Friday, August 07, 2026

Sikorsky CH-54A Tarhe, N793HT, fatal accident occurred on August 7, 2026, near Beaver, Utah

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

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N793HT

Photo via Facebook

- History of Flight:
On August 7, 2026, at about 1100 local time, a Sikorsky CH-54A Tarhe helicopter, N793HT, operated by Helicopter Transport Services out of Aurora, Oregon, was destroyed when it was involved in an accident at the Three Creeks Reservoir near Beaver, Utah. The two pilots onboard were fatally injured. The public-use firefighting flight originated from Richfield Municipal Airport (RIF/KRIF), 
Richfield, Utah, at 1016 LT.

Nothing else is known right now. Updates soon.

NTSB Preliminary: Dakota Cub AC-18, N84AJ, fatal accident occurred on July 16, 2026, near Plymouth Municipal Airport (PYM/KPYM), Plymouth, Massachusetts

  • Location: Plymouth, MA 
  • Accident Number: CEN26FA257 
  • Date & Time: July 16, 2026, 07:40 Local 
  • Registration: N84AJ 
  • Aircraft: Dakota Cub Super 18 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203409/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N84AJ

On July 16, 2026, about 0740 eastern daylight time, a Dakota Cub Super 18 airplane, N84AJ, was substantially damaged when it was involved in an accident near Plymouth, Massachusetts. The pilot was fatally injured. The airplane operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

ADS-B data obtained from the FAA and data extracted from the airplane’s Garmin G3X showed that the airplane departed from Plymouth Municipal Airport (PYM), Plymouth, Massachusetts, about 0632, and flew south towards Katama Airpark(1B2), Edgartown, Massachusetts, and then flew back towards PYM, generally staying below 1,000 ft above ground level. The airplane flew a path similar to a straight-in for runway 33 until it was about 1.4 miles from the departure end of the runway (see figure 1).

According to preliminary information provided by the Massachusetts State Police, eyewitnesses by Curlew Pond reported that as the airplane flew over the pond, the engine started to sputter. The airplane initially continued toward the airport but turned back toward the water, and then the engine noise went quiet. The airplane glided to the water and then nosed over inverted (see figure 2). 

The airplane was brought to a nearby shore, and turned back to the upright position. After initial documentation of the airplane, it was transported to the airport for further examination.

Postaccident examination revealed the magneto switch was selected to the BOTH position and the fuel pump switch was in the ON position. The fuel selector was selected to the left tank. Neither wing fuel cap was recovered with the airplane. The left fuel tank contained less than 10 ounces of fuel and the right fuel tank contained less than 4 ounces of fuel; neither fuel tank was breached. Fuel lines from the fuel tanks to the fuel selector remained secured and when opened contained fuel. Using a water detection paste, the fuel from the left fuel tank line contained some water and the fuel in the right fuel tank line did not contain any water. A fuel sample from the gascolator bowl contained a mixture of fuel and water. It is unknown how much fuel may have drained out of either tank while the airplane was inverted in the water. The fuel line from the engine driven fuel pump to the fuel servo was empty of fuel. The fuel servo’s fuel screen was free of visual contaminants. 

The pilot held a private pilot certificate with ratings for both airplane single engine land and airplane single engine sea.

Beechcraft V35 Bonanza, N3707Q, accident occurred on July 24, 2026, near Arthur N Neu Airport (CIN/KCIN), Carroll, Iowa

  • Location: Carroll, IA 
  • Accident Number: CEN26LA271 
  • Date & Time: July 24, 2026, 15:50 Local 
  • Registration: N3707Q 
  • Aircraft: Beech V35 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203471/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N3707Q

On July 24, 2026, about 1550 central daylight time, a Beech V35 airplane, N3707Q, was substantially damaged when it was involved in an accident near Carroll, Iowa. The pilot was not injured. The flight was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight. 

According to the pilot, he departed from the Arthur N Neu Airport (CIN), Carroll, Iowa, and flew towards Stanton County Municipal Airport (JHN), Johnson City, Kansas. The pilot reported that shortly after takeoff, the engine started to run rough. He turned back towards CIN and noticed that the oil pressure began to decrease. About 5 miles from CIN, the oil pressure dropped to zero. When the airplane was about 3 miles from the airport, the engine started to smoke, and total engine power was lost. He performed a forced landing to a bean field. During the forced landing, the right aileron sustained substantial damage. 

A postaccident visual inspection of the engine revealed a hole in the crankcase above the No. 4 cylinder and additional case damage above the No. 3 cylinder. The oil dipstick showed little or no oil remained in the sump. 

The airplane was retained for further examination.

Thursday, August 06, 2026

Piper PA-24-250 Comanche, N8422P, fatal accident occurred on August 4, 2026, near Bethany, Missouri

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

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N8422P

- History of Flight:
On August 4, 2026, at about 1838 local time, a Piper PA-24-250 Comanche, N8422P, was destroyed when it was involved in an accident near Bethany, Missouri. The pilot was fatally injured.

The rest of the post will be completed later.

- Pilot Information:
Will be written later.

- Airplane Information:
Will be written later.

- Wreckage and Impact Information:
None.

- Weather:
The nearest weather station reported the following conditions about 20 minutes after the accident: 10 miles 
visibility, distant lighting from all quadrants, thunderstorms in the vicinity, a broken cloud layer at 8,000 ft AGL, and an overcast ceiling at 9,500 ft AGL.

Another nearby airport reported the following conditions 3 minutes before the accident: Visibility 7 miles, winds 360 at 13 knots gusting 18 knots, a cloud layer at 1,200 ft AGL and 9,500 ft AGL and a broken layer at 12,000 ft AGL.

The local area forecast discussion reported the following at 1753 LT: "Another round of showers/storms possible Wednesday afternoon and Wednesday night into Thursday morning. A few storms may be strong, with locally moderate to heavy rainfall also possible."

(1) METARs:

METAR KLWD 042253Z AUTO 03010KT 10SM BKN090 24/21 A3001 RMK AO2 SLP156 T02440206

METAR KLWD 042353Z AUTO 01010KT 10SM VCTS BKN080 OVC095 23/21 A3002 RMK AO2 LTG DSNT ALQDS SLP159 T02330211 10289 20233 53005

METAR KEVU 042335Z AUTO 36013G18KT 7SM SCT012 SCT095 BKN120 23/23 A3004 RMK AO2 T02400232

METAR KEVU 042355Z AUTO 03013G18KT 7SM -RA SCT012 SCT042 SCT070 22/22 A2999 RMK AO2 LTG DSNT E T02300230

METAR KEZZ 042335Z AUTO 12004KT 10SM CLR 30/20 A3003 RMK AO2 LTG DSNT N

METAR KEZZ 042355Z AUTO 11003KT 10SM BKN120 30/19 A3003 RMK AO2 LTG DSNT N

(2) Area Forecast Discussion:

Area Forecast Discussion
National Weather Service Kansas City/Pleasant Hill MO
553 PM CDT Tue Aug 4 2026

.KEY MESSAGES...

- Shower/storms possible tonight into Wednesday morning.

- Another round of showers/storms possible Wednesday afternoon
  and Wednesday night into Thursday morning. A few storms may be
  strong, with locally moderate to heavy rainfall also possible.

- Temperatures warm Friday and into the weekend.

&&

.DISCUSSION...
Issued at 150 PM CDT Tue Aug 4 2026

Current H5 analysis shows mid/upper troughing across the
Northern Plains and encroaching on the Upper Midwest, with a
band of 40+ knot H5 winds extending from northern Colorado into
NE Minnesota and western Ontario. At the surface, a cold front
is analyzed northeast to southwest through Iowa, into extreme
SE Nebraska and further into SW Kansas, where a weak surface
cyclone has developed. At this time, showers and a few
thunderstorms are ongoing, primarily north of the cold front
(elevated), across portions of eastern Nebraska and western
Iowa. Meanwhile, south of the front across our CWA, temperatures
have risen into the upper 80s as of 2 PM, with afternoon Max Ts
expected to reach the lower to even mid 90s (south of the KC
metro) by later this afternoon. The front is likely to stall out
and become essentially stationary by later this
afternoon/evening across NW Missouri into NE Kansas. While
stronger mid level flow and better forcing for ascent should
remain north of the front, cannot completely rule out a strong
thunderstorm or two late afternoon into early evening toward the
Iowa border thanks to a moderately unstable air mass in place
along and south of the front, which has prompted SPC to include
northern Missouri within a marginal risk for severe storms.
However, CAM guidance has trended toward keeping convection
primarily north of the Iowa border. By late tonight into the
overnight period. a vort max currently over Colorado, pushes
eastward toward our region, and along with a modest low level
jet, should help develop showers and thunderstorms north of the
front across SE Nebraska into SW Iowa. Once again, most of this
activity should remain north of our CWA, but may sneak southward
into northern Missouri.

As we head into tomorrow, another mid level vort maxima moves
into the region as broad mid/upper troughing across the north
central CONUS digs a little further south into the region, with
the stalled front still in place across the CWA, which should
help generate isolated to scattered showers and storms tomorrow
morning into early afternoon, with another round of convection
possible late tomorrow evening into early Thursday morning. With
dew points in the upper 60s to lower 70s, decent mid level flow
allowing for 30 to 35 knots of effective shear, and 1500 to
2000 J/kg of ML CAPE, a few storms could be strong to severe.
Additionally, with PWATs in the 1.8" to 2" range and deep warm
cloud depths, locally moderate to heavy rainfall may be
possible. There will be yet another chance for showers and
thunderstorms late Thursday into Friday morning.

By Friday and into the weekend, the western ridge re-establishes
itself, with a 597 dam H5 high developing over the Four Corners
region, yielding increasing mid level heights over our CWA.
Afternoon highs should return to the 90s across the CWA for
Saturday and Sunday, with max heat indices ranging from the
upper 90s to the mid 100s, with generally dry weather likely.

&&


.AVIATION /00Z TAFS THROUGH 00Z THURSDAY/...
Issued at 552 PM CDT Tue Aug 4 2026

VFR conds are expected with bkn-ovc mid-lvl clouds btn 10-15kft
expected thru the pd. The exception will be fm 13Z-17Z when a
pd of lgt tsra will be poss at the TAF site. There will also be
the potential for storms at the TAF site late in the TAF pd aft
22z however conf is too low at this time for inclusion in the
TAF. Winds to begin the TAF pd will be out of the ESE/SE btn
5-10kts thru 09Z-11Z aft which they will be lgt and vrb.

&&

.EAX WATCHES/WARNINGS/ADVISORIES...
MO...None.
KS...None.

&&

$$

DISCUSSION...Williams
AVIATION...73

- Additional Information:
None

NTSB Preliminary: Luscombe 8A, N1164K, fatal accident occurred on July 14, 2026, near Canton, Texas

  • Location: Canton, TX 
  • Accident Number: WPR26FA257 
  • Date & Time: July 14, 2026, 13:56 Local 
  • Registration: N1164K 
  • Aircraft: Luscombe 8A 
  • Injuries: 1 Fatal
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203392/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N1164K

On July 14, 2026, sometime between 1252 and 1356 CDT, a Luscombe 8A, N1164K, was substantially damaged when it crashed in a field near Canton, Texas. The pilot, who was the sole occupant, was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The flight had originated from the pilot’s private airstrip where the airplane was hangared, which was oriented north to south. A farmer discovered the airplane wreckage about 800 ft northwest of the private airstrip, at about 1356. 

There were no eyewitnesses to the accident. The pilot sent a text message to a friend at about 1252, which was his last known communication. Additionally, a nearby resident reported hearing what sounded like an engine “winding up” for a few seconds, followed by less than a second of silence, then a “boom” sound. He stated that he heard the sound within the general timeframe of the accident, but he was unable to identify the specific time. 

The accident pilot purchased the airplane in December 2025. His wife told investigators that the pilot flew the airplane frequently and that they felt it did not produce sufficient take-off performance for them to fly together. She said he usually flew it in the morning or evening and had not flown the airplane much in high-temperature conditions. When she returned home from an appointment at around 1400, she observed the windsock located at the north end of the runway, which indicated the wind was from the north. She noted that the wind had been coming from the south earlier in the day. She said that the pilot typically took off to the south because the prevailing winds were generally from that direction, but on the day of the accident she believed he must have taken off to the north.

The airplane impacted a field in a steep, nose-down attitude about 800 feet northwest of the northern end of the private airstrip. The longitudinal axis of the fuselage was oriented on a heading of about 349° magnetic and exhibited fore-aft crushing. All major structures and components of the airplane were located within the immediate wreckage area. Pieces of windscreen plexiglass were scattered forward and left of the primary wreckage, within about a 30-ft diameter. Disturbance of the surface soil was limited to the area located immediately under the wreckage.

The right wing was displaced aft and the left wing was displaced forward. Compression wrinkling was observed along the top skin of the left wing along with forward bending at the wing root leading edge. The right wing was damaged at the outboard leading edge and the aft spar had separated at the fuselage. Both the left and right ailerons remained attached to their respective wings. The empennage remained intact and attached to the aft fuselage. Both elevators and the rudder also remained attached. The elevator trim tab was connected to the left elevator and articulated freely by hand. The upper fuselage had collapsed into the cabin. 

The propeller remained attached to the engine crank flange. One blade was intact and exhibited no chordwise scratches or damage. The second blade was fractured and splintered near the blade root with aft bending.

NTSB Preliminary: Montana Coyote, N448VQ, fatal accident occurred on July 14, 2026, near Shannon Airport (EZF/KEZF), Fredericksburg, Virginia

  • Location: Fredericksburg, VA 
  • Accident Number: CEN26FA253 
  • Date & Time: July 14, 2026, 11:05 Local 
  • Registration: N448VQ 
  • Aircraft: Montana Coyote 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Flight test 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203389/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?nNumberTxt=N448VQ

On July 14, 2026, about 1105 eastern daylight time, an experimental Montana Coyote airplane, N448VQ, was substantially damaged when it was involved in an accident near Fredericksburg, Virginia. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 test flight.

Family members reported that the pilot was conducting a flight test after completing repairs to the airplane after a landing ground loop during a Phase 1 flight test on May 17, 2024. 

Video surveillance showed the airplane departing about 1049 from runway 24 at the Shannon Airport (EZF) in Fredericksburg, Virgina. ADS-B radar data then showed the airplane departing the traffic pattern to the south before returning to airport a few minutes after departure. At 1102, additional video surveillance showed the airplane on a final approach to runway 24. Starting at 1102:57, the start of a level right turn was captured with the airplane deviating to the right of the runway centerline to the right. At 1103:57, the bank angle suddenly increased followed by a drop of the nose with the airplane entering a descending right spiral. At 1103:05, the airplane disappeared behind a treeline in a nose low inverted right bank. A pilot-rated witness stated that everything seemed normal and that he could hear the engine operating normally with an increase in engine noise when the airplane was in the descending spiral.

The airplane came to rest in an equipment storage lot about 0.13 nautical miles from the threshold of runway 24. The airframe was found on its right side with the right wing separated at the wing root. The left wing was partially separated at the forward spar. A small depression was located under the forward fuselage that contained fragments of the composite propeller and cowl.

Flight control continuity was established for the elevator, rudder, and right aileron from the control surfaces to their respective cockpit controls. However, the left aileron torque tube was found separated from the fuselage bellcrank with no bending or witness marks observed on the tube or bellcrank attachment housing. The right aileron torque tube remained secure in the bellcrank attachment housing. The torque tube was attached to the housing using four equally spaced rivets around the circumference of the tube. 

The engine crankshaft was unable to be rotated by hand due to damage of the forward engine case. The magnetos were removed and rotated with a drill with spark observed on all leads. The fuel system was found compromised in numerous locations. Fuel was only observed in the fuel selector. 

The airplane’s Dynon SV-HDX1100 and both aileron torque tube and bellcrank assemblies were retained for further examination.  

NTSB Preliminary: Piper PA-24-260 Comanche, N8606P, accident occurred on July 16, 2026, near Baraboo/Wisconsin Dells Regional Airport (DLL/KDLL), Baraboo, Wisconsin

  • Location: Baraboo, WI 
  • Accident Number: CEN26LA263 
  • Date & Time: July 16, 2026, 15:08 Local 
  • Registration: N8606P 
  • Aircraft: Piper PA24 
  • Injuries: 1 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203432/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N8606P

On July 16, 2026, about 1508 central daylight time, a Piper PA-24-260 airplane, N8606P, sustained substantial damage when it was involved in an accident near Baraboo, Wisconsin. The pilot sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The pilot reported that for the cross-country flight, the airplane had about 6.5 hours of fuel onboard, and the planned flight only required about 2.5 hours of fuel. 

A preliminary review of ADS-B data showed the airplane depart, about 1232, from the Mitchell Municipal Airport (MHE), Mitchell, South Dakota. The airplane traveled to the east toward the destination airport, the Baraboo/Wisconsin Dells Regional Airport (DLL), Baraboo, Wisconsin. About 22 miles to the west of DLL, the pilot maneuvered the airplane to the south of DLL. About 17 miles to the south of DLL, the pilot maneuvered the airplane to the north toward DLL. According to air traffic control, the airplane was cleared for the RNAV (GPS) runway 1 instrument approach at DLL. 

As the airplane flew toward the approach end of runway 1, the airplane turned slightly to the west and then flew to the north over the various hangars, located to the west of runway 1. The airplane then maneuvered to the east, flying over runway 1. The pilot reported that the engine was not responding to his commands, but he did not hear any sputtering or popping noises. The airplane flew to the north of runway 1, the airplane turned to the west, and impacted trees. The pilot reported the airplane impacted trees because it could not produce climb power. The airplane came to rest upright on a flat grass field, on private property, located about 0.30 miles to the northwest of the approach end of runway 19. 

The airplane sustained substantial damage to the fuselage and to both wings. The airplane was recovered from the accident site, and it was transported to a secure location for future examination