Thursday, July 31, 2025

Loss of control in flight: Bell UH-1H Iroquois, N567VF, fatal accident occurred on July 31, 2023, near Oakdale, Illinois

  • Location: Oakdale, Illinois 
  • Accident Number: CEN23FA340 
  • Date & Time: July 31, 2023, 13:11 Local 
  • Registration: N567VF 
  • Aircraft: RICHARDS HEAVYLIFT HELO INC UH-1H 
  • Aircraft Damage: Substantial 
  • Defining Event: Loss of control in flight 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 137: Agricultural
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/192758/pdf

https://data.ntsb.gov/Docket?ProjectID=192758

On July 31, 2023, about 1311 central daylight time (CDT), a Richard’s Heavylift Helo UH-1H helicopter, N567VF, was substantially damaged when it was involved in an accident near Oakdale, Illinois. The pilot was fatally injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

The pilot was flying an aerial application flight in a pattern consisting of north-south passes starting on the western edge of the field with turns to the east to work the field. ADS-B and onboard GPS devices that recorded the accident flight showed that before the accident, for undetermined reasons, the helicopter turned to the west, descended, and impacted terrain

An examination of the helicopter and its engine did not detect any preimpact anomalies that would have contributed to a loss of control. A visual examination of the nearby power lines did not show evidence of arcing or damage to the lines or power pole.

The pilot’s severe coronary artery disease increased his risk of experiencing a sudden impairing or incapacitating cardiac event, such as arrhythmia, chest pain, or heart attack. The autopsy does not provide evidence that such an event occurred; however, such an event does not leave reliable autopsy evidence if it occurs shortly before death. Even severe coronary artery disease may not cause major symptoms.

Toxicology results indicate that the pilot had used the medication cetirizine. The cetirizine levels in his cavity blood and tissue indicate a possibility that the pilot may have been experiencing some associated impairing effects, such as mild sedation, at the time of the accident. However, it is also possible that the pilot was not experiencing any impairing effects of his cetirizine use.

- Probable Cause: An in-flight loss of control for undetermined reasons.

Loss of visual reference: Cessna 172G Skyhawk, N3992L, fatal accident occurred on December 16, 2023, near Independence State Airport (7S5), Independence, Oregon

  • Location: Independence, Oregon 
  • Accident Number: WPR24FA057 
  • Date & Time: December 16, 2023, 16:54 Local 
  • Registration: N3992L 
  • Aircraft: Cessna 172G 
  • Aircraft Damage: Destroyed 
  • Defining Event: Loss of visual reference 
  • Injuries: 3 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/193533/pdf

https://data.ntsb.gov/Docket?ProjectID=193533

On December 16, 2023, about 1654 Pacific standard time, a Cessna 172G airplane, N3992L, was substantially damaged when it was involved in an accident near Independence, Oregon. The pilot and the two pilot-rated passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot and two pilot-rated passengers were returning to their home airport after they were advised by the pilot's flight instructor not to return due to dense fog that reduced visibility to about 500 ft. During their arrival, the pilot made multiple advisory radio calls that confirmed his intention to land and activated the pilot-controlled runway lights (PCL). Recorded ADS-B data showed that while on the downwind leg, after passing the runway lights,  the airplane veered toward  the runway centerline as it continued the downwind leg. The pilot then performed a 180° base to final turn and overshot the runway centerline twice. The airplane then flew past the runway threshold and off to the side of the runway, where it impacted a power distribution line support pole about 694 ft from the approach end of the runway threshold. A postaccident fire substantially damaged the airplane.

Postaccident examination of the airframe and engine revealed no mechanical malfunctions of failures that would have precluded normal operation. A weather study confirmed that instrument meteorological conditions (IMC) prevailed about the time of the airplane's arrival. The pilot likely lost his ability to maintain visual reference through the fog during the landing approach.

- Probable Cause: The pilot's decision to continue flight under visual flight rules into instrument meteorological conditions, which resulted in collision with an obstacle while landing.

Loss of control in flight: Kubicek BB85Z, N4961D, fatal accident occurred on January 14, 2024, near Eloy, Arizona

  • Location: Eloy, Arizona
  • Accident Number: WPR24FA072
  • Date & Time: January 14, 2024, 07:47 Local
  • Registration: N4961D
  • Aircraft: Kubicek BB85Z
  • Aircraft Damage: Substantial
  • Defining Event: Loss of control in flight
  • Injuries: 4 Fatal, 1 Serious, 8 None
  • Flight Conducted Under: Part 91: General aviation - Other work use
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/193647/pdf

https://data.ntsb.gov/Docket?ProjectID=193647

On January 14, 2024, about 0747 mountain standard time, a Kubicek BB85Z balloon, N4961D, was involved in an accident near Eloy, Arizona. The pilot and three passengers were fatally injured, and one passenger sustained serious injuries. The balloon was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 sightseeing passenger and skydiving (commercial) flight.

The balloon departed with the pilot, eight skydivers, and four passengers on a sightseeing passenger and skydiving (commercial) flight. Interviews with the skydivers revealed that after about 35 minutes, the balloon reached an altitude of about 10,000 ft mean sea level (msl) and all 8 skydivers departed from the basket in 4 groups numbering 3, 2, 1 and 2 jumpers, respectively. The four passengers and pilot remained in the basket. After the jumpers exited the basket, the pilot pulled the red rapid deflation valve line 12 times to open the rapid deflation valve. This action resulted in a rapid loss of air that deformed the envelope, causing the deflation system's control lines to drop in and around the basket, which pinched the Red-White line in the flying cables. About 46 seconds later, the pilot attempted to add hot air to the envelope and attempted to close the rapid deflation valve but, was unsuccessful. During the descent the envelope continued to deflate until it was in a streamer-type configuration. Additionally, at times a burner flame under the deflated envelope was observed, as the pilot attempted to inflate the balloon envelope. The balloon continued to descend until it impacted the terrain.

Witnesses saw the balloon descending toward the ground. A review of multiple mobile phone videos revealed that the balloon was descending with the envelope deflated and trailing above the basket. 

Postaccident examination of the balloon did not reveal any preimpact anomalies that would have precluded normal operation. According to the balloon flight manual, the rapid deflation system was designed for fast and efficient deflation of the envelope during landing below 6.5 ft above ground level to prevent the basket from being dragged in windy conditions. If the pilot had used the parachute valve to manage the descent, he likely would have been able to land the balloon without injuries. Several online videos showed the pilot using the rapid deflation system while at high altitudes in other flights, indicating that that this was a common practice for him.

- Probable Cause: The pilot's decision to open the rapid deflation valve during flight as a means of descending, which resulted in the deflation of the envelope and hard impact with terrain.

Fuel exhaustion: Cessna 150M, N6266K, accident occurred on November 18, 2023, near Woodland, Washington

  • Location: Woodland, Washington
  • Accident Number: WPR24LA039
  • Date & Time: November 18, 2023, 15:22 Local
  • Registration: N6266K
  • Aircraft: Cessna 150M
  • Aircraft Damage: Substantial
  • Defining Event: Fuel exhaustion
  • Injuries: 2 None
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/193408/pdf

https://data.ntsb.gov/Docket?ProjectID=193408 

On November 18, 2023, about 1522 Pacific standard time, a Cessna 150M, N6266K, was substantially damaged when it was involved in an accident near Woodland, Washington. The flight instructor and student pilot sustained no injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The student pilot used a fuel dipstick ruler to measure the quantity of fuel in each wing tank and reported 13 and 9 gallons, respectively, during the preflight. Shortly after, the student and the flight instructor departed the local airport to practice steep turns and slow-flight maneuvers, including an introduction to power-off stalls and recovery. About an hour into the flight, during a stall maneuver recovery (with carburetor heat on), the instructor increased the throttle setting but the engine remained at idle. As the power remained unchanged, the instructor decided to execute an off-airport landing to a nearby field. Shortly after touchdown, the landing gear separated and the airplane nosed over, resulting in substantial damage to the aft fuselage.

Postaccident examination of the airframe and engine did not reveal any mechanical anomalies. Flight control and valvetrain continuity were established. No fuel was recovered at the accident site. The fuel system was traced from each wing tank to the carburetor at the engine through the fuel selector, which rotated normally and was unobstructed. The fuel filter bowl remained secured to its mount and had about 2 oz of fuel consistent with 100LL avgas.

Although weather conditions were conducive to serious carburetor icing at cruise power, the flight instructor reported that carburetor heat was applied during the stall maneuvers. The operator reported that the airplane was not refueled after the previous flight or before the accident flight. Based on the engine time that accrued since the last fueling, and the minimal amount of fuel found in the airplane after the accident, the student pilot’s fuel reading was likely incorrect and did not accurately account for the amount of fuel available for the flight.

As a result of the accident, the operator updated their procedures requiring all flight instructors to verify and sign off on the reported fuel level after each student preflight.

- Probeble Cause: The flight instructor’s inadequate preflight planning, which resulted in fuel exhaustion and a total loss of engine power.

Bell 206L-1 LongRanger II, N2611, fatal accident occurred on July 23, 2025, near Thibodaux, Louisiana

  • Location: Thibodaux, LA 
  • Accident Number: CEN25FA281 
  • Date & Time: July 23, 2025, 06:30 Local 
  • Registration: N2611 
  • Aircraft: BELL HELICOPTER TEXTRON 206L-1 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 137: Agricultural

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200614/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N2611

On July 23, 2025, about 0630 central daylight time, a Bell 206L-1 helicopter, N2611, was destroyed when it was involved in an accident near Thibodaux, Louisiana. The pilot was fatally injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 137 agricultural application flight.

The operator reported the accident occurred during the first flight of the day while the pilot was applying pesticide to a sugar cane field. The field was oriented northeast-southwest (030° - 210°), and the crop was about 6 to 8 ft high. A tree line bordered the west edge of the field. Fields immediately east, north, and northeast of the field being sprayed were fallow.

A set of powerlines was located about 180 ft from the north edge of the field being sprayed.

 The lines consisted of three transmission and two static lines. The static lines were about 85 ft above ground level (agl) at the supporting H-frames. The south static line was broken during the accident sequence.

The fuselage came to rest lying on its left side, oriented on an approximate 115° heading, about 60 ft north of the south static line. The right landing skid forward of the attachment strut was separated and located about 70 ft south of the static line. The upper surface of the separated skid exhibited repetitive abrasion marks consistent with contact to a powerline. The fracture surface appeared consistent with an overstress failure.

The engine and main rotor transmission remained securely attached to the airframe. The engine exhibited impact related damage to the left side but appeared otherwise intact. The main rotor mast was fractured at the transmission housing. The fracture surface appeared consistent with overstress. The separated portion of the mast with the rotor hub and inboard segments of the main rotor blades attached was lying adjacent to the fuselage. The outboard segments of both main rotor blades with the blade tips intact were located about 50 ft north of the fuselage.

The tailboom was separated at the aft fuselage and fragmented. The aft 6-foot section of the tailboom was positioned about 110 ft northeast of the fuselage. The tail rotor blades and transmission remained attached and were intact. A 5-foot section of the tailboom with the horizontal stabilizers attached was located about 150 ft east of the fuselage.

An AgNav unit has been retained for further examination and download.

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.

Tuesday, July 29, 2025

Van's RV-10, N847CS, fatal accident occurred on June 28, 2025, near Capron, Illinois

  • Location: Capron, IL
  • Accident Number: CEN25FA224 
  • Date & Time: June 28, 2025, 09:34 Local
  • Registration: N847CS 
  • Aircraft: Vans RV-10 
  • Injuries: 2 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Instructional 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200406/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N847CS

On June 28, 2025, about 0934 central daylight time, a Vans RV-10 airplane, N847CS, was substantially damaged during an accident near Capron, Illinois. The pilot and flight instructor were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 instructional flight.

The purpose of the flight was for the pilot to complete a flight review with the flight instructor. According to automatic dependent surveillance-broadcast (ADS-B) flight data, at 0909:06, the airplane departed runway 23 at Waukegan National Airport (UGN), Waukegan, Illinois. After takeoff, the airplane flew to the west and climbed to about 3,300 ft mean sea level (msl) where the flight track was consistent with maneuvers that are often associated with flight reviews. 

After the maneuvers, the airplane continued flying to the west until 0931:53, when it entered a right descending turn from about 3,000 ft msl. The airplane completed two 360° turns, over a period of 1 minute 40 seconds, as it continued to descend. Beginning at 0933:33, the airplane briefly flew northwest about 0.3 nautical miles (nm) while it continued to descend. About 13 seconds later, the airplane flew over Capron Road, a north-south road, about 590 ft above ground level (agl) before it entered a right turn to the east and continued to descend. At 0934:03, the airplane crossed over Capron Road for a second time, on an east heading. As of the final ADS-B data return at 0934:05, the airplane was about 315 ft agl and 154 ft west of the accident site. Preliminary aircraft performance calculations indicated that as of the final ADS-B return, the airplane had decelerated to about 54 knots calibrated airspeed (KCAS) and was descending about 2,850 feet per minute (fpm).

There were no witnesses to the accident. The airplane impacted a cornfield on a west heading. The corn damage was generally circular with a diameter consistent with the airplane’s wingspan. Based on the impact crater and the minimal lateral damage to the corn, the airplane impacted the ground while in a steep nose-down pitch attitude.

All structural components and flight control surfaces were located at the accident site. Elevator and aileron flight control continuity could not be confirmed due to impact-related damage; however, all observed separations to the flight control push/pull tubes and rod end bearings were consistent with overstress. Rudder cable continuity was confirmed from the cockpit pedals to the rudder control horn. Each flap remained attached to its respective wing; however, due to impact-related damage the flap setting was not determined during the onsite examination.

Both wing fuel tanks ruptured during impact, but there was evidence of fuel blight observed on the corn leaves surrounding the accident site. The airframe fuel lines were also damaged during impact, but residual fuel was observed at the fuel selector and the fuel line between the engine-driven fuel pump and the fuel servo. The engine-driven fuel pump discharged fuel when operated by hand. The fuel servo’s inlet fuel screen was not contaminated with debris and remained wet with residual fuel. The fuel flow transducer separated from the engine but was otherwise undamaged, and blown air passed through the fuel flow transducer without restriction.

The engine was found partially buried in the impact crater. A visual examination of the engine did not reveal any crankcase or cylinder fractures. Internal engine and valve train continuity was confirmed as the engine crankshaft was rotated through the propeller governor drive gear. The engine rear accessory gear section rotated freely. Compression and suction were noted on all six cylinders in conjunction with crankshaft rotation. An unquantified amount of engine oil remained in sump. The screw-on oil filter was found separated from the rear accessory section. The engine was equipped with two electronic magnetos that were not tested during the onsite examination. The top sparkplugs exhibited features consistent with normal engine operation. The fuel distribution valve and associated fuel injector lines exhibited impact-related damage. The fuel injectors were found attached to their respective fuel injector line, and each fuel injector was found properly installed in its respective cylinder head. The fuel injectors were clear of debris. The fuel servo exhibited significant impact-related damage. The engine examination revealed no evidence of a mechanical malfunction or failure that would have precluded normal operation.

The two-blade propeller remained attached to the engine crankshaft. One of the two propeller blades was found completely buried in the soil; however, when recovered the propeller blade exhibited an S-shaped spanwise bend, chordwise scratches, burnishing, and leading-edge damage. The other propeller blade remained relatively straight and exhibited minor chordwise scratches.

The airplane’s damaged primary flight display (PFD), multifunction display (MFD), electronic attitude indicator, and digital navigation/communication device were shipped to the NTSB Vehicle Recorder Laboratory for examination and possible data extraction. The airplane wreckage was recovered from the accident site to a secure location.

Rans S-7S Courier, N69TY, accident occurred on July 12, 2025, near Blackfoot, Idaho

  • Location: Blackfoot, ID 
  • Accident Number: WPR25LA210 
  • Date & Time: July 12, 2025, 20:15 Local 
  • Registration: N69TY 
  • Aircraft: HIBBARD RICK RANS S7 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200414/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N69TY

On July 12, 2025, about 2015 mountain daylight time, an experimental amateur-built Rans S7 airplane, N69TY, was substantially damaged when it was involved in an accident near Blackfoot, Idaho. 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 after flying for about 45 minutes and completing a 75-mile loop covering his farm property, he was headed home when the engine popped and started to vibrate. He continued to run the engine at reduced power and subsequently observed the oil pressure drop to 0 psi at which time the engine stopped producing power. He initiated a forced landing to a wheat field. During landing the airplane nosed over and sustained substantial damage to the rudder.

During the recovery of the airplane the lower fuselage was covered in oil and the engine crankcase and one of the engines cylinders were damaged.

The pilot reported that at the time of the accident the engine had accrued about 959 hours of operation and 13 hours since the last inspection on March 8, 2025.

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

Beechcraft 95-B55 Baron, N9420Y, accident occurred on June 29, 2025, near Eustis-Mid-Florida Airport (X55), Mount Dora, Florida


  • Location: Mount Dora, FL 
  • Accident Number: ERA25LA250 
  • Date & Time: June 29, 2025, 11:07 Local 
  • Registration: N9420Y 
  • Aircraft: Beech 95-B55 (T42A) 
  • Injuries: 1 Serious, 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200414/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N9420Y

Premier One Express LLC

On June 29, 2025, about 1107 eastern daylight time, a Beech 95-B55, N9420Y, was substantially damaged when it was involved in an accident near Mount Dora, Florida. The private pilot was seriously injured and the passenger sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the passenger, the purpose of the flight was to obtain fuel at a different, unspecified, airport. This was the passenger’s first time being in an airplane. He described watching the pilot do a preflight of the airplane, but no fuel was added. During the start-up, everything appeared normal, and they taxied to the runway for departure. He described that once the nose of the airplane became airborne, the right engine “sputtered out” and they immediately went to the right. The airplane contacted a tree, before it came to rest in an adjacent lake. He further described that once the airplane came to rest, the pilot shut the fuel off, and they began to walk back to the airport for assistance.

The airplane came to rest partially in the water of a pond in a residential area. The impact resulted in substantial damage to the left wing and fuselage.

The wreckage was retained for further investigation. 

Monday, July 28, 2025

Mooney M20J, N5764H, fatal accident occurred on July 27, 2025, near Nampa Municipal Airport (MAN/KMAN), Nampa, Idaho

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=N5764H

Sleeptytime PLLC


- History of Flight:
On July 27, 2025, at about 1741 local time, a Mooney M20J, N5764H, registered to Sleeptytime PLLC out of Eagle, ID, was destroyed when it impacted terrain near Nampa Municipal Airport (MAN/KMAN), Nampa, Idaho. The pilot and two passengers were fatally injured. The flight was originating at the time, and was destined to an unknown location.

According to flight-track history, the airplane frequently flew from Nampa to McMinnville, Oregon. It had arrived from McMinnville on July 25, 2025.

According to automatic dependent surveillance-broadcast (ADS-B) data, at 1734:02, the airplane was observed taxiing from the ramp to runway 29. At about 1739:30, the airplane started the takeoff roll from runway 29. At 1740:05, the airplane lifted off, about halfway down the runway. At 1740:33, the airplane was at 2700 ft, 64 knots groundspeed, and climbing. 11 seconds later, at 1740:44, the airplane was observed at 2800 ft, 57 knots groundspeed, and initiating what appeared to be a left turn. 6 seconds later, at 1740:50, the airplane started a 180 degree turn. At 1740:56, the airplane reached an altitude of 2875 ft, 58 knots groundspeed. 3 seconds later, the airplane ceased climbing and was about halfway through the turn when it started to lose altitude. At 1741:05, the last ADS-B return was recorded in the area of the accident site and less than 0.50 mile from the departure end of runway 29. The airplane was at 2800 ft, 68 knots groundspeed, and descending 3000 feet per minute (fpm). (Figure 1)

Figure 1: ADS-B Data Plot

A witness reported that they were in the backyard of a house and observing the accident aircraft takeoff. They stated that the airplane "start turning way too low, looked like they were trying to head back, I think turned too sharp and slow and stalled, nosedived straight into the ground." Which appears consistent with the ADS-B data.

- Pilot Info:
The pilot, aged 43, held a private pilot certificate (a most recent/updated issue date of 6/28/2024), with a rating for airplane single engine land aircraft. His second class FAA medical was issued on February 2024, with a note stating he must use corrective lens(es) to meet vision standards at all required distances.

- Wreckage and Impact Information:
The airplane impacted an unoccupied structure and came to rest upright.. All four corners of the aircraft were accounted for at the accident site. There was no post crash fire. Both wings sustained extensive aft crush damage and remained attached to the airframe. The cockpit/front section sustained aft crush damage. The tail remained attached to the fuselage, was pointed upwards, and sustained deformation damage. The accident appears consistent with a low altitude aerodynamic stall/spin.

The position of the flaps and landing gear could not be determined based on available accident site photos. The forward section of the fuselage was cut by first responders to reach the occupants.

- Aircraft Info:
The 4-seat, low wing, retractable gear airplane, MSN 24-1477, was manufactured in 1984. It was powered by a Lycoming IO-360 SER engine. The certified max gross weight was 2740 lbs.

The following is the stall speeds chart from the POH:


- Airport Info:
Runway 11/29 was 5,000 feet long by 75 feet wide. The runway surface was asphalt. The airport field elevation was 2,537 feet.

- Weather:
METAR KMAN 272335Z AUTO 00000KT 9SM CLR 32/11 A2993 RMK A01
METAR KMAN 272355Z AUTO 00000KT 9SM CLR 32/11 A2993 RMK A01

The density altitude was calculated at 5143 ft.

- Additional Information:
According to the Mooney M20J Pilot Operating Handbook (POH), page 41:

"The best spin recovery technique is to avoid flight conditions conducive to spin entry. Low speed flight near stall should be approached with caution and excessive flight control movements in this flight regime should be avoided, Should an unintentional stall occur the aircraft should not be allowed to progress into a deep stall. Fast, but smooth stall recovery will minimize the risk of progressing into a spin, If an unusual post stall attitude develops and results in a spin, quick application of anti-spin procedures should shorten the the recovery."

Sunday, July 27, 2025

VFR encounter with IMC: Piper PA-60-601P Aerostar, N100PB, fatal accident occurred on July 6, 2023, near Burlington, Colorado

  • Location: Burlington, Colorado 
  • Accident Number: CEN23FA285 
  • Date & Time: July 6, 2023, 13:30 Local 
  • Registration: N100PB 
  • Aircraft: Piper PA-60-601P 
  • Aircraft Damage: Destroyed 
  • Defining Event: VFR encounter with IMC 
  • Injuries: 1 Fatal Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/192561/pdf

https://data.ntsb.gov/Docket?ProjectID=192561

On July 6, 2023, at an unknown time, a Piper PA-60-601P airplane, N100PB, was destroyed when it was involved in an accident near Burlington, Colorado. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot departed the airport about 1330 local time for an unknown destination in visual flight rules conditions. The accident site was located about 12 nautical miles (nm) from the airport; however, the airplane’s flight path and time of the accident are unknown as there was no flight track or recorded data available; there were no witnesses to the accident.

Postaccident examination revealed no preimpact anomalies with the airplane or engines that would have precluded normal operation. Weather conditions after the airplane’s departure suggest the airplane may have encountered an area of deteriorating weather and instrument meteorological conditions (IMC) that reduced visibility and obscured terrain. However, as the accident time is unknown, the investigation was unable to determine if the airplane crashed during a time of deteriorating weather. The pilot was also operating the airplane with an inoperative GPS, which could have decreased the pilot’s ability to maintain situational awareness. The accident site signatures were consistent with a loss of control and impact with terrain.

An autopsy was conducted on the pilot; however, due to the condition of the remains, it could not be determined if an impairing condition or natural disease contributed to the accident. An unknown quantity of ethanol detected by toxicological testing may have been from postmortem production; however, the limited results also do not exclude the possibility of ethanol consumption or related impairment.

- Probable Cause: The pilot’s visual flight rules flight into instrument meteorological conditions, which resulted in a loss of control in flight and subsequent impact with terrain.