Wednesday, August 12, 2026

Nose over/nose down: Cessna A185F Skywagon, N61323, fatal accident occurred on August 24, 2024, in Kent, Washington

  • Location: Kent, Washington 
  • Accident Number: WPR24FA285 
  • Date & Time: August 24, 2024, 10:10 Local 
  • Registration: N61323
  • Aircraft: Cessna A185F 
  • Aircraft Damage: Substantial 
  • Defining Event: Nose over/nose down 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/194996/pdf

https://data.ntsb.gov/Docket?ProjectID=194996

On August 24, 2024, about 1010 Pacific daylight time, an amphibious float-equipped Cessna A185F airplane, N61323, was substantially damaged when it was involved in an accident near Kent, Washington. The pilot was fatally injured. The flight was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot had been storing his amphibious float-equipped airplane at a nearby airport for about 7 weeks and was returning the airplane to his lakefront home less than 3 nautical miles (nm) away, intending to moor the airplane to serve as a photo backdrop for a private event the same day. Area weather at the time of the accident included light rain but met visual flight rules (VFR) criteria. On the morning of the accident, a pilot (and guest of honor of the event) told the accident pilot not to worry about flying the airplane over, given the rainy weather, but the accident pilot expressed no concern. Witnesses who watched the airplane depart reported that its landing gear was not retracted before they lost sight of it.

As the airplane made its landing approach to the lake, witnesses observed that the landing gear was in the extended position and reported that the airplane “flipped” as soon as the floats began to contact the water. They reported that the airplane’s approach otherwise appeared normal. 

Postaccident examination of the airplane revealed that the landing gear was extended at the time of touchdown and that the landing gear selector handle was in the “down” position. Although foreign objects (loose tools) were found in the engine cowling and left nosewheel gear well, their locations before the accident sequence are not known, and there was no evidence of any preimpact interference with the engine operation or landing gear mechanism. (An open bin of tools was found in the cabin.) Examination of the airplane and testing of the airplane’s landing gear position advisory unit revealed no mechanical malfunction or failure that would have precluded normal operation.

Based on the evidence, the pilot left the landing gear in the extended position before the water landing.

- Probable Cause: The pilot’s failure to properly configure the amphibious landing gear for a water landing, which resulted in a touchdown on the water with the wheels extended, noseover, and airplane submersion.

Tuesday, August 11, 2026

Enstrom F-28F Falcon, N8624B, accident occurred on July 21, 2026, at Malad Airport (MLD/KMLD), Malad City, Idaho

  • Location: Malad City, ID 
  • Accident Number: WPR26LA270 
  • Date & Time: July 21, 2026, 08:15 Local 
  • Registration: N8624B 
  • Aircraft: Enstrom F-28F 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203436/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N8624B

On July 21, 2026, about 0815 mountain daylight time, an Enstrom F-28F helicopter, N8624B, was substantially damaged when it was involved in an accident near Malad City, Idaho. The pilot and pilot-rated passenger were not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The pilot in command, who was positioned in the left seat reported that the intent for the flight was to fly around the local area. After conducting a preflight inspection with no anomalies noted, he started the engine, conducted engine runup checks, increased the engine and rotor RPM to 100 percent and ascended to a hover. While conducting the helicopters in ground effect hover checks, he noticed that the manifold pressure was high, but still in the green. The pilot air taxied from the hangar parking area to the north toward the taxiway intersection near the approach end of runway 35 and saw that the manifold pressure was abnormally high. He landed the helicopter on the asphalt ramp to assess the instruments and conduct another magneto check, but when he rolled the throttle to flight idle, the engine lost total power. 

The pilot stated that with the engine and rotor RPM still married, he immediately engaged the starter and the engine restarted, but he noticed smoke emanating from the right side of the engine compartment, and there were flames on the lower left side of the engine. He attempted to shut down the engine by pulling the fuel/air mixture control on the instrument panel to the idle cut off position, but the engine continued to operate. He then turned the ignition switch to the off position to no avail, and he engaged the manual fuel shut-off located between the pilot and passenger seat, but the engine continued to operate. Unable to shut down the engine, the pilot and the passenger egressed the helicopter and searched for a fire extinguisher. Unable to locate a fire extinguisher, they contacted first responders, remained a safe distance from the burning helicopter and waited for the fire department to extinguish the blaze. 

The wreckage has been recovered to a secure facility for further examination.

Taylorcraft BC12-D, N43665, accident occurred on August 2, 2026, near Boyceville, Wisconsin

  • Location: Boyceville, WI 
  • Accident Number: CEN26LA277 
  • Date & Time: August 2, 2026, 12:23 Local 
  • Registration: N43665 
  • Aircraft: Taylorcraft BC12-D 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal  

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203519/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N43665

On August 2, 2026, about 1223 central daylight time, a Taylorcraft BC12-D airplane, N43665 was substantially damaged when it was involved in an accident near Boyceville, Wisconsin. Both the pilot and passenger were seriously injured. The airplane was operated under Title 14 Code of Federal Regulations Part 91 as a personal flight. 

According to the passenger, they departed from Marshfield, Wisconsin, earlier in the day and then flew to Red Wing, Minnesota, and then Boyceville, Wisconsin. He said that the engine performed normally and neither he nor the pilot were concerned about the airplane’s performance. The passenger said that before they left Boyceville, the pilot performed a preflight check, which included checking the oil and fuel levels. Shortly after the airplane departed from Boyceville, about 75 to 100 ft above the ground, the engine began to sputter and cut in and out. The passenger stated that the pilot maneuvered the airplane away from trees and then the engine quite completely. The airplane impacted a cornfield. The fuselage and both wings were substantially damaged. 

The airplane was retained for further examination.

Monday, August 10, 2026

Flightstar II SC, N432JP, accident occurred on July 4, 2026, near South Lakeland Airport (X49), Lakeland, Florida

  • Location: Mulberry, FL 
  • Accident Number: ERA26LA258 
  • Date & Time: July 4, 2026, 11:21 Local 
  • Registration: N432JP 
  • Aircraft: PORTZLINE JOAN M FLIGHT STAR II SC 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203314/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?nNumberTxt=N432JP

On July 4, 2026, about 1121 eastern daylight time, an experimental amateur-built Flight Star II SC airplane, N432JP, was substantially damaged when it was involved in an accident near Mulberry, Florida. The private pilot and a passenger were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The pilot stated that he fueled the airplane, performed a preflight inspection, and completed a safety briefing with the passenger. He started the engine and taxied to the runway where he completed an engine runup and a flight control systems check, noting that all instrument indications were normal. He communicated his intentions to take off on runway 14 and began his takeoff roll. The pilot rotated the airplane at 60 mph and established a positive rate of climb. Suddenly, the airplane started to descend. He described the feeling like being on an elevator. The pilot stated that he had felt this before at a neighboring airport during landing. Powerlines obstructed the direction of flight, and unable to climb above the obstruction, the pilot turned the airplane to the right attempting to fly between the poles. The right wing contacted a wire, before the airplane descended and impacted the ground. The airplane came to rest on a roadway on its side and incurred substantial damage to both wings and the fuselage. 

A witness, who was also a pilot, observed the takeoff. He stated that the airplane appeared to maintain a reduced rate of climb relative to its observed pitch attitude. As the airplane passed abeam his position, it began to descend. Throughout the observed sequence, he did not perceive any changes in engine sound. 

The wreckage was recovered and retained for further examination.

Sunday, August 09, 2026

Loss of control in flight: Air Tractor AT-802F Fire Boss, N10122, fatal accident occurred on July 10, 2024, near Helena, Montana

  • Location: Helena, Montana 
  • Accident Number: WPR24FA238 
  • Date & Time: July 10, 2024, 12:10 Local
  • Registration: N10122 
  • Aircraft: AIR TRACTOR INC AT-802A 
  • Aircraft Damage: Substantial 
  • Defining Event: Loss of control in flight 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Public aircraft

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/194667/pdf

https://data.ntsb.gov/Docket?ProjectID=194667

On July 10, 2024, about 1210 mountain daylight time, an Air Tractor AT-802A (Fire Boss) airplane, N10122, was substantially damaged when it was involved in an accident near Helena, Montana. The pilot was fatally injured. The airplane was operated as public use aircraft for the purpose of firefighting.

The pilot of the single-engine air tanker flew as part of a group of four airplanes and was in the No. 2 position. The group departed from their home airport in support of aerial firefighting efforts and arrived at the destination 1 hour and 44 minutes later. Once they arrived on scene, near the wildfire, they flew to a nearby lake to begin the water scooping portion of the mission; the accident occurred during the first scoop sequence.

Witnesses on the lake and in their homes reported that the lead airplane successfully completed its scoop and lifted off from the lake. The float-equipped accident airplane was beginning to scoop when witnesses observed the airplane “moving unsteadily” before the left wing dipped into the water, the right wing rose into the air, the airplane veered left and subsequently impacted the rock face. 

During the initial water scoop, the lead pilot transmitted an instruction to abort the scoop due to a tailwind. As the lead airplane climbed away from the lake, the accident airplane had descended toward the water. The pilot did not acknowledge the abort instruction, and the airplane began to drift to the left. A review of the airplane’s SpiderTrack flight tracking data showed that during the final 1,447 ft of the water scoop, the airplane drifted about 10° left while on the water. The lead airplane’s flight data showed that the accident airplane’s drift to the left, away from the middle of the waterway and toward the shoreline and rock face, occurred simultaneously with the lead airplane’s turn to the left. The pilot did not take any evasive action to avoid the rock face. 

According to the operator, this was the accident pilot’s first fire season. The pilot’s training history showed that during tactical flying, the pilot at times lost situational awareness, which led to a regression in fundamental flying skills and freezing at the flight controls. 

Given these documented deficiencies, the pilot likely experienced a similar degradation in performance during the accident sequence.

Postaccident examination of the wreckage revealed no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 

Toxicology results indicated a low level of cetirizine in the pilot’s postmortem femoral blood; with the low level found, the pilot was not likely to have experienced any significant impairment effects at the time of the accident. Additionally, a very low level measured concentration of morphine was identified in the pilot’s urine. The positive toxicology result is nonspecific and may have been found after opioid drug use or poppy seed consumption. Given the low level detected, it is unlikely that the pilot was impaired by the effects of morphine at the time of the accident.

- Probable Cause: The pilot’s loss of situational awareness during the water scoop due to task overload while operating in a multi-airplane tactical firefighting environment, which resulted in the pilot’s failure to maintain directional control and the airplane’s collision with terrain. 

VFR encounter with IMC: Rans S-19 Venterra, N519JR, fatal accident occurred on August 26, 2024, near Crofton, Nebraska

  • Location: Crofton, Nebraska 
  • Accident Number: CEN24FA326
  • Date & Time: August 26, 2024, 08:41 Local
  • Registration: N519JR 
  • Aircraft: RANS S19 
  • 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/194999/pdf

https://data.ntsb.gov/Docket?ProjectID=194999

On August 26, 2024, about 0841, central daylight time, an experimental, amateur-built Rans S19 airplane, N519JR, was destroyed when it was involved in an accident near Crofton, Nebraska. The pilot sustained fatal injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The airplane departed in daylight, visual weather conditions and proceeded along a meandering flight path before heading towards Yankton, South Dakota, for an unknown destination. About an hour after departure, while over Yankton, the pilot made a telephone call to a friend to inquire about the weather and airport options, stating that he was unable to land due to the weather as he did not hold an instrument rating. The pilot was not instrument rated, the airplane was equipped for only visual flight rules (VFR) operations, and the weather conditions at the nearby airport included a cloud ceiling at 200 ft above ground level (agl) with 1/4-mile visibility in fog and light rain. The friend suggested two airports south of the pilot’s position with automated weather stations reporting VFR weather conditions. The friend also stated that the pilot seemed calm and did not mention if he was in instrument meteorological conditions (IMC). 

A NTSB weather study determined that a cold front and inversion in the area, along with lowand mid-level troughs, made for an environment conducive to sustained low-level cloud cover, moisture, and precipitation. A review of recovered flight track data from an onboard GPS unit revealed that about the time that the pilot called his friend, the airplane was at an altitude of 3,239 ft mean sea level (msl) tracking roughly southwest. The flight track remained consistent during the next 8 minutes for about 14 nm, suggesting that the pilot was in VFR conditions above the cloud tops.

The airplane then began a right turn to the west with a slow climb to a maximum altitude of about 4,000 ft msl. About 1 minute later, the airplane began an S-turn, followed by a descending left turn for less than a minute before the data was lost. The accident site was located about 3/4 nm northeast of the last data point. The weather study determined that the accident flight was likely in IMC from 3,500 ft msl down to 200 ft agl, with visibility restricted to 1/4 mile or less below the cloud cover. The study also noted that a band of rain showers was moving northeast across the accident site at the accident time, which likely further reduced visibility below the cloud layer and had associated convective turbulence.

A postaccident examination of the airplane revealed no evidence of mechanical malfunction or failure that would have precluded normal operation. However, flight control continuity could not be established due to impact damage.

It is unknown what, if any, weather information the pilot checked before or during the flight, or whether the nearby airport (at the time that the pilot called his friend) was the intended destination. However, the reported weather at that airport from more than 2 hours before the accident flight departed through the time of the accident consistently included low instrument flight rules (LIFR) conditions. (LIFR is defined as a ceiling below 500 ft agl and/or visibility less than 1 mile.)

The weather forecast information applicable for the accident time did not include any graphical or text AIRMETs for instrument flight rules (IFR) conditions, and no terminal aerodrome forecasts were available within 30 miles of the accident site. The National Weather Service (NWS) graphical forecast analysis products issued more than 3 hours before the accident flight departed forecast LIFR surface visibility for the area of the accident applicable about 1 hour 40 minutes before the accident and VFR surface visibility with a cloud ceiling at 2,300 ft msl (about 600 ft agl) for the area of the accident applicable about 1 hour 20 minutes after the accident. The weather conditions encountered by the accident pilot were worse than NWS forecasts valid for the accident time. Several pilot reports (PIREPs) reported cloud tops between 2,600 ft MSL and 3,500 ft MSL in the area.

Loss of external visual references during VFR flight presents a high risk of spatial disorientation and loss of control. Several risk factors for spatial disorientation were present in this accident: the lack of IFR flight instruments, the non-instrument rated pilot, and the weather conditions. Based on these factors, as well as the airplane’s flight track and the orientation and fragmentation of the wreckage consistent with a high-energy impact, the pilot likely experienced spatial disorientation after entering an area of rain, convective turbulence, and IMC which may have been higher than the surrounding cloud tops, and he subsequently lost control of the airplane.

- Probable Cause: The non-instrument-rated pilot's decision to continue visual flight into an area of low cloud cover and precipitation which resulted in an inadvertent encounter with instrument meteorological conditions and a loss of control due to spatial disorientation.