- 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
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
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.