Wednesday, September 10, 2025

Ground collision: Bombardier CRJ-200LR, N420AW, accident occurred on February 1, 2025, at Chicago O’Hare International Airport (ORD/KORD), Chicago, Illinois

  • Location: Chicago, Illinois 
  • Accident Number: DCA25LA120 
  • Date & Time: February 1, 2025, 19:02 Local 
  • Registration: N420AW 
  • Aircraft: BOMBARDIER INC CL-600-2B19 
  • Aircraft Damage: Substantial 
  • Defining Event: Ground collision 
  • Injuries: 1 Serious, 13 None 
  • Flight Conducted Under: Part 121: Air carrier - Scheduled

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/199663/pdf

https://data.ntsb.gov/Docket?ProjectID=199663

A serious injury was sustained by a tug driver following a collision with the left wing of Air Wisconsin flight 6181, a CRJ-200, during taxi operations at Chicago O’Hare International Airport (ORD). No injuries were reported among the airplane’s crew or passengers. Night visual meteorological conditions (VMC) prevailed at the time of the accident.

Flight 6181 landed at ORD and was initially held at the B Pad for an open gate (see Figure 1). Once cleared, the aircraft proceeded southbound on Taxiway A under a standard clearance. The first officer was actively monitoring both ramp and ground control frequencies during the taxi.


The captain reported first observing the tug on Taxiway B as the tug began crossing at the access road. The tug appeared to be slowing down suggesting an intent to stop. The captain could not recall whether the tug’s headlights were illuminated and believed he saw the vehicle using ambient lighting.

After briefly diverting attention toward the gate area, the captain looked back and recognized an imminent collision with the tug. Braking was initiated immediately by the captain, but the impact occurred shortly thereafter. The captain described the impact as “not that bad” and believed the tug had struck the wingtip. The flight crew then communicated with the flight attendants, followed by dispatch via the Aircraft Communications Addressing and Reporting System (ACARS).

According to the tug driver, while returning from the international terminal, the vehicle approached the service road leading to the L gates. Before entering the road and crossing taxiway B, the tug came to a complete stop at the designated stop sign and the driver observed an airplane taxiing outbound on Taxiway B. The driver checked both directions and waited until the outbound aircraft cleared the taxiway. The driver also verified that no aircraft were approaching from behind or the opposite direction before proceeding to cross the taxiways (A&B).

The driver stated that as the tug was crossing the taxiways, the left wing of flight 6181, approaching on taxiway A, was not visible until the last moment, leaving insufficient time to react. He also noted the absence of a nose-gear light on flight 6181, which may have contributed to the tug driver not detecting the presence of flight 6181 before the collision.

The collision resulted in the tug overturning and trapping the driver, leading to serious injury. Post-flight inspection revealed substantial damage to the leading-edge front spar of the airplane’s left wing. The tug driver emphasized that had he been aware of the airplane’s presence, he would not have entered the intersection.


According to the Chicago Department of Aviation (CDA) ground motor vehicle operating regulations manual, dated August 2023, a driver must stop prior to initiating the crossing of the taxiways A, B, and V to determine if the crossing could be accomplished without stopping in the islands between the taxiways. Vehicles on service roads must yield to vehicles crossing taxiways.

- Probable Cause: The tug driver’s failure to ensure the taxiway was clear of aircraft prior to crossing, resulting in a collision with the left wing of the taxiing aircraft. Contributing to the accident was the limited visibility of the aircraft due to ambient lighting conditions and the absence of the aircraft’s nose-gear light, which reduced the tug driver’s ability to detect the aircraft’s presence in time to avoid the collision.

Beechcraft K35 Bonanza, N6021E, fatal accident occurred on September 4, 2025, near Cambridge Municipal Airport (CBG/KCBG), Cambridge, Minnesota

  • Location: Cambridge, MN 
  • Accident Number: CEN25FA364 
  • Date & Time: September 4, 2025, 11:05 Local 
  • Registration: N6021E 
  • Aircraft: Beech K35 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200942/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N6901E

On September 4, 2025, about 1105 central daylight time, a Beech K35 airplane, N6021E, sustained substantial damage when it was involved in an accident near Cambridge, Minnesota. The pilot sustained fatal injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A preliminary review of ADS-B data showed that the pilot, who is also the airplane owner, departed in the airplane at 1052 from the Anoka County/Blaine Airport (ANE), Minneapolis, Minnesota. The airplane flew to the north with the intention to land at the Cambridge Municipal Airport (CBG), Cambridge, Minnesota, which is a non-towered airport. The ADS-B data terminated about 2.38 miles to the south of the approach end of runway 34 at CBG.

The airplane came to rest upright in a grass field just to the north of runway 16 at CBG. The location of the airplane was about 0.37 miles from the approach end of runway 16. The airplane sustained substantial damage to both wings and the fuselage.

Onsite examination of the airframe confirmed flight control cable continuity. The main landing gear and flaps were found retracted. The pitch trim was found at 10°, trim tab down.

The fuel selector valve was found in the auxiliary fuel tank position. About 18 gallons of fuel was recovered from the right wing main fuel tank and about one gallon of fuel was recovered from the right wing auxiliary fuel tank. Due to the impact damage sustained, no fuel was recovered from the left wing main fuel tank and the left wing auxiliary fuel tank. The strainer was removed, and no debris was found in the strainer. About two ounces of fuel were recovered from the strainer. No debris or water contamination was noted in the fuel that was recovered from the airframe.

For the onsite examination of the engine, the engine-driven fuel injection pump was removed, the pump drive coupling was found intact with no noted damage, the flexible fuel lines were removed from the pump, with the hose supplying fuel from the firewall to the fuel pump fractured at the fuel pump fitting. All hoses were noted to be nearly free of fuel, only trace amounts of fuel were found. The fuel metering valve and finger screen were found intact with the finger screen being free of contamination and a lack of fuel in the entire metering valve. The fuel manifold was disassembled, the screen was found free of contamination, and no fuel was found in the sediment area of the manifold. No fuel leaks were observed on the engine and no loose fuel line b-nuts were found.

The wreckage was recovered from the accident site, and it was transported to a secure location. A J.P. Instruments EDM 830 unit and Sentry ADS-B unit were secured and transported to the NTSB Vehicle Recorders Laboratory.

The airplane was equipped with a Continental Motors IO-470-C reciprocating engine and a Beech 278-100-7 two-blade constant speed aluminum propeller.

According to the Beech K35 Pilot’s Operating Handbook and FAA-Approved Airplane Flight Manual, the fuel limitations state in part:

Use auxiliary fuel in level flight only and do not use for takeoff or landing.

Additionally, the fuel selector valve has a required placard, which the accident airplane had installed, for the usage of the auxiliary fuel that states:

Level flight only.

Beechcraft A36 Bonanza, N855DC, accident occurred on August 24, 2025, near Gulf Shores International Airport (GUF/KJKA), Gulf Shores, Alabama

  • Location: Gulf Shores, AL
  • Accident Number: ERA25LA313 
  • Date & Time: August 24, 2025, 15:00 Local 
  • Registration: N855DC 
  • Aircraft: Raytheon Aircraft Company A36 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200856/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N855DC

On August 24, 2025, about 1500 eastern daylight time, a Raytheon Aircraft Company A36, N855DC, was substantially damaged when it was involved in an accident near Gulf Shores, Alabama. The pilot and passenger were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to the pilot, he departed Cox field Airport (PRX), Paris, Texas, for a cross-country flight to Gulf Shores International Airport / Jack Edwards Field (JKA), Gulf Shores, Alabama. He topped-off the main fuel tanks before departure. The 3.2-hour flight was uneventful, and he switched fuel tanks every 30 minutes. During the approach to JKA, the pilot decreased the throttle, descended to the traffic pattern altitude and configured the GPS for landing. He switched fuel tanks to the fullest tank, which was the right fuel tank, which was 1/2 full. The left tank was 3/8 full. After the pilot lowered the landing gear and flaps, he noticed the airspeed dropped “a little too much,” so he increased the throttle. At that point, the pilot realized that the engine was not producing power, and the propeller was just windmilling. The airplane was less than 1 mile from the runway threshold when it began to impact trees and then impacted the ground in a vertical decent. The airplane’s left wing was impact-separated.

Examination of the airplane revealed that it was equipped with D’Shannon Aviation 20-gallon tip tanks which included a fuel transfer system; however, they were not filled prior to the accident flight, and there was no fuel in the tanks. The fuel selector operated correctly in the Left, Right, and Off positions when tested with air at each port. The integrity of the fuel lines from the selector to the wing roots and firewall were verified using air. The fuel boost pump successfully operated when it was connected to the main battery. Samples of fluid from the fuel selector and boost pump were consistent with 100LL aviation gasoline. The samples were tested with water finding paste and determined to have no water present. The fuel tank filler cap O-rings were intact and not damaged. Neither fuel tank contained fuel; however, the left tank was breached, and the right tank fuel line was compromised.

The engine and propeller were separated from the airframe. The engine driven fuel injection pump was removed. The drive-coupling was found intact and undamaged. Each fuel system line was removed, drained of their remaining fluid, which was collected, and tested for water using water finding paste, which indicated no water was present. The flexible lines were then tested for obstructions with compressed air, with no obstructions noted. The fuel metering valve and throttle assembly functioned normally. The fuel manifold was disassembled and found free of contamination and functioned normally.

The upper spark plugs were removed and inspected; they were normal for operation and wear. All cylinders were tested for compression using the thumb method. All cylinders were inspected with a borescope; each cylinder showed indications of normal operation and wear. Magneto operation was observed by the sparks produced at the lead terminal springs, magneto timing was verified at 21-22 degrees before top dead center for the left and right magnetos. All the engine control cables were found attached to their respective components; however, cable continuity was breached consistent with impact damage. The exhaust mufflers were removed, inspected and each flame cone in each muffler was found intact with no blockage, the tail pipes were crushed due to impact damage. The air intake from the filter to the throttle assembly was found intact with no obstructions noted.

Cessna 172L Skyhawk, N7205Q, accident occurred on August 15, 2025, near Space Coast Regional Airport (TIX/KTIX), Titusville, Florida

 

  • Location: Titusville, FL 
  • Accident Number: ERA25LA302 
  • Date & Time: August 15, 2025, 14:15 Local 
  • Registration: N7205Q 
  • Aircraft: Cessna 172 
  • Injuries: 1 Serious, 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Instructional 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200801/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N7205Q

On August 15, 2025, about 1415 eastern daylight time, a Cessna 172, N7205Q, was substantially damaged when it was involved in an accident near Titusville, Florida. The pilot was seriously injured and the flight instructor received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

According to the pilot, a preflight inspection was performed on the airplane and fuel onboard was 17.5 gallons. After about 40 minutes of flying, they returned to the departure airport to practice touch and go landings. While in the traffic pattern on the third touch and go, the airplane was in a descent, and when the pilot attempted to add power, the engine did not respond. The flight instructor stated that he noticed the tachometer was reading 1,000 rpm, but the throttle lever was fully in. He stated that the fuel selector was on both, the mixture was in the rich position, and the carburetor heat was “on”, but the engine did not respond. The flight instructor took control of the airplane and attempted to fly back towards the runway, but the airplane contacted trees about ½ mile from the airport property.

A postaccident examination of the airplane by a Federal Aviation Administration inspector revealed several gallons of automotive fuel remained in the tanks of the airplane.

The wreckage was retained for further examination.

Tuesday, September 09, 2025

Lancair NLA-275-FR-C Super Barracuda, N345LA, fatal accident occurred on August 18, 2025, near Bradley, Arkansas

  • Location: Bradley, AR 
  • Accident Number: CEN25FA321 
  • Date & Time: August 18, 2025, 21:33 Local 
  • Registration: N345LA 
  • Aircraft: Lancair NLA-275-FR-C 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200808/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N345LA

On August 18, 2025, about 2133 central daylight time, a Lancair NLA-275-FR-C airplane, N345LA, was destroyed when it was involved in an accident near Bradley, Arkansas. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A preliminary review of ADS-B data showed the airplane departed Lakeway Airpark, Lakeway, Texas, about 2011. The airplane then proceeded on a predominant northeast course. At 2018, the airplane reached an altitude of about 10,000 ft mean sea level (msl). After about 50 minutes, the airplane began a climb to an altitude of about 12,175 ft msl. After about 18 minutes, the airplane climbed to maximum altitude of about 14,125 ft msl, followed by a descent to about 12,375 ft msl.

The airplane then began a climb from 12,375 ft msl to 12,675 ft msl, followed by a descent. About 2132 and at 11,800 ft msl, the airplane began a rapid right spiraling descent. Near the end of the descent, the data indicated that the airplane made a momentary level off and climb before a descending left turn into terrain (see figure 1).

The main wreckage of the airplane was located in wooded terrain. The initial impact point was a pine tree about 200 ft from the main wreckage. The path from the initial impact point to the main wreckage was on a true heading of 066°. The debris field from the initial impact point to the main wreckage contained fragments of the right wing.

The main wreckage was oriented with the airframe upright and the engine was inverted with a final heading of 180°. The airplane was destroyed by the impact sequence and the postimpact fire.

The wreckage was recovered from the accident site and was transported to a secure location for future examination. 

Cessna 340A RAM VI, N888MT, fatal accident occurred on August 27, 2025, near Midwest National Air Center Airport (GPH/KGPH), Mosby, Missouri

  • Location: Kearney, MO 
  • Accident Number: CEN25FA346 
  • Date & Time: August 27, 2025, 11:58 Local 
  • Registration: N888MT 
  • Aircraft: Cessna 340
  • Injuries: 2 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200880/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N888MT

On August 27, 2025, about 1158 central daylight time, a Cessna 340A, N888MT, was substantially damaged when it was involved in an accident near Kearney, Missouri. The pilot and passenger were fatally injured. The airplane operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

ADS-B data showed that the airplane departed the Washington Regional Airport (KFYG), Washington, Missouri, about 1057, and cruised at 4,500 ft mean sea level towards the Midwest National Air Center Airport (KGPH), Mosby, Missouri. About 25 miles from the airport, the airplane descended and entered the traffic pattern for a left base turn. The airplane’s altitude was lower than normal for a standard traffic pattern and continued to descend.

An eyewitness who lived near the accident site reported that the airplane appeared to be low and slow. The airplane’s left wing dipped down momentarily, returned wings level, then the left wing dipped again, and the airplane rolled left until it collided with terrain.

The airplane impacted an uncultivated soybean field about 0.6 miles from the approach end of runway 18. The initial impact point consisted of ground scars consistent with the left wing and airplane nose. A divot in the ground made by the right engine contained the right propeller assembly which had fractured at the crankshaft. The debris field was about 95 ft long, orientated along a 225° magnetic heading. The main wreckage consisted of the remainder of the airplane, to include the fuselage, empennage, tail section, both wings, both engines, and the left propeller. The main wreckage was aligned on a 120° magnetic heading. A postimpact fire had consumed a large portion of the fuselage.

On-scene examination of the airplane found that the landing gear was down, and the flaps were retracted. Flight control continuity was established from the cockpit to the flight controls. The cockpit instrumentation and electronic displays were largely destroyed in the fire.

The wreckage was retained for further examination.

Cessna 310Q, N7664Q, fatal accident occurred on August 23, 2025, near Milledgeville, Georgia

  • Location: Milledgeville, GA 
  • Accident Number: ERA25FA310 
  • Date & Time: August 23, 2025, 18:25 Local 
  • Registration: N7664Q 
  • Aircraft: Cessna 310Q 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200847/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N7664Q

On August 23, 2025, about 1825 eastern daylight time, a Cessna 310Q, N7664Q was destroyed when it was involved in an accident near Milledgeville, Georgia. The commercial pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations personal flight.

According to a witness, the pilot, who was based in Hilton Head, South Carolina, had flown to Fairfield County Airport (FDW), Winnsboro, South Carolina to obtain an instrument flight rules (equipment) recertification. Once completed, the pilot departed runway 4 at FDW about 1723 on an instrument flight rules (IFR) flight plan to Baldwin County Regional Airport (MLJ), Milledgeville, Georgia, about 130 nautical miles to the south-southwest.

Preliminary air traffic control communications and ADS-B data provided by the Federal Aviation Administration showed that after departure the pilot made a right turn and flew east for about 6 miles then made a left 360° turn to the southwest while climbing to an en route cruising altitude of about 10,000 ft mean sea level (msl). Altitudes, ground speeds and headings were consistent throughout the en route portion of the flight. As the airplane approached the initial approach fix (IBUDY) for the RNAV GPS 10 arrival to MLJ, the pilot was in communications with the Atlanta radar approach controller.

The pilot was issued a descent to 4,000 ft, provided the MLJ altimeter, and asked to verify that he was in receipt of the weather. The pilot responded with confirmation and was subsequently cleared for the RNAV Runway 10 Approach; the controller instructed the pilot to pass over IBUDY at or above 3,000 ft, which was acknowledged. There were no further transmissions from the pilot. About 10 seconds after the last communications and 6 miles east IBUDY, the airplane entered a left turn towards the south and descended. The controller advised the pilot “Low altitude alert, six four Quebec, check your altitude immediately.” The airplane continued on a track of about 120° and descended until flight track data was lost at 1821, about 6 nm west of the approach end of runway 10 at MLJ. During the descent, the airplane’s ground speed increased from 140 kts to 179 kts.

Reported weather conditions around the time of the accident showed overcast conditions around 2,200 to 2,500 ft with clouds extending to 10,000 ft. There was no precipitation activity in the area. There was a 10 to 15 knot tailwind during the last portion of the flight and the  freezing level was above 15,000 ft with no reported PIREPs in the region.

The airplane initially impacted the tops of 78-ft pine trees, then level terrain before coming to rest at an elevation of 462 ft. The wreckage path was oriented on a magnetic heading of 151° and the debris field was 135 ft wide and 660 ft long. The airplane wreckage was highly fragmented. There was no evidence of a post impact fire observed at the accident site and no evidence of an inflight fire was observed on the airplane wreckage. Tree and ground impact evidence was consistent with a slight airplane nose down wings level attitude.

Subsequent examination of the wreckage revealed that all major components of the airplane were accounted for. Elevator, rudder, and aileron flight control continuity were confirmed from the control surfaces through the cockpit controls; the control cables were traced through tensile overload breaks in the cables that exhibited a “broomstraw” appearance. The elevator trim position was measured through the actuator and corresponded to a trim setting about 5° nose up. The flap handle was in the up (retracted) position.

The fuel system components that were undamaged contained fluid with the smell and consistency of aviation fuel that was absent of contamination.

The landing gear selector was in the up (retracted) position and the landing gear actuators indicated that all 3-landing gear were retracted at the time of impact.

The instrument panel analog gauges and electronic primary flight instruments were all severely damaged by impact forces and their readings could not be observed; there was no non-volatile memory available for download.

Both engines separated from their respective wing mounts during the accident sequence. They were discovered on the last 1/3 of the wreckage path and were impact damaged. The spark plugs remained in their respective locations and the magnetos were impact-separated and located along the wreckage path.

Both propeller assemblies separated from their respective engines and were located within the wreckage path. Both 3-bladed metal propellers showed chordwise scraping on several of the blades with leading edge gouging and bends. One blade on each of the hubs, was separated and discovered within the wreckage field. The remaining propeller blades remained attached to their respective hubs.

The wreckage was retained for further examination.