Friday, August 28, 2026

Politechnika Warszawska PW-5 Smyk, N105WS, fatal accident occurred on August 6, 2026, near Briggs, Texas

  • Location: Briggs, TX
  • Accident Number: CEN26LA282
  • Date & Time: August 6, 2026, 15:38 Local
  • Registration: N105WS
  • Aircraft: PZL-BIELSKO B1-PW-5
  • Injuries: 1 Fatal
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203557/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N105WS 

On August 6, 2026, about 1538 central daylight time, a PZL-Bielsko B1-PW-5 glider, N105WS, was substantially damaged when it was involved in an accident near Briggs, Texas. The pilot was fatally injured. The glider was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The glider was departing on an auto-tow launch at the time of the accident. According to witness statements, the glider achieved level flight at about 1,000 ft before release from the towline. Following the release, the glider yawed to the right and entered a descending spiral, completing about 7 to 8 rotations before impacting terrain west of the glider port. Witnesses reported that the glider impacted the ground in a near-vertical attitude. 

The cockpit and forward fuselage were crushed aft during the impact. Both wings remained attached to the fuselage. The tail section and vertical stabilizer were partially separated, with the aft 4 ft of the tail boom folded over the aft fuselage. 

The glider was retained for further examination.

Aviat A-1B Husky, N299CA, accident occurred on August 17, 2026, near Pilot Grove, Minnesota

  • Location: Pilot Grove, MN 
  • Accident Number: CEN26LA295 
  • Date & Time: August 17, 2026, 14:46 Local 
  • Registration: N299CA 
  • Aircraft: AVIAT AIRCRAFT INC A-1B 
  • Injuries: 2 Minor 
  • Flight Conducted Under: Part 91: General aviation - Other work use 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203613/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N299CA

On August 17, 2026, about 1446 central daylight time, an Aviat Aircraft Inc A-1B airplane, N299CA, was substantially damaged when it was involved in an accident near Pilot Grove, Minnesota. The two pilots received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 aerial photography flight. 

The pilot in the rear seat stated they were conducting an aerial photography flight and had flown for about 5 ½ hours that day. During the flight, the front seat pilot was manipulating the flight controls and noted that the airplane was not responding normally. They observed that the left aileron had partially detached from the wing and the outboard end was hanging down. The front seat pilot executed an emergency landing to a field. During the landing, the airplane nosed over and sustained substantial damage to both wings and the empennage. 

Postaccident examination of the airplane revealed that the left outboard aileron hinge bracket was fractured. The airplane was retained for further examination. 

A review of NTSB records revealed that the airplane was involved in a similar accident in 2017 involving an inflight failure of the left outboard aileron hinge bracket assembly. 

Robinson R44 Raven II, N26KL, accident occurred on August 2, 2026, near Bennett, Iowa

  • Location: Bennett, IA 
  • Accident Number: CEN26LA276 
  • Date & Time: August 2, 2026, 13:18 Local 
  • Registration: N26KL 
  • Aircraft: Robinson Helicopter Company R44 II 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 137: Agricultural

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203517/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N26KL

On August 2, 2026, about 1318 central daylight time, a Robinson Helicopter Company R44 II helicopter, N26KL, was substantially damaged when it was involved in an accident near Bennett, Iowa. The pilot was not injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 137 agricultural flight.

The pilot reported that as the helicopter passed over a tree line he felt a vibration in the airframe and when the vibration increased he decided to perform an autorotation into the next field. According to the pilot, the helicopter descended rapidly from about 20 ft above the ground which resulted in a hard landing.

A witness to the accident reported hearing an “awful” noise before the helicopter passed over a tree. The witness stated that as the helicopter descended the main rotor blades almost stopped rotating when the helicopter was about 10 to 15 ft above the ground, and then the helicopter dropped vertically into the field.

The airframe and tailboom sustained substantial damage during the hard landing.

The helicopter was recovered to a secure facility pending an examination.

Thursday, August 27, 2026

Embraer ERJ-170-200LR, N307LH, and Sikorsky VH3D, incident occurred on August 4, 2026, near Ronald Reagan National Airport (DCA/KDCA), Washington, DCA

  • Location: Washington, DC 
  • Incident Number: OPS26LA063 
  • Date & Time: August 4, 2026, 14:34 Local 
  • Registration: MILITARY - VM1 (A1); N307LH (A2) 
  • Aircraft: Sikorsky VH3D (A1); YABORA INDUSTRIA AERONAUTICA S ERJ 170-200 LR (A2) Injuries: N/A (A1); N/A (A2) 
  • Flight Conducted Under: Armed Forces (A1); Part 121: Air carrier - Scheduled (A2)

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203529/pdf

On August 4, 2026, about 1434 eastern daylight time (EDT), Marine One (VM1) a Sikorsky VH3D, and Envoy Air flight 3742 (ENY3742), an Embraer E-170, were involved in a loss of separation about 2 miles north of Ronald Reagan Washington National Airport (DCA), Arlington, Virginia. There were no injuries reported to the passengers or crewmembers on board either aircraft.  

VM1 was a military Presidential transport local flight operating under the provisions of Title 14 Code of Federal Regulations (CFR) Part 91 from The Ellipse Park, Washington, D.C. ENY3742 was a scheduled domestic passenger flight operating under the provisions of Title 14 CFR Part 121 from DCA to Pensacola International Airport (PNS), Pensacola, Florida. At the time of the loss of separation, VM1 had departed The Ellipse when ENY3742 was departing runway 1 and beginning their initial climb. After the loss of separation, VM1 completed their local flight without incident while ENY3742 completed their flight to PNS without incident. Figure 1 below shows key locations and estimated position of both aircraft at FAA’s estimated closest proximity.

As part of the investigative process, the NTSB invited qualified parties to participate in the investigation. Parties to the investigation include the Federal Aviation Administration (FAA), Department of the Navy (DON), and Envoy Air Inc. In accordance with the International Civil Aviation Organization (ICAO) Annex 13, Centro de Investigação e Prevenção de Acidentes Aeronáuticos (CENIPA) of Brazil, representing the State of Design of the Embraer 170 airplane, was notified of the investigation.

Certified air traffic control (ATC) audio recordings and Standard Terminal Automation Replacement System (STARS) radar data were provided by the FAA. Table 1 provides a summary of key communications between the DCA Airport Traffic Control Tower (ATCT) Helicopter Control (HC) and Local Control (LC) controllers and the flight crews of VM1 and ENY3742. The two transmissions in red italics were sourced from a third-party application: ATC – Live Air Traffic Radio. According to the disclaimer in their application, ATC audio in their application is sourced from Enhanced Radar (a company that builds Artificial Intelligence (AI)- driven systems to transcribe, analyze, and optimize ATC communications and airspace operations) and processed with their Y4-small AI model. These transmissions were not received by FAA ATC radio receivers and were unable to be heard by the DCA ATCT HC or LC controllers. Note: The HC and LC positions operate on different frequencies and therefore, flightcrews and controllers can only hear what is being transmitted on the frequency they are using – in this case, VM1 was on the HC frequency and ENY3742 was on the LC frequency.  


A preliminary FAA estimate of the closest proximity between VM1 and ENY3742 determined they were about .82 miles apart laterally and about 700 feet vertically, as shown in figure 2.

Envoy Air Flight 3742 Flightcrew Statements 

Postincident statements provided by ENY3742 flightcrew revealed the first officer (FO) was the pilot flying and the captain was the pilot monitoring. Both crewmembers recalled that after takeoff from runway 1, as the aircraft climbed and accelerated, the Terminal Collision Avoidance System (TCAS) announced a traffic advisory (TA) with “Traffic, Traffic.” At no time was the TCAS TA target acquired visually by either crewmember. The TCAS TA target symbol remained to the right and below their own-ship symbol the entire time. Both recalled seeing 600 feet of vertical separation being displayed on TCAS as the TA target passed behind their right wing of the own-ship symbol on the display. The captain added that at no time was the TCAS resolution advisory (RA) displayed, announced, or commanded.

DCA Helicopter Frequency Communications 

Certified ATC audio recordings revealed that the first attempt to contact DCA ATCT was not received at all, and the second attempt was broken and completely unreadable (to which the controller advised on frequency). The frequency had been working normally and there were no known outages or reports of degradation of this frequency on the day of the event, nor was there a history of problems with this frequency according to FAA. As a result of the missed transmissions with VM1 on the day of the incident, FAA technicians from Spectrum Engineering conducted a coverage analysis and determined that there was not adequate lineof-sight to ensure communications between the radio transmitter/receiver sight and The Ellipse, where VM1 was temporarily operating from while construction was ongoing at the White House.

FAA Technical Operations Personnel Interviews 

Postincident interviews were conducted with personnel from FAA’s technical operations responsible for the ATC radios used at DCA ATCT. Both technicians stated that there had been no documented history of reported problems with the HC frequency and had been no report on the day of the incident until after the incident had occurred. After finding the line-of-sight deficiencies in their coverage analysis done immediately after becoming aware of the problem, the FAA relocated the radios for the HC frequency from their location in a nearby residential neighborhood, to the top of the DCA ATCT.

DCA ATCT Air Traffic Manager Interview 

The postincident interview with the air traffic manager (ATM) also revealed that there was no known history of problems with the HC frequency from ATC. The ATM also reported that once the technicians had relocated the radios to the tower, ATC conducted radio checks with two separate Marine Helicopter Squadron One (HMX-1) aircraft located at The Ellipse and in the local vicinity and reported no deficiencies. Additionally, there were no deficiencies noted in communication with other helicopters in communication with DCA ATCT either. 

Meeting Between DCA ATCT and HMX-1 

DCA ATCT and HMX-1 staff met the week preceding the incident on July 30, 2026. According to the ATM, this was not a regularly scheduled meeting, but rather a meeting that had been requested by HMX-1 to discuss local operations and to express the need for more training flights within the DCA Class B airspace, and ATC wanted to discuss concern with recent reports of their not receiving the required 3 minute to liftoff call from HMX-1 flight crews. At that time, HMX-1 advised that communications “had been spotty,” and felt that may have been the reason. It was agreed that they would attempt other means of reaching the tower in situations where they were unable to reach them to provide the 3-minute call (for example, relaying through another aircraft), and on the day of the incident evidence showed they did. After not reaching them on their initial attempt, they had attempted to relay the 3-minute call through the helicopter facility at Joint Base Anacostia-Bolling, which was also unsuccessful.

Loss of Standard Separation

The FAA reported the preliminary estimated closest proximity between VM1 and ENY3742 as about .82 nm laterally and 700 feet vertically. This would meet the required minimum radar separation as set forth in FAA Order JO 7110.65BB, Air Traffic Control, paragraph 7-9-4, which required 1.5 nm lateral or 500 feet vertical separation within Class B airspace, between a VFR aircraft and any aircraft weighing more than 19,000 pounds or any turbojet aircraft. The NTSB is still reviewing all sources of surveillance data to calculate and confirm closest proximity. Additionally, in accordance with the letter of agreement (LOA) between HMX-1 and Washington, DC area ATC facilities, aircraft operations with the President on board require flightcrews to contact DCA ATCT on 134.35 (HC frequency) 3 minutes prior to departure, and according to the LOA between DCA ATCT and PCT TRACON, DCA would stop all departures once the 3-minute call was received. In this incident, after attempting to contact DCA ATCT at least twice, they ultimately departed and were then able to reach DCA ATCT when the helicopter reached an altitude that provided adequate line-of sight communications. Having received no 3-minute call, the LC controller had cleared ENY3742 for takeoff and the airplane was becoming airborne simultaneously as VM1 established communications with the tower. The current altimeter setting and traffic advisory were provided to VM1, to which the crew immediately reported visual contact with the traffic. 

The NTSB’s incident investigation is ongoing.

Wednesday, August 26, 2026

Van's RV-8, C-GFWR, accident occurred on August 5, 2026, at Great Falls International Airport (GTF/KGTF), Great Falls, Montana

  • Location: Great Falls, MT 
  • Accident Number: WPR26LA295 
  • Date & Time: August 5, 2026, 10:34 Local 
  • Registration: C-GFWR 
  • Aircraft: Vans RV8 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203563/pdf

https://wwwapps.tc.gc.ca/Saf-Sec-Sur/2/CCARCS-RIACC/ADet.aspx?id=531133&rfr=RchSimp.aspx

On August 5, 2026, at about 1034 mountain daylight time, a Van’s Aircraft RV-8, C-GFWR, was substantially damaged when it was involved in an accident near Great Falls, Montana. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The airplane departed Villeneuve Airport (CZVL), near Edmonton, Alberta, Canada, and landed on runway 21 at Great Falls International Airport (KGTF), Great Falls, Montana. During the landing rollout, the airplane veered right. The pilot applied engine power while attempting to regain directional control, and the airplane subsequently ground looped to the right and departed the runway. The left main landing gear collapsed, and the left wing contacted the ground. The airplane came to rest in the grass adjacent to the runway. 

The airplane sustained substantial damage to the left wing, and fuselage. The pilot reported that the tailwheel assembly had been replaced about two weeks before the accident and that the accident flight was the airplane’s first flight and landing since the replacement. 

The airplane was retained for examination.

Cessna 177B Cardinal, N34852, accident occurred on August 5, 2026, near Perris, California

  • Location: Perris, CA 
  • Accident Number: WPR26LA291 
  • Date & Time: August 5, 2026, 11:17 Local 
  • Registration: N34852 
  • Aircraft: Cessna 177B 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203540/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?nNumberTxt=N34852

On August 5, 2026, at 1117 mountain daylight time, a Cessna 177B, N34852, was substantially damaged when it was involved in an accident near Perris, California. The flight instructor and student pilot were not injured. The airplane was being operated as a Title 14 Code of Federal Regulations Part 91 instructional flight. 

According to both pilots, after completing a series of maneuvers, the engine lost power while positioning the airplane to practice S-turns at 1,500 ft AGL. Attempts to restart the engine were unsuccessful so the flight instructor performed an emergency landing to a field. During landing the airplane struck vegetation and nosed over, resulting in substantial damage to the left wing and fuselage. The pilots reported 44 gallons of fuel onboard at takeoff and they had been airborne about 1.5 hrs when the engine quit.

Tuesday, August 25, 2026

Piper PA-22-150 Tri-Pacer, N4535A, fatal accident occurred on July 27, 2026, at Dan Creek Airstrip near Chitina, Alaska

  • Location: Chitina, AK 
  • Accident Number: ANC26FA077 
  • Date & Time: July 27, 2026, 21:30 Local 
  • Registration: N4535A 
  • Aircraft: Piper PA22 
  • Injuries: 3 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203476/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N4535A

On July 27, 2026, about 2130 Alaska daylight time, a deregistered Piper PA-22-150 airplane, N4535A, was destroyed when it was involved in an accident near Chitina, Alaska. The pilot and two passengers were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

According to witnesses, the pilot and two passengers departed McCarthy Airport, McCarthy, Alaska, to drop off the passengers and supplies at the upper Dan Creek airstrip, located about 12 miles southeast of McCarthy. The upper Dan Creek airstrip is an uncharted private strip that is generally considered one way in and out, surrounded by steeply rising terrain, and goarounds are not recommended. 

Multiple witnesses, located on the ground in the vicinity of the airstrip, reported hearing the airplane approaching the southeast runway for landing at a normal approach power setting. The witnesses stated that they then heard the airplane’s engine increase to a high-power setting, then there was a moment of silence, followed by the sound of an impact.

The airplane impacted a berm on a rock-covered riverbank in a left-wing-low flight attitude about 740 ft north of the airstrip. The wreckage was oriented on a northwest heading. All four corners of the airplane were accounted for at the accident site. The outboard portion of the left wing was bent downwards and aft. The fuselage, inboard left wing, and portions of the inboard right wing were consumed by a postimpact fire. 

During the onsite investigation, no preimpact anomalies were visually observed with the flight control system. The fuel selector was positioned on the left tank, and 100LL aviation fuel was present in the left wing. The throttle was found in the idle position and was bent in the direction of the pilot. The propeller blades exhibited rotational signatures including leading edge tip damage and chordwise witness marks, indicative of operation at a low-power setting upon impact. 

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