on June 9, 2025. During the inspection, it was noted that the airframe had accumulated 440.4 hours total time, and the engine had accumulated 2,220.9 hours total time (with 911.9 hours since overhaul).
The pilot reported that the airplane maintenance records and the historical airplane build records were stored in the baggage compartment and consumed by the fire.
Rans S-20 Raven, N327KM, accident occurred on May 27, 2025, near Fairfield, Utah
- Location: Fairfield, UT
- Accident Number: WPR25LA163
- Date & Time: May 27, 2025, 13:30 Local
- Registration: N327KM
- Aircraft: RANS S20
- Injuries: 1 None
- Flight Conducted Under: Part 91: General aviation - Personal
https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N327KM
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200237/pdf
On May 27, 2025, about 1330 mountain daylight time, an experimental amateur-built RANS S20 Raven, N327KM, was substantially damaged when it was involved in an accident near Fairfield, Utah. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.
The pilot reported that shortly after departing the runway at the West Desert Airpark (UT9), Fairfield, Utah, about 800 ft above ground level, the airplane had a total loss of engine power followed by an error message on the multi function display. The pilot attempted to restart the engine but was unsuccessful, and initiated a forced landing on a field. The airplane landed hard on a vegetated field and sustained substantial damage to the fuselage.
The airplane was recovered to a secure location for further examination