Crash of a BAe 125-700 in the Warunta

Date & Time: Jul 2, 2025
Type of aircraft:
Operator:
Registration:
N10TN
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
257085
YOM:
1979
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The airplane departed Venezuela on a flight to Honduras, carrying an unknown number of people. According to local Authorities, the flight was illegal and the crew did not receive any authorization to enter the Honduran airspace. The airplane was probably engaged in an illegal flight and is believed to have crashed while the crew attempted to land in shallow water of a swampy area located in the Warunta River. The airplane was destroyed and nobody was found on site. Honduras State Police also reported that no drugs was found in the airplane. If still operated under registration N10TN, registered to Pacific RIM Management LLC.

Crash of a Cessna 414 Chancellor of Point Loma: 6 killed

Date & Time: Jun 8, 2025 at 1230 LT
Type of aircraft:
Operator:
Registration:
N414BA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
San Diego - Phoenix
MSN:
414-0047
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The twin engine airplane departed San Diego-Lindbergh Field International Airport Runway 27 at 1225LT on a flight to Phoenix-Sky Harbor Airport, carrying five passengers and one pilot. After takeoff, while climbing, the pilot was instructed for heading 180 when he reported controllability problems. Shortly later, the airplane showed erratic altitude, speed and heading data before crashing into the Pacific Ocean off Point Loma. Few debris were found floating on water and all six occupants were killed.

Crash of a Cessna 500 Citation I off Caracas: 5 killed

Date & Time: Jun 3, 2025 at 1957 LT
Type of aircraft:
Operator:
Registration:
YV3217
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Caracas - Porlamar
MSN:
500-0187
YOM:
1974
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
Few minutes after takeoff from Caracas-Maiquetía-Simón Bolívar Airport, while climbing to an altitude of 7,000 feet, the airplane entered an uncontrolled descent and crashed into the sea off Caracas. In the afternoon of the next day, debris were found floating on water approximately 11 km north of the airport, at coordinates 10° 42' 14" N 66° 59' 00" W. On June 5, other debris were recovered at coordinates 10° 37' 00" N 66° 59' 15" W. The airplane was totally destroyed and all five occupants were killed.

Crash of a De Havilland DHC-2 Beaver off Saint-Mathias-sur-Richelieu: 1 killed

Date & Time: May 2, 2025 at 1100 LT
Type of aircraft:
Operator:
Registration:
C-FYNT
Flight Phase:
Survivors:
Yes
Schedule:
Saint-Mathias-sur-Richelieu - Saint-Mathias-sur-Richelieu
MSN:
1054
YOM:
1956
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
11000
Circumstances:
On the morning of 02 May 2025, the pilot of the float-equipped De Havilland Aircraft of Canada Limited DHC-2 Mk. I aircraft (registration C-FYNT, serial number 1054) operated by ETA Aviation & César Camp du Nord Inc. arrived at the facilities of the approved maintenance organization Aviation B.L. Inc. at the St‑Mathias Water Aerodrome (CSV9), Quebec. The pilot and the person responsible for maintenance (PRM) discussed the maintenance work that had been done on the 3 aircraft operated by ETA Aviation & César Camp du Nord Inc., which had been stored at Aviation B.L. Inc. over the winter. The weather conditions forecast for that day were suitable for conducting a flight. The aircraft was refueled so that there were approximately 79 imperial gallons of fuel on board. The occurrence aircraft was placed in the water by the pilot, with the help of a passenger (who was also a pilot), and the pilot conducted a preflight inspection. The pilot and the passenger boarded the aircraft and taxied down the river in a northeasterly direction, buckling their safety belts and performing pre-takeoff checks, including the run-up. At approximately 1100, the aircraft began its take-off run in a southwesterly direction to conduct a local private flight under visual flight rules. The pilot attempted to raise the right wing by rotating the control wheel to the left. The left wing began to lift, contrary to the pilot’s expectations. The pilot reacted by rotating the control wheel completely to the left, which only accentuated the lifting of the left wing. The aircraft then rolled to the right, the right wing touched the surface of the water, and the aircraft overturned. The passenger unbuckled his safety belt and tried, in vain, to open the door on his side. He then managed to open the window and was able to egress through it. He received serious injuries to his right arm. After catching his breath at the surface, the passenger went back under the water to try to help the pilot, but the water was very opaque and he had difficulty swimming due to his injury and wet clothing. Eyewitnesses called 911. Emergency services went to the west shore. Given that no boats were immediately available, emergency services tried throwing ropes to the passenger to help him reach the shore. The passenger ultimately had to swim to the west shore on his own, where emergency services assessed him and drove him to the hospital for treatment of his injuries. The pilot was found dead in the aircraft, with his safety belt unbuckled, when the aircraft was brought to shore later that day.
Probable cause:
On 20 October 2024, the occurrence aircraft was brought to the approved maintenance organization’s facilities. The aircraft was then stored for the winter, during which time the annual and 300-hour routine inspections were to be performed. The maintenance work began in February 2025, and while the work was being carried out, a crack that needed to be repaired was noticed in the control column. To perform the repair, the chain linking the control wheel to the aileron system cables had to be removed. After the repair was completed, the chain was reinstalled in mid-March 2025 by the apprentice who had worked on the aircraft and had removed the chain before performing the repair. When the chain was reinstalled, the ends did not match the aileron system cables, so the apprentice asked for assistance from another apprentice to fix the problem. The manufacturer’s procedures were not consulted for reinstalling the chain, and the work was not directly supervised by an aircraft maintenance engineer (AME). After the control column and chain were reinstalled, the apprentice did not check the directional movement of the ailerons. When maintenance work is completed on a flight control system, in addition to AME certification, an independent inspection must also be completed by another qualified person. The certification process and independent inspection both include verifying the assembly and its locking mechanism, as well as verifying the directional movement of the ailerons. In this case, the work was not certified before the independent inspection. Knowing that an independent inspection had to be conducted, the apprentice who performed the maintenance work asked an AME to conduct this independent inspection. During the independent inspection, the AME was reportedly interrupted, and directional movement of the ailerons was not verified. When the PRM certified all the work on 01 and 02 May 2025, the AME who had conducted the independent inspection signed the independent inspection of the flight control system with the same dates.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 400 off Hua Hin: 6 killed

Date & Time: Apr 25, 2025 at 0810 LT
Operator:
Registration:
36964
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Hua Hin - Hua Hin
MSN:
964
YOM:
2017
Flight number:
RTP964
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The airplane was engaged in a local test flight at Hua Hin Airport, carrying three passengers and three crew members. After takeoff from runway 16, while climbing, it entered an uncontrolled descent and crashed in shallow water. The airplane was destroyed and all six occupants were killed, among them three pilots, two mechanics and one engineer.
Probable cause:
It was reported that the right engine failed during initial climb.

Crash of a Honda HA-420 HondaJet in North Bend

Date & Time: Apr 7, 2025 at 0607 LT
Type of aircraft:
Registration:
N826E
Flight Type:
Survivors:
Yes
Schedule:
Saint George – South Bend
MSN:
420-00170
YOM:
2019
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing on runway 05 at North Bend-Southwest Oregon Regional Airport, the airplane was unable to stop within the remaining distance. It overran and came to rest into the Coos Bay. All five occupants were uninjured and quickly rescued. The airplane was damaged beyond repair.

Crash of a BAe 3212 Jetstream 31 off Roatán: 12 killed

Date & Time: Mar 17, 2025 at 1818 LT
Type of aircraft:
Operator:
Registration:
HR-AYW
Flight Phase:
Survivors:
Yes
Schedule:
Roatán – La Ceiba
MSN:
863
YOM:
1990
Flight number:
LNH018
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
12
Circumstances:
The twin engine airplane took off from Roatán-Juan Manuel Gálvez Airport Runway 07 shortly after sunset. While in initial climb, it entered an uncontrolled descent and crashed into the sea about one km offshore. Twelve occupants were killed and five others were rescued. It is believed that the crew encountered mechanical problems after takeoff.

Crash of a Cessna 208B Grand Caravan EX into the Norton Sound: 10 killed

Date & Time: Feb 6, 2025 at 1516 LT
Type of aircraft:
Operator:
Registration:
N321BA
Flight Phase:
Survivors:
No
Schedule:
Unalakleet - Nome
MSN:
208B-5613
YOM:
2020
Flight number:
BRG445
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
The single engine airplane departed Unalakleet Airport Runway 33 at 1538LT on a regular service (flight BRG445) to Nome, carrying nine passengers and one pilot. The airplane continued at an altitude of 7,700 feet for about 30 minutes then the pilot reduced his altitude to 5,300 feet when radar contact was lost at 1516LT. At this time, the airplane was about 70 km from the destination airport. The wreckage was found a day later on sea ice in the Norton Sound approximately 34 miles (54,7 km) southeast of Nome. There are no survivors.

Crash of a Canadair CRJ-701ER in Washington DC: 64 killed

Date & Time: Jan 29, 2025 at 2048 LT
Operator:
Registration:
N709PS
Survivors:
No
Schedule:
Wichita - Washington DC
MSN:
10165
YOM:
2004
Flight number:
AA5342
Crew on board:
4
Crew fatalities:
Pax on board:
60
Pax fatalities:
Other fatalities:
Total fatalities:
64
Captain / Total flying hours:
3950
Captain / Total hours on type:
3024.00
Copilot / Total flying hours:
2469
Copilot / Total hours on type:
965
Circumstances:
On January 29, 2025, about 2048 eastern standard time (EST), a Sikorsky UH-60L, operated by the US Army under the callsign PAT25 (Priority Air Transport Flight 25), and an MHI (Mitsubishi Heavy Industries) RJ Aviation (formerly Bombardier) CL-600-2C10 (CRJ700), N709PS, operated by PSA Airlines as American Airlines flight 5342, collided in flight about 0.5 miles southeast of Ronald Reagan Washington National Airport (DCA), Arlington, Virginia, and impacted the Potomac River in southwest Washington, DC. The 2 pilots, 2 flight attendants, and 60 passengers on board the airplane and all 3 crew members on board the helicopter died. Both aircraft were destroyed as a result of the accident. Flight 5342 was operating under the provisions of Title 14 Code of Federal Regulations Part 121 as a scheduled domestic passenger flight from Wichita Dwight D. Eisenhower National Airport, Wichita, Kansas, to DCA. PAT25 originated from Davison Army Airfield (DAA), Fort Belvoir, Virginia, for the purpose of the pilot’s annual standardization evaluation flight with the use of night vision goggles (NVGs). Night visual meteorological conditions prevailed in the area of DCA at the time of the accident. PAT25 departed DAA and landed at sites in Virginia and Maryland before the crew turned south toward Washington, DC, and was cleared by the DCA tower controller (who was working combined local control and helicopter control positions) to transition the DCA airspace via helicopter Routes 1 and 4 before proceeding back to DAA. The helicopter joined Route 1 near Cabin John, Maryland, and followed the Potomac River southbound at low altitude, passing the Key Bridge, Memorial Bridge, Tidal Basin, and Hains Point before continuing onto Route 4. At the same time, flight 5342 was approaching DCA on an instrument flight rules flight that had been uneventful during departure, cruise, and initial descent. The airplane was inbound from the south on a visual approach to runway 1 when the DCA tower controller asked the flight crew if they could accept runway 33 instead. After confirming landing performance, the crew accepted a circling approach to runway 33 and maneuvered the airplane to align with the runway 33 final approach path. While PAT25 was transitioning from Route 1 to Route 4 and flight 5342 was circling to land, the controller issued a traffic advisory to the helicopter crew about the airplane, which was south of the Woodrow Wilson Bridge. At this time, the airplane was about 6.5 nautical miles (about 7.5 statute miles) south of the helicopter’s position, and its exterior lights would have been visible in the dark among those of several other airplanes, which were on approach to runway 1 from the south. The instructor pilot onboard PAT25 stated that they had the traffic in sight and requested visual separation, which the controller approved. As the aircraft flightpaths converged near the runway 33 approach corridor about 1 1/2 minutes later (20 seconds before impact), the controller asked the helicopter crew whether they had the airplane in sight and instructed PAT25 to pass behind it; however, one of the helicopter pilots pressed the radio push-to-talk switch for 0.8 seconds while the controller was speaking, and this brief radio transmission blocked the helicopter crew from receiving the “pass behind” portion of the controller’s instruction. The instructor pilot onboard PAT25 again indicated that they had the airplane in sight and requested visual separation, which the controller approved. PAT25 continued southbound along Route 4 while flight 5342 descended on final approach for runway 33, and the aircraft collided over the Potomac River at an altitude about 278 ft above mean sea level (msl).
Probable cause:
We determined that the probable cause of this accident was the FAA’s placement of a helicopter route in close proximity to a runway approach path; their failure to regularly review and evaluate helicopter routes and available data, and their failure to act on recommendations to mitigate the risk of a midair collision near Ronald Reagan Washington National Airport; as well as the air traffic system’s overreliance on visual separation in order to promote efficient traffic flow without consideration for the limitations of the see-and-avoid concept. Also causal was the lack of effective pilot-applied visual separation by the helicopter crew, which resulted in a midair collision. Additional causal factors were the tower team’s loss of situation awareness and degraded performance due to the high workload of the combined helicopter and local control positions and the absence of a risk assessment process to identify and mitigate real-time operational risk factors, which resulted in misprioritization of duties, inadequate traffic advisories, and the lack of safety alerts to both flight crews. Also causal was the Army’s failure to ensure pilots were aware of the effects of error tolerances on barometric altimeters in their helicopters, which resulted in the crew flying above the maximum published helicopter route altitude. Contributing factors included:
• the limitations of the traffic awareness and collision alerting systems on both aircraft, which precluded effective alerting of the impending collision to the flight crews;
• an unsustainable airport arrival rate, increasing traffic volume with a changing fleet mix, and airline scheduling practices at DCA, which regularly strained the DCA ATCT workforce and degraded safety over time;
• the Army’s lack of a fully implemented safety management system, which should have identified and addressed hazards associated with altitude exceedances on the Washington, DC, helicopter routes;
• the FAA’s failure across multiple organizations to implement previous NTSB recommendations, including ADS-B In, and to follow and fully integrate its established safety management system, which should have led to several organizational and operational changes based on previously identified risks that were known to management; and
• the absence of effective data sharing and analysis among the FAA, aircraft operators, and other relevant organizations.
Final Report:

Crash of a Cessna 208 Caravan I off Rottnest Island: 3 killed

Date & Time: Jan 7, 2025 at 1600 LT
Type of aircraft:
Operator:
Registration:
VH-WTY
Flight Phase:
Survivors:
Yes
Schedule:
Rottnest Island - Perth
MSN:
208-00586
YOM:
2016
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
After takeoff from the Thomson Bay in Rottnest Island, the single engine seaplane banked left, causing the left wing tip to struck the water surface. The airplane water looped and plunged into the water, floating in a vertical attitude. Three passengers were seriously injured while one was unhurt. Two others (one Swiss and one Danish citizen) as well as the pilot were killed.