Monday, August 03, 2026

Piper PA-30-160 Twin Comanche, N8154Y, accident occurred on July 9, 2026, at Tulsa Riverside Airport (RVS/KRVS), Tulsa, Oklahoma

  • Location: Tulsa, OK 
  • Accident Number: CEN26LA248 
  • Date & Time: July 9, 2026, 17:29 Local 
  • Registration: N8154Y 
  • Aircraft: Piper PA-30 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203379/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N8154Y

On July 9, 2026, about 1729 central daylight time, a Piper PA-30 airplane, N8154Y, was substantially damaged when it was involved in an accident near Tulsa, Oklahoma. The flight instructor and pilot under instruction were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The flight instructor reported that while conducting training maneuverers in the practice area she heard a noise similar to “sputtering” from the right engine and noticed the RPM drop to about 1500 rpms. Shortly after the rpm drop, the noise stopped and the rpm returned to normal. However, due to unexpected right engine issue, she chose to return to the airport. While returning to the airport, the flight instructor reported that all the engine gauges were observed to be within their respective normal ranges. 

During the approach, the flight instructor took the flight controls from the pilot under instruction as she observed that the airplane was too high and drifting from the runway centerline. However, the flight instructor was unable to correct for the unstable approach and chose to perform a go-around. The flight instructor reported that the airplane suddenly rolled inverted to the right after she applied full engine power to perform the go-around.

Video surveillance imagery showed the airplane start an initial climb during the go-around followed by a sudden inverted roll to the right and then impacting terrain in a vertical nose low orientation. The airplane sustained substantial damage to both wings and the fuselage. 

The airplane owner reported that both propeller governors had been recently removed, overhauled, and reinstalled. The airplane was retained for further examination.  

Beechcraft 95-A55 Baron, N7501S, accident occurred on July 2, 2026, near Lancaster, South Carolina

  • Location: Lancaster, SC 
  • Accident Number: CEN26FA241 
  • Date & Time: July 2, 2026, 00:52 Local 
  • Registration: N7501S 
  • Aircraft: Beech 95-A55 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203306/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N7501S

On July 2, 2026, at 0052 eastern daylight time (EDT), a Beech model 95-A55 airplane, N7501S, was destroyed when it was involved in an accident near Lancaster, South Carolina. Both pilots received serious injuries. The accident flight was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

The airplane owner reported that the pilots were renting the airplane for the purpose of building multiengine flight experience.

Preliminary ADS-B data indicated that three flights prior to the accident flight were conducted on July 1, 2026. The first flight departed from the Stanly County Airport (VUJ), Albemarle, North Carolina, at 0707 EDT on July 1, 2026, arriving at the Copiah County Airport (M11), Crystal Springs, Mississippi, at 0939 central daylight time (CDT). The second flight departed M11 at 1008 CDT, arriving at Laredo International Airport (LRD), Laredo, Texas, landing at 1336 CDT. The third flight departed LRD at 1553 CDT and arrived at the Poplarville/Pearl River County Airport (M13), Poplarville, Mississippi, landing at 1941 CDT. The airport manager at M13 confirmed that 106 gallons of 100LL aviation fuel was added to the airplane while it was on the ground at M13. 

At 2017 CDT, the airplane departed M13 on the accident flight with VUJ as the intended destination. ADS-B data showed that the airplane proceeded east-northeast until 0043 EDT on July 2, 2026, when it made a left turn to a heading of about 025°. Shortly, thereafter, the airplane turned further left to a westerly heading. At 0046, the crew declared an emergency and advised air traffic control (ATC) services that they were going to divert to Kirk Air Base Airport (T73), Lancaster, South Carolina, due to issues with both engines. When the airplane was about 2 nm north of T73, they advised that they would instead divert to the Lancaster County Airport-Mc Whirter Field (LKR), Lancaster, South Carolina. ADS-B data showed that the airplane continued descending and the final recorded location was about 4 nm and 105° from LKR. The accident location was 0.2 nm west of the final recorded ADS-B position (see figure 1). 

The airplane came to rest on a wooded hillside. There was evidence of a postimpact fire that consumed most of the cabin section of the airplane. 

The forward part of the airplane’s fuselage, including the baggage compartment, cabin and nose were almost completely consumed by the postimpact fire. The aft fuselage was predominately intact.

The left horizontal stabilizer and elevator, along with the vertical stabilizer and rudder, remained attached to the aft fuselage. The right horizontal stabilizer and elevator had separated from the airplane and was located in the immediate area of the main wreckage.

The left wing remained partially attached by control cables; however, the inboard portion of the wing between the engine nacelle and the fuselage side was mostly consumed by fire but was otherwise intact to the left-wing tip. The left engine nacelle from the firewall aft was attached to the wing but the engine had separated. The landing gear was present at the accident site but its position could not be determined during the on-scene phase of the examination. The cockpit and cabin section of the fuselage was almost completely consumed by the postimpact fire. Both engines were present near the main wreckage.

The outboard portion of the right wing from about the flap/aileron joint was separated and located in the immediate area of the main wreckage. The inboard portion of the right wing, including the engine nacelle aft of the firewall was mostly consumed by the postimpact fire. The engine and firewall came to rest near the main wreckage. A portion of the right-wing flap came to rest near the separated portion of the right wing. 

On-scene examination was limited due to the location of the wreckage and the prevailing terrain. The wreckage was recovered for further examination. 

First responders reported that the pilots were outside of the airplane before they arrived and there was no information as to which seats the pilots occupied. Therefore, it is unknown which pilot was manipulating the flight controls at the time of the accident. Both pilots received severe burns and were transported to a hospital burn unit for treatment.

One pilot held a commercial pilot certificate with airplane single engine land, multiengine land, and instrument airplane ratings. He also had a second-class medical certificate issued March 2026. 

The other pilot held a commercial pilot certificate with airplane single engine land, multiengine land, and instrument airplane ratings. He also held a flight instructor certificate with airplane single engine and instrument ratings. The airplane owner reported that this pilot had recently received his flight instructor rating for multiengine land airplanes. He also had a first-class medical certificate issued February 2026. 

Stoddard-Hamilton Glasair I-RG, N141CG, accident occurred on July 9, 2026, near Utica, Minnesota

  • Location: Utica, MN 
  • Accident Number: CEN26LA250 
  • Date & Time: July 9, 2026, 18:05 Local 
  • Registration: N141CG 
  • Aircraft: Glasair I RG 
  • Injuries: 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203383/pdf

http://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N141CG

On July 9, 2026, about 1805 central daylight time, a Glasair 1RG airplane, N141CG, sustained substantial damage when it was involved in an accident near Utica, Minnesota. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight.

The pilot reported that the flight was for the purpose of checking the electric pitch trim system of the airplane. While testing the system in flight, at altitudes between 2,000 and 3,000 ft msl, the engine lost power. At this time the pilot had the electronic flight information (EFIS) screen of his avionics suite displaying mostly flight information. When the engine lost power, the pilot switched the EFIS to the engine management page and it showed that the airplane’s header tank was empty.

The pilot attempted to restore engine power but was unsuccessful. He executed a forced landing to a road. During the landing, while attempting to avoid obstacles along the roadway. The airplane went off the road and struck a culvert before coming to rest. During the forced landing the airplane sustained substantial damage to the forward fuselage.

Discussion regarding the airplane’s fuel system with the pilot and with the original builder of the airplane revealed that the airplane had a single main wing tank, and a fuselage mounted header tank. Each tank was connected to a selector valve which determined which tank the engine would draw fuel from. In addition, there was a transfer pump installed that allowed pumping fuel from the wing tank to the header tank. Any overflow of fuel from the header tank would return to the wing tank. The original builder stated that it was possible to leave the transfer pump on at all times with the selector valve set to the header tank.

The pilot stated that during the accident flight the transfer pump switch was in the “on” position and he verified this when the engine lost power. Once the engine lost power the pilot switched the fuel selector to the main wing tank and attempted to restart the engine without success. Further testing of the transfer pump is planned. 

Robinson R44 Astro, N484AT, accident occurred on July 18, 2026, near Adair, Iowa

  • Location: Adair, IA 
  • Accident Number: CEN26LA259 
  • Date & Time: July 18, 2026, 14:40 Local 
  • Registration: N484AT 
  • Aircraft: ROBINSON HELICOPTER R44 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 137: Agricultural

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203426/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?NNumberTxt=N484AT

On July 18, 2026, about 1440 central daylight time, a Robinson Helicopter Company R44, N484AT, was substantially damaged when it was involved in an accident near Adair, Iowa. The pilot was not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

The pilot stated that he was recently hired by the owner to complete agricultural spraying operations. He spoke with the pilot who flew the helicopter on the previous day and reported that the engine governor was slow to respond and that he should watch it during subsequent flights. The accident pilot decided to load the helicopter with water and complete a test flight to ensure normal operations and no governor malfunctions. The test flight was completed with no anomalies noted, and the governor was working normally. The pilot completed about 5 hours of flight time and sprayed about 600 acres without incident. Shortly before the accident, the pilot landed the helicopter on the refueler truck and added 1 quart of oil to the engine, then continued to spray another field. The pilot had completed 2 to 3 spray passes and climbed out of the field to turn around for another pass. During the turn, the low rotor rpm horn sounded so the pilot lowered the collective and increased the throttle, which increased the rotor rpm and the horn turned off. The pilot continued another spray pass and the low rotor rpm horn sounded again. He attempted to increase the throttle beyond the governor limitation, but the horn continued. The helicopter was flying about 60 mph and was about 15 to 20 ft above the field, so he executed an autorotation and landed in the mature corn. The helicopter slid in the field and rolled left, then came to rest upright. 

The responding FAA inspector reported that the helicopter sustained substantial damage to the main rotor blades, fuselage, and tailcone. Postaccident examination revealed that the governor control unit was not secured to its mounting location but was still connected to the airframe main wiring harness. 

The owner and company mechanic stated that the helicopter was recently purchased for the agricultural business and discovered that the previous owner had removed the governor control unit. They acquired another governor control unit and helicopter underwent an overhaul. When the helicopter was put back into service, the governor control unit was not secured to its mounting location. 

The helicopter was retained for further examination. 

Aero Commander Callair A-9B, N7799V, accident occurred on July 27, 2026, near Livonia, Missouri

  • Location: Livonia, MO 
  • Accident Number: CEN26LA269 
  • Date & Time: July 27, 2026, 08:19 Local 
  • Registration: N7799V
  • Aircraft: Aero Commander CALLAIR A-9B 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 137: Agricultural

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203464/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?NNumberTxt=N7799V

On July 27, 2026, about 0819 central daylight time, an Aero Commander Callair A-9B airplane, N7799V, was substantially damaged when it was involved in an accident near Livonia, Missouri. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 agricultural application flight. 

The pilot stated that he was spraying a field at the time of the accident. When the airplane was about 50 feet above ground level, the engine lost power abruptly as it came over a tree line on a final application pass. The pilot conducted a forced landing into the soybean field. The airplane sustained damage to the ailerons, fuselage, empennage and rudder during the forced landing.

The pilot informed investigators that the airplane was fully fueled before the flight. Examinations of the engine and airframe fuel system are planned following recovery of the airplane from the accident site.

de Havilland Canada DHC-2 Beaver, N791PW, accident occurred on July 19, 2026, in Nondalton, Alaska

  • Location: Nondalton, AK 
  • Accident Number: ANC26LA072 
  • Date & Time: July 19, 2026, 14:40 Local 
  • Registration: N791PW 
  • Aircraft: DEHAVILLAND DHC-2 MK.I 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Business

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203418/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N791PW

On July 19, 2026 about 1440 Alaska standard time, a DeHavilland DHC-2 airplane, N791PW was substantially damaged when it was involved in an accident near Nondalton, Alaska. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 business flight. 

The pilot reported that he conducted a normal landing on a remote airstrip, and after touching down he applied the brakes, but the right brake did not respond. The airplane veered to the left, the pilot attempted to correct the left drift by adding additional right brake; the brake did not respond. The airplane ground looped and departed the runway which resulted in substantial damage to the right wing and right elevator. 

A postaccident examination of the brake system is pending.

Piper PA-28-180 Cherokee C, N454MD, accident occurred on July 20, 2026, near Bulverde Airpark (1T8), San Antonio, Texas

  • Location: Bulverde, TX
  • Accident Number: CEN26LA265
  • Date & Time: July 20, 2026, 13:40 Local
  • Registration: N454MD Aircraft: Piper PA-28-180
  • Injuries: 2 Minor
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203440/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N454MD

On July 20, 2026, about 1340 central daylight time, a Piper PA-28-180, N454MD was substantially damaged when it was involved in an accident near Bulberde, Texas. The flight instructor and student pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 instructional flight.

The flight instructor reported that they had been performing takeoff and landing practice and had accomplished three successful takeoffs and landings. On the forth takeoff, when the airplane was 50 to 60 ft above the ground, the engine stopped producing power. A forced landing was executed, during which, the airplane struck trees and sustained substantial damage to the fuselage, both wings, and the empennage surfaces.

The airplane has been retained for further examination.