Thursday, July 31, 2025

Piper PA-28-180 Cherokee, N8375W, fatal accident occurred on July 13, 2025, at Needles Airport (EED/KEED), Needles, California

  • Location: Needles, CA
  • Accident Number: WPR25FA208
  • Date & Time: July 13, 2025, 21:28 Local
  • Registration: N8375W
  • Aircraft: Piper PA-28-180
  • Injuries: 2 Fatal
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200521/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N8375W

On July 13, 2025, about 2128 Pacific daylight time, a Piper PA-28-180, N8375W, was substantially damaged when it was involved in an accident near Needles, California. Both pilots sustained fatal injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The operator reported that the two pilots rented the airplane to accumulate flight hours. Preliminary ADS-B data provided by a commercially available third-party service showed the airplane depart North Las Vegas Airport (VGT), Las Vegas, Nevada, at 1934 and subsequently land at Needles Airport (EED), Needles, California about one hour later. The operator then received an emergency locator transmitter (ELT) alert about 2133. Local law-enforcement officers observed a fire at 2140 and subsequently located the main wreckage about 1,425 ft southwest from the departure end of runway 20.

The airplane came to rest inverted with thermal damage to the fuselage. The first identified point of contact (FIPC) was a ground scar about 225 ft north of the main wreckage, approximately 1,200 ft from the departure end of the runway. The debris path continued to the south with the propeller and hub assembly at the end of the debris path about 25 ft beyond the main wreckage. The total debris path spanned about 250 ft from the FIPC to the propeller. All major airplane components and control surfaces were located and identified within the debris path.

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

Lancair IVP, N49BX, fatal accident occurred on July 30, 2025, near Indy South Greenwood Airport (HFY/KHFY), Greenwood, Indiana

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=N49BX


- Hitstory of Flight:
On July 30, 2025, at about 1046 local time, a Lancair IVP, N49BX, was substantially damaged when it impacted terrain shortly after takeoff from Indy South Greenwood Airport (HFY/KHFY), Greenwood, Indiana. The aircraft was registered to, and being operated by the airline transport pilot, who sustained fatal injuries. The Part 91 personal flight was originating at the time, and was destined to an unknown airport in Pennsylvania 
(at the time of this writing).

On July 27, 2025, the pilot departed Oshkosh-Wittman Field (OSH/KOSH), Oshkosh, Wisconsin, on a round-the-world solo trip. The airplane landed at Greenwood, and remained parked until the accident flight.

According to automatic dependent surveillance-broadcast (ADS-B) data, at 1045:34, the airplane was seen departing runway 19 at KHFY. The airplane was approximately 3600 ft down (the 5100 ft runway) and 150 ft to the left side of the runway over the grass and climbing at 98 knots groundspeed.

The airplane continued the shallow left climb. At 1045:54, the airplane was observed at 1000 ft, 111 knots groundspeed, but was now showing descending vertical climb rate. At 1045:58, the airplane entered an "aggressive" left hand turn, and was now showing a positive vertical climb rate and losing (ground) speed. At 1046:04, the airplane was observed at 1150 ft, 93 knots, and climbing 1300 fpm. At 1046:05, the airplane was at 1175 knots, 91 knots, and climbing 1800 fpm. At 1046:08, the airplane was observed at 1200 ft, 65 knots groundspeed, and descending -768 fpm. The last ADS-B data return was recorded at 1046:10, the airplane was at 1150 ft, 34 knots groundspeed, and descending -2800 fpm. (figure 1)
Figure 1: ADS-B Exchange Data with Google Earth

One witness stated that "The plane was kind of banking and they started to lower and then pulled up and started to roll, and I thought it’s like a sky show and they went straight into the ground.”

Another witness stated "She was banking hard left to go north, and all of the sudden, the nose dove and she went into a spin and just went straight down."

- Wreckage and Impact Information:
The airplane impacted a grassy ditch behind a gas station located about 0.70 mile from the departure end of runway 19. The main wreckage consisted of the entire airplane, which was orientated on a 300° magnetic heading. The wreckage was in an upright position, and there was a very small appreciable wreckage debris path. There was no post crash fire.

The engine remained partially attached to its engine mounts and the firewall. The propeller remained attached to the engine propeller flange. Two propeller blades remained attached to the hub assembly (the third blade was not visible in online photographs but was most likely somewhere in the path debris).

The left wing was impact damaged and destroyed during the accident. The outer right wing was impact damaged and separated, but a portion of the inner right wing remained attached to the fuselage. The fuselage (including the pilot/passenger cabin) remained intact. The tail was severed by impact forces.

The start of the debris path included parts from both wings and landing gear which lead to the main wreckage (figure 2). The impact appears consistent with a low altitude aerodynamic stall/spin with little to no forward speed.

Figure 2

- Pilot Info:
The certificated airline transport pilot, age 44, held an airline transport pilot certificate, with a rating for airplane multi-engine land aircraft (with a most recent issue/update date of issued on October 4, 2023)
. She held a commercial pilot certificate, with ratings for airplane single-engine land, single-engine sea, and instrument airplane. The pilot also held a flight instructor certificate, with ratings for airplane single-engine and mulit-engine, and instrument airplane, issued/updated on August 31, 2024. The pilot's first class FAA medical was issued on February 2025, with a note about wearing corrective lenses to meet vision standards at all required distances.

The pilot held a type rating in the Boeing 757 and Boeing 767 aircraft (subject to pilot-in-command limitations).

- Aircraft Info:
The accident aircraft, MSN LIV-465, was manufactured in 2005. It was a 4-seat, pressurized, low-wing airplane equipped with a retractable tricycle landing gear, electrically actuated wing flaps, and a single reciprocating engine with a constant speed propeller. The airframe was constructed of high temperature, epoxy prepreg, carbon fiber materials.

The airplane was equipped with a Continental TSIO-550-E engine which drove a three-bladed Hartzell propeller.

- Airport Information:
KHFY is a non-towered public airport located about 10 miles southeast of Indianapolis, Indiana. It features a single asphalt/grooved runway 1/19 which is 5102 x 75 ft. The airport elevation was 822 ft.

- Weather:
The nearest airport, KIND, reported the following conditions:

METAR KIND 301354Z 00000KT 10SM FEW010 BKN250 28/22 A3009 RMK AO2 SLP180 FU FEW010 T02780222

METAR KIND 301454Z 00000KT 10SM FEW030 SCT250 30/23 A3010 RMK AO2 SLP182 T03000228 53006

- Additional Information:
The pilot was the 10th woman to fly solo around the world.

Wednesday, July 30, 2025

Van's RV-14A, N21KL, fatal accident occurred on July 21, 2025, near Lowell City Airport (24C), Lowell, Michigan


https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200599/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N21KL

On July 21, 2025, about 1627 eastern daylight time, a Van’s Aircraft RV-14A airplane, N21KL, was destroyed when it was involved in an accident near Lowell, Michigan. The pilot and the pilot-rated passenger sustained fatal injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The purpose of the flight was for the pilot and the passenger to view N471NP (a Van’s Aircraft RV-6 airplane), that was for sale, at the Lowell City Airport (24C), Lowell, Michigan. The passenger was interested in potentially purchasing the airplane.

A preliminary review of ADS-B data showed that the pilot departed in the airplane at 1433 from his home base at the Alpena County Regional Airport (APN), Alpena, Michigan. The airplane landed at 1456 at the Oscoda/Wurtsmith Airport (OSC), Oscoda, Michigan, and the passenger boarded the airplane. The airplane departed from OSC at 1532 and flew southwest to 24C, which is a non-towered airport.

Upon approaching 24C, the airplane flew to the west of the Flat River. The ADS-B data showed that as the airplane flew over Lincoln Lake Road, it then turned to the south. Shortly after turning south, the airplane continued in a descending turn toward the east. The airplane impacted a storage unit building about 0.43 miles from the approach end of runway 12 at 24C.

When the airplane impacted the storage unit building, an explosion occurred. A postimpact fire consumed the wreckage and the storage unit building. The wreckage was recovered from the accident site, and it was transported to a secure location.

According to a witness, he and his son observed the airplane inflight while they were driving in a vehicle near 24C on Vergennes Street. While the airplane was in the descending turn and prior to impact, they did not observe any smoke or flames emitting from the airplane, nor did they hear any abnormal engine noises such as sputtering or backfiring.

The two-seat experimental airplane was built from a kit in 2024 by the pilot, who in addition to holding a private pilot certificate (airplane single engine land), he also held a repairman certificate (experimental aircraft builder for the accident airplane). The passenger held a private pilot certificate (airplane single engine land) and an airframe and powerplant mechanic certificate.

The airplane was equipped with a Lycoming Engines YIO-390-EXP248 reciprocating engine, part of the Thunderbolt experimental engine series. The airplane was also equipped with a Whirlwind Propellers 300-3B/A-72 three-blade controllable pitch composite propeller.

A preliminary review of meteorological data for the accident location and time did not reveal any meteorological areas of concern. The calculated density altitude for the closest meteorological reporting station was 2,266 ft.

Cessna T210N Turbo Centurion, N93HP, accident occurred on July 21, 2025, near Crosby, Texas


  • Location: Crosby, TX
  • Accident Number: CEN25LA282
  • Date & Time: July 21, 2025, 07:45 Local
  • Registration: N93HP
  • Aircraft: Cessna T210N
  • Injuries: 2 None
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200615/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N93HP

On July 21, 2025, about 0745 central daylight time, a Cessna T210N, N93HP, was substantially damaged when it was involved in an accident near Crosby, Texas. The pilot and passenger were not injured. The airplane operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane departed from the George Bush Intercontinental Airport (IAH), Houston, Texas, at 0734 for the Dunham Field Airport (1XS1), Crosby, Texas. The pilot reported that after departure, the airplane began losing fuel. Shortly after, the engine began to lose power, and the No. 5 cylinder showed low exhaust gas and cylinder head temperatures. The pilot then elected to perform an off-field landing.

During the off-field landing, the airplane impacted a water retention pond. A postimpact fire ensured consuming portions of the engine cowling and fuselage. The pilot and passenger were able to egress without injuries.

The airplane was retained for further examination.

Beechcraft A36 Bonanza, N41VH, accident occurred on July 8, 2025, at Cavanaugh Bay Airport (66S), Coolin, Idaho

  • Location: Coolin, ID
  • Accident Number: WPR25LA204
  • Date & Time: July 8, 2025, 18:40 Local
  • Registration: N41VH
  • Aircraft: Beech A36
  • Injuries: 2 Minor
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200487/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N41VH

On July 8, 2025, about 1840 Pacific daylight time, a Beech A36, N41VH, was substantially damaged when it was involved in an accident near Coolin, Idaho. The pilot and passenger sustained minor injuries. The airplane was operated under Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, while departing from Cavanaugh Bay Airport (66S) Coolin, Idaho, the right wing contacted a tree at the end of the runway, and the airplane rolled over and came to rest in a lake located just off the end of the runway. The airplane sustained substantial damage to the fuselage and wings.

Witnesses to the accident reported they heard the engine running at a “high RPM” and saw the airplane make a steep right bank on the departure end of the runway before the right wing struck trees. Density altitude at the time of the accident was calculated to be about 5,267 ft.

The wreckage was retained for further examination. 

Lancair 360, N360RF, fatal accident occurred on June 29, 2023, at Ottawa Executive Airport (Z98), Zeeland, Michigan

  • Location: Zeeland, MI 
  • Accident Number: ERA25FA248 
  • Date & Time: June 29, 2025, 10:49 Local 
  • Registration: N360RF 
  • Aircraft: ROBERT FIDLER LANCAIR 320/360 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200409/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N360RF

On June 29, 2025, at 10:49 eastern daylight time, an experimental, amateur-built Lancair 360, N360RF, was destroyed when it was involved in an accident near Zeeland, Michigan. The private pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to a witness, the pilot taxied to the fuel service station and added fuel to the airplane just prior to the accident flight. After fueling, the airplane was seen taking off from runway 20. Shortly after rotation, the airplane began to roll to the left, and the roll continued until the airplane was in a steep bank angle. Subsequently, the nose pitched down, and the airplane impacted terrain to the east of the runway; a postaccident fire ensued.

The initial impact point was approximately 100 ft east of the runway centerline. A crater that was approximately 12 ft from the initial impact point contained the propeller, starter ring gear support, and multiple pieces of plexiglass and composite material. The main wreckage location was about 40 ft from the initial impact point and contained the engine, cockpit, fuselage, both wings, and the empennage. A post-impact fire consumed most of the airframe, and the engine displayed heavy thermal damage. All of the major airplane components were located at the accident site.

The airframe was mostly consumed by the post-impact fire, and displayed impact damage signatures. Flight control continuity for the rudder was established from the rudder bellcrank to the rudder pedal attach brackets for both the left and right rudder controls. One of the left rudder cables was noted to have an unsecured Nicopress compression sleeve. At the time of the examination, the compression sleeve was approximately 5 inches from the rudder pedal attach bracket for the left rudder cable. The compression sleeve showed no signs of being compressed to secure it to the rudder cable.

The right aileron remained attached to its installation point and was thermally damaged. The right aileron control tube that attached the aileron to the bellcrank remained intact and was secured to both the aileron and the bellcrank. The right aileron bellcrank remained intact and was capable of normal movement. The control tube that attached the aileron bellcrank to the idler bellcrank was thermally damaged at the idler bellcrank; however, the rod end remained attached to the idler bellcrank and the bolt, washer, and nut remained secured to the rod end. The right idler bellcrank was thermally damaged and was partially melted. The control tube going from the idler bellcrank to the controls in the cockpit was thermally damaged and was mostly destroyed. The rod end that was attached to the idler bellcrank was located near the idler bellcrank location, and the bolt, washer, and nut remained secured to the rod end. The control tube rod end that was attached to the cockpit controls remained secured to its installation point.

The left aileron remained attached to its installation point and was thermally damaged. All the aluminum portions of the left aileron control tubes and bellcranks were thermally destroyed; however, all of the control tube rod ends remained. The left aileron control tube rod end that attached to the aileron remained secured to the aileron, and the control tube rod end that attached to the cockpit controls remained secured to its installation point. The other four rod ends were located at their respective destroyed bellcrank locations, and each rod end still contained the attaching bolt, washer and nut.

Both elevators remained attached to the elevator bellcrank and displayed thermal damage signatures. The elevator control rod going from the elevator bellcrank to the idler bellcrank remained attached to the elevator bellcrank, the control tube was thermally damaged near the idler bellcrank and was melted; however, the elevator control tube rod end was located and contained the bolt, washer, and nut. The idler bellcrank was destroyed by the postaccident fire and only the support remained. The elevator control tube going from the idler bellcrank to the control sticks torque tube was completely melted except for the two rod ends. The rod end that was attached to the idler bellcrank was found near the idler bellcrank support and the rod end bolt, washer, and nut remained secure. The other rod end for the elevator control tube remained secured to the control torque tube.

Both flaps were thermally damaged, the attachment hinges were melted, and the flaps were separated from the airframe, being found adjacent to their original installation points. The flap torque tube was thermally damaged, and the flap actuator bellcrank was destroyed. Both flap actuating rods remained attached to the torque tube, and the other ends still had the bolts and nutplates attached to the rod ends. 

The engine remained attached to the airframe through its mounts, cables, wires, and hoses. The engine was thermally damaged from the postaccident fire. The crankcase was intact, and there were no visible signs of a catastrophic internal engine failure. The propeller flange was impact-separated from the rest of the crankshaft and remained attached to the propeller. The top spark plugs were removed and the electrodes displayed normal wear and operating signatures. 

The propeller was located in the crater near the initial impact point and was mostly buried in the soil. Both propeller blades remained within the propeller hub and could not be moved. The propeller blades were marked with “A” and “B” for documentation purposes during the postaccident examination. The propeller blade marked “A” displayed leading edge gouging, chordwise scratches, and minor twisting deformation. The propeller blade marked “B” displayed leading edge gouging, chordwise scratches, and minor aft bending and twisting deformation. The wreckage was retained for further examination.

Cessna 182Q Skylane, N4953N, accident occurred on June 26, 2025, at Brantley County Airport (4J1), Nahunta, Georgia

  • Location: Nahunta, GA 
  • Accident Number: ERA25LA242 
  • Date & Time: June 26, 2025, 09:30 Local 
  • Registration: N4953N 
  • Aircraft: Cessna 182Q 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200393/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N4953N

On June 26, 2025, at about 09:30 eastern daylight time, a Cessna 182Q, N4953N, was substantially damaged when it was involved in an accident near Nahunta, Georgia. The private pilot was uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, the airplane had just undergone extensive maintenance in Sylacauga, Alabama, and he was planning to take the airplane to the W H 'Bud' Barron Airport (DBN), Dublin, Georgia. The pilot stopped at the Brantley County Airport (4J1), Nahunta, Georgia, on June 24, 2025, and the airplane remained parked until the day of the accident. The pilot reported that he performed a preflight inspection followed by a normal start of the engine. He allowed the engine to warm up and performed a magneto drop and propeller governor check. Shortly thereafter, a fire suddenly came up from the floor around the rudder pedals. The pilot exited the airplane and unsuccessfully attempted to extinguish the fire with a handheld fire extinguisher. The fire consumed most of the fuselage and the right wing, and the left wing was thermally damaged at the wing root.

The wreckage was retained for further examination.