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. 

Glasair Sportsman 2+2, N202AZ, fatal accident occurred on August 10, 2026, near Pine, Arizona

  • Location: Pine, AZ 
  • Accident Number: WPR26FA301 
  • Date & Time: August 10, 2026, 18:35 Local 
  • Registration: N202AZ 
  • Aircraft: New Glasair Sportsman 2 Plus 2 
  • Injuries: 2 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203571/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumberTxt=N202AZ

On August 10, 2026, at about 1835 mountain daylight time, an experimental amateur built Glasair Sportsman 2 Plus 2 airplane, N202AZ, was destroyed when it was involved in an accident near Pine, Arizona. The pilot and passenger were fatally injured. The airplane was operated as Title 14 Code of Federal Regulations Part 91 personal flight. 

According to preliminary ADS-B data, the airplane departed from runway 06 at Payson Airport (PAN), Payson, Arizona about 1827:07. The airplane flew on a northwest heading, climbing to about 5,850 ft mean sea level (msl) at 1831:51, before turning to the southwest above mountainous terrain about 7 nautical miles (nm) northwest of PAN. The airplane proceeded to the southwest and descended into a canyon, when the ADS-B signal was lost at 1835:47, about an altitude of 4,675 ft msl (about 680 ft above ground level and 136 ft above the canyon rim). 

The airplane impacted terrain about 3 nm west of the last ADS-B data point, on the northwestern face of a draw at an elevation of about 3,994 ft msl. The accident site area was comprised of roughly 45° sloping terrain with desert junipers and prickly pear cacti scattered along the rocky slope. The first identifiable point of impact (FIPOI) was a desert juniper with separated and damaged branches along with the left wing tip located at the base of the tree. The FIPOI was located about 791 ft above the base of the ravine, and about 1,300 ft below the ridgeline. The wreckage debris path was about 102 ft in length and oriented on a magnetic heading of 175°. The left wing, left aileron, left flap, right wing tip, fuselage, empennage, and engine were distributed throughout the wreckage debris path. A majority of the wreckage was consumed by a post impact fire. The fuselage came to rest in a right wing low, nose down attitude, on a heading of about 022 ° magnetic. The propeller was separated from the crankshaft aft of the propeller flange. Both propeller blades exhibited “S” bending, and leadingedge gouges. 

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

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

  • Location: Bethany, MO 
  • Accident Number: CEN26FA280 
  • Date & Time: August 4, 2026, 18:39 Local 
  • Registration: N8422P 
  • Aircraft: Piper PA-24-250 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203525/pdf

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

On August 4, 2026, about 1839 central daylight time, a Piper PA-24-250 airplane, N8422P, was destroyed when it was involved in an accident near Bethany, Missouri. The pilot received fatal injuries. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 flight. 

The pilot, who was also the airplane owner, departed on a personal flight under visual flight rules from Peoria International Airport Peoria, Illinois, to Rapid City Regional Airport, Rapid City, South Dakota. Preliminary radar data showed that the flight climbed to an initial cruise altitude of about 13,000 ft msl after departure and operated at an altitude about 12,500 ft msl for about 90 minutes. The cruise altitude increased above 18,000 ft msl and into Class A airspace during the flight, which operated without air traffic control clearance or services. A review of weather data showed the flight entered convective activity after which it descended and impacted terrain. The airplane was destroyed by impact forces and a postcrash fire. 

Postaccident examination of the airplane revealed that it was not equipped with an installed breathable or a portable breathable oxygen system. The postaccident examination revealed no mechanical anomalies that would have precluded normal airplane operation.

Mooney M20G Statesman, N6916N, accident occurred on August 13, 2026, near Luling, Texas

  • Location: Luling, TX 
  • Accident Number: CEN26LA287 
  • Date & Time: August 13, 2026, 13:02 Local 
  • Registration: N6916N 
  • Aircraft: Mooney M20G 
  • Injuries: 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/203588/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N6916N

On August 13, 2026, about 1302 central daylight time, a Mooney M20G airplane, N6916N, sustained substantial damage when it was involved in an accident near Luling, Texas. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 personal flight. 

According to ADS-B data, the flight originated from the David Wayne Hooks Memorial Airport (DWH), Houston, Texas, about 1058. The airplane proceeded to the west-southwest toward San Antonio, Texas, for about an hour. About this time, the pilot contacted San Antonio Approach Control and declared an emergency. The pilot informed the air traffic controller that the airplane’s engine had lost power. The controller advised the pilot of an airport 7 miles northeast. The pilot requested a vector to the airport which the controller supplied. The pilot later reported having the airport in-sight before the airplane’s position reports ceased. 

The pilot reported that he executed a forced landing to a road. He said that during the landing roll, the airplane’s left wingtip contacted vegetation along the side of the road which pulled the airplane to the left. The main landing gear went onto the shoulder of the road and the airplane veered off the road and struck trees. The airplane sustained substantial damage to its left wing.