Wednesday, July 16, 2025

Beechcraft F35 Bonanza, N5009B, fatal accident occurred on July 6, 2025, near Eagle Nest, New Mexico

  • Location: Eagle Nest, NM 
  • Accident Number: WPR25FA205 
  • Date & Time: July 6, 2025, 13:45 Local 
  • Registration: N5009B 
  • Aircraft: Beech F35 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

On July 6, 2025, about 1345 mountain daylight time, a Beech F35, N5009B, was destroyed when it was involved in an accident near Eagle Nest, New Mexico. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot lived in the town of Eagle Nest but worked in the Hobbs area of Southern New Mexico. His routine was to fly home in the airplane every three weeks, landing at Angel Fire airport (AXX), and on July 4th he made the trip home to celebrate the holiday.

He had planned to return to Hobbs on July 6th, and because it was a Sunday and the Fixed Base Operator was closing early, he returned to refuel the airplane in the morning. He asked the lineman to refuel the airplane to capacity, and 28 gallons of fuel was added.

The pilot returned to the airport just after noon with family members, and after loading the airplane, he departed about 1330. According to the pilot’s wife, when they arrived, the airport was surrounded to the north, east, and west by towering storm clouds, and the south was obscured by a wall of grey clouds. She became concerned that the weather would not be safe for flight, but the pilot stated that he was able to monitor it with his ForeFlight application and if it became dangerous, he would return to the airport.

Witnesses stated that they observed the pilot perform work to the nose gear of the airplane prior to departure. The pilot’s wife stated that this was not unusual, because the nose gear strut had developed a leak, and he would often service it with air. She observed the takeoff, which was to the north, and reported that it was uneventful.

Angel Fire Airport was within a 5-mile-wide valley at an elevation of 8,380 ft msl. It was bound by mountain peaks reaching 11,721 ft to the east, and 13,161 ft to the west. According to family, after departure the pilot typically flew to the Eagle Nest Damn just to the north, and followed Cimarron Canyon through to the lower plains, about 20 miles east. From there he would fly south to Hobbs (see figure 1).

Due to the terrain surrounding the airport, there was no radar available, and review of the airplane’s flight history indicated that its ADS-B system was not operating consistently during the months leading to the accident.

Family members became concerned when the pilot did not arrive in Hobbs later that day and an alert notice (ALNOT) was issued with the FAA. The airplane was located two days later, about 10 miles northeast of AXX.

The airplane came to rest on a 30° slope at an elevation of 9,932 feet msl, at the end of a box canyon. It was about 500 ft below, and 2 miles west, of Cimarroncito Peak.

The area was composed of loose rock, and tightly spaced pine and aspen trees reaching about 75 ft in height. All the airplane’s primary structure and flight control surfaces were accounted for at the accident site and were within a 50 ft diameter of the main wreckage.

The first identified point of impact was to the tops of three trees, which had their crowns severed by about 5 ft. Sections of bark had been stripped from the south and west faces of the trees, with fragments of wing skins at their bases. The outboard section of the left wing was located in the branches of one tree. A 10 ft wide and 18-inch-deep ground disruption containing both propeller blades was located about 25 ft northeast of the first impact point. The tail section came to rest on top of the disruption, with the cabin and right wing just to the north. With the exception of the left wing located in the tree, and the outboard section of the right wing, almost the entire airplane had been consumed by fire, with only steel remnants and burnt aluminum and plastic fragments remaining.

Cessna 208B Supervan 900, N716MM, accident occurred on July 2, 2025, at Cross Keys Airport (17N), Monroe, New Jersey

  • Location: Monroe, NJ
  • Accident Number: ERA25LA254 
  • Date & Time: July 2, 2025, 17:29 Local 
  • Registration: N716MM 
  • Aircraft: Cessna 208 
  • Injuries: 12 Serious, 3 Minor 
  • Flight Conducted Under: Part 91: General aviation - Skydiving

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N716MM

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200453/pdf

On July 2, 2025, about 1729 eastern daylight time, a Cessna 208B, N716MM, was substantially damaged when it was involved in an accident near Monroe, New Jersey. The two commercial pilots and 10 passengers were seriously injured, while three passengers incurred minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 skydive flight.

Due to their injuries, the pilots could not initially provide a statement. According to airplane and fueling records, the accident flight was the second flight of the day. The airplane was fueled with 44.9 gallons of Jet-A, bringing the total fuel load to 800 lbs. It was then flown on an 18-minute skydive flight uneventfully. That flight departed at 1623, and the accident flight departed at 1714, with 700 lbs. of fuel onboard.

According to preliminary ADS-B information provided by the Federal Aviation Administration (FAA), along with witness statements, during climb, about 3,000 ft mean sea level, the pilot reported a loss of engine power and attempted to glide the airplane back to runway 27 at Cross Keys Airport (17N), Cross, New Jersey. Runway 27 was 3,500 ft-long, 50 ft-wide, and consisted of asphalt. The airplane approached the runway fast, floated, and touched down near the end. It traveled off the end of the runway and collided with trees about 700 ft beyond the runway. It then traveled about 250 ft through the trees, coming to rest upright.

Postaccident examination of the wreckage at the accident site revealed substantial damage to the fuselage and wings. Three of the four propeller blades had separated, while the remaining blade was in a feathered position. The wreckage was subsequently recovered from the accident site and examined in further detail. Both sides of the fuselage were crushed inward. The cabin left side bench seat and right side bench seat remained intact, with the two aft legs of the left bench seat separated. The pilots’ five-point harnesses and the 17 harnesses for the bench seats in the cabin remain intact; some were cut by rescue personnel. Both wing fuel tanks and the reservoir header tank were breached; however, .5 gallon of fuel was able to be recovered from the breached reservoir header tank. The fuel was clear and absent of any visible debris. The flaps and flap jackscrew were found in the fully extended position. A multifunction display was recovered from the cockpit and retained for data download.

A cursory examination of the (TPE331) engine was performed before it was prepared for shipment to a manufacturer facility for further teardown examination. Rotation of the propeller confirmed drivetrain continuity to the power section, gearbox scavenger pump, and accessory pad. The metal chip detector was removed, and no debris was observed. Approximately 8 ounces of fuel was drained from the fuel line to the engine fuel pump fuel filter bowl. The fuel was clear and absent of any visible debris.

ICP Savannah SRL, N5000S, accident occurred on June 30, 2025, near Magnolia Airpark (LS77), Slaughter, Louisiana

  • Location: Slaughter, LA
  • Accident Number: CEN25LA233 
  • Date & Time: June 30, 2025, 19:32 Local 
  • Registration: N5000S 
  • Aircraft: ICP SRL SAVANNAH S 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200467/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N5000S

On June 30, 2025, about 1932 central daylight time an I.C.P. Srl Savannah S light sport airplane, N5000S was substantially damaged when it was involved in an accident near Slaughter, LA. The pilot and passenger were not injured. The flight was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

According to the pilot, prior to the accident flight, the flap position indicator failed to function. The pilot said that immediately after takeoff, the flaps would retract, and he was unable to lower them for landing. When he tested the flaps on the ground, they would work.

On the morning of the accident, the pilot performed maintenance on the flap motor and determined that the flap potentiometer was secure. He adjusted the alignment of the flaps using a rigging protractor. After the maintenance was performed, the flaps were able to be lowered and raised between 0°, 15°, and 30°. The flap indicator also displayed proper flap position.

The pilot reported that he wanted to check the flaps while flying, so he taxied to runway 36 at Magnolia Airpark (LS77) in Slaughter, Louisiana, set the flaps to 15° for a normal takeoff, added full throttle, right rudder, and departed the runway. Immediately after the airplane became airborne, the nose pitched up steeply, the airplane veered to the left, and it would not climb. The pilot lowered the nose of the airplane and turned the airplane back toward the runway. The airplane stalled about 10 ft above the ground and then impacted a child’s play structure. The wings, fuselage, and empennage sustained substantial damage.

The airplane was retained for further examination.

Tecnam P2010 Mk II, N258CM, accident occurred on June 26, 2025, near Draughon-Miller Central Texas Regional Airport (TPL/KTPL), Temple, Texas

  • Location: Temple, TX 
  • Accident Number: CEN25LA225 
  • Date & Time: June 26, 2025, 11:30 Local 
  • Registration: N258CM 
  • Aircraft: Tecnam P2010 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200412/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N258CM

On June 26, 2025, about 1130 central daylight time, a Tecnam P2010 airplane, N258CM, was substantially damaged when it was involved in an accident near Temple, Texas. The flight instructor and student pilot were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The flight instructor reported that he had completed a preflight inspection, engine run-up, and two touch-and-go landings with no anomalies noted. During the third traffic pattern, while on the downwind leg, the flight instructor switched the fuel selector from the left tank to the right tank. He then verified that the electric fuel pump was on, and the engine instruments were indicating normal. While configured for landing on final approach, the flight instructor noticed an uncommanded change in manifold pressure. He took over the flight controls from the student pilot and moved the throttle lever full forward with no change to the manifold pressure. The flight instructor reported that there were no associated warning or caution crew alerting system (CAS) messages. The flight instructor switched the fuel selector to the left tank in an attempt to restore engine power, however, there was no change. Unable to make the runway, the flight instructor executed a forced landing into a wooded area near the airport perimeter. During the forced landing, the airplane sustained substantial damage to both wings, the fuselage, and the horizontal stabilator.

The airplane was recovered for further examination.

Van’s RV-9, N696WG, accident occurred on June 23, 2025, near Morgan Hill, California

  • Location: Morgan Hill, CA 
  • Accident Number: WPR25LA188 
  • Date & Time: June 23, 2025, 12:17 Local 
  • Registration: N696WG 
  • Aircraft: FILBY GERRY RV-9 
  • Injuries: 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N696WG

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200384/pdf

On June 23, 2025, about 1217 Pacific daylight time, an experimental amateur-built Vans Aircraft Inc RV-9 airplane, N696WG, was substantially damaged when it was involved in an accident near Morgan Hill, California. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that about 4,500 ft mean sea level, the airplane’s engine made a pronounced sound for about 2 seconds, and then both the oil pressure and fuel pressure rapidly decreased to zero. The engine initially continued to operate, but shortly afterwards lost all power. Unable to make it to an airport, the pilot made a forced landing on an open field. During the landing sequence, the pilot maneuvered the airplane to avoid a sports track, and one of its wheels struck a berm which resulted in substantial damage to the wings.

The airplane was recovered and retained at a secure facility for further examination. 

Piper PA-22-150 Tri-Pacer, N3609Z, accident occurred on June 30, 2025, near Chinitna Bay, Alaska

  • Location: Chinitna Bay, AK 
  • Accident Number: ANC25LA060 
  • Date & Time: June 30, 2025, 16:30 Local 
  • Registration: N3609Z 
  • Aircraft: Piper PA-22-150 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 
https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N3609Z

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200440/pdf

On June 30, 2025, about 1630 Alaska daylight time, a Piper PA 22-150 airplane, N3609Z, was substantially damaged when it was involved in an accident near Chinitna Bay, Alaska. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that, while en route he heard two or three loud “thuds” followed by reduced rudder control. He said that the airplane began to yaw back and forth and increased when he added engine power. The pilot made the decision to perform a precautionary landing on a remote beach. During the landing the right wheel touched down first, and the airplane veered to the right. The pilot said that he had no rudder control and attempted to correct with left aileron to no avail, subsequently the airplane nosed over. The airplane sustained substantial damage to both wings, lift struts and rudder.

Examination of the airframe is pending the recovery of the wreckage. 

Rans S-14 Airaile, N981CS, fatal accident occurred on June 30, 2025, near Guthrie, Oklahoma


Note: The NTSB did not travel to the scene of this accident.
  • Location: Guthrie, OK 
  • Accident Number: CEN25LA229 
  • Date & Time: June 30, 2025, 20:54 Local 
  • Registration: N981CS 
  • Aircraft: RANS S-14 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 
https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N981CS

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200436/pdf

On June 30, 2025, about 2054 central daylight time, a Rans S-14 airplane, N981CS, was substantially damaged when it was involved in an accident near Guthrie, Oklahoma. The non-certificated pilot was fatally injured. The airplane was  operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A witness reported that he told the non-certificated pilot that he was not allowed to fly the airplane and that he was only supposed to taxi the airplane. About 2015 the non-certificated pilot began to practice taxiing the airplane on the private airstrip. The witnesses stated that about 39 minutes had passed, and he no longer heard the airplane.

Witnesses and several others began to search for the airplane; subsequently it was found crashed in a field about 1/2 mile west of the private airstrip with the engine still idling.

The airplane was recovered for further examination.

Landing gear collapse: Velocity 173 Elite RG, N160MH, accident occurred on January 5, 2025, at Norfolk International Airport (ORF/KORF), Norfolk, Virginia

  • Location: Norfolk, Virginia 
  • Accident Number: ERA25LA090 
  • Date & Time: January 5, 2025, 15:26 Local 
  • Registration: N160MH 
  • Aircraft: HINSON MELVIN J VELOCITY 
  • Aircraft Damage: Substantial 
  • Defining Event: Landing gear collapse 
  • Injuries: 3 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/199507/pdf

https://data.ntsb.gov/Docket?ProjectID=199507

At the conclusion of an uneventful cross-country flight, the pilot of the experimental amateur-built airplane entered the traffic pattern at the destination airport and extended the airplane’s landing gear. He then observed a normal “down and locked” indication on the airplane’s avionics and continued the landing approach. The pilot described that the wind was coming from the right during the approach, with a reported velocity of about 6 knots, gusting to 18 knots. Shortly after touching down on the runway, the pilot described that there was an abnormal vibration, after which he lost directional control of the airplane. He responded by applying full rudder and brake in an attempt to counter the crosswind. The airplane continued in an uncontrolled slide and drifted left until it came to rest at the left edge of the runway. The airplane’s main landing gear collapsed during the accident sequence and the lower aft and left side of the fuselage were substantially damaged. Additionally, the nose landing gear’s wheel separated at the fork during the accident sequence. Postaccident examination of the landing gear extension/retraction system revealed that it operated normally. 

- Probable Cause: A landing gear collapse during landing in gusty crosswind conditions.

Wildlife encounter (non-bird): Cessna 172S Skyhawk SP, N885GT, accident occurred on December 11, 2024, at Jackson County Airport (JCA/KJCA), Jefferson, Georgia

  • Location: Jefferson, Georgia 
  • Accident Number: ERA25LA078 
  • Date & Time: December 11, 2024, 20:00 Local 
  • Registration: N885GT 
  • Aircraft: Cessna 172 
  • Aircraft Damage: Substantial 
  • Defining Event: Wildlife encounter (non-bird) 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Instructional 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/199429/pdf

https://data.ntsb.gov/Docket?ProjectID=199429

The flight instructor stated that after completion of a night practice instrument approach, they continued to the runway to perform a touch-and-go landing. As the main landing gear touched down on the runway, three deer ran in front of the airplane. The flight crew aborted the landing and then heard a loud “bang” when the airplane’s nose landing gear struck one of the deer as the airplane ascended. The underside of the fuselage was substantially damaged as a result of the collision. The pilot continued the departure, notified air traffic control, and landed at an alternate airport without further incident. The flight instructor reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

- Probable Cause: The airplane’s collision with a deer on the runway during landing.

Loss of control on ground: Aviat A-1B Husky, N79HY, accident occurred on October 11, 2024, at Cheat River Island Airport (56WV), Rowlesburg, Rowlesburg, West Virginia

  • Location: Rowlesburg, West Virginia
  • Accident Number: ERA25LA015 
  • Date & Time: October 11, 2024, 18:40 Local 
  • Registration: N79HY 
  • Aircraft: Aviat A1 
  • Aircraft Damage: Substantial 
  • Defining Event: Loss of control on ground 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/195314/pdf

https://data.ntsb.gov/Docket?ProjectID=195314

The pilot entered the airport traffic pattern on the downwind leg and turned onto the base and final legs for runway 31 with wind from 260° at 5 knots. A witness observed and the pilot reported a normal landing, with the airplane touching down an estimated 300 to 400 ft down the runway. The pilot stated that, during the landing roll, the airplane bounced about 3 ft then touched back down and then, with no brakes applied, the airplane began veering to the left. He attempted to correct with right rudder and right brake but the veer to the left continued and the airplane impacted trees on the left side of the runway. The pilot informed the Federal Aviation Administration (FAA) airworthiness inspector that he had not noticed any tendencies for the airplane to pull left during landings on previous flights.

Postaccident examination of the airplane by a FAA airworthiness inspector revealed substantial damage to the right wing. A check of the flight controls revealed they appeared to be intact and functioning properly. A check of the brakes was performed with no discrepancies noted. A detailed examination of the tail wheel assembly, which was installed in accordance with a supplemental type certificate, revealed it was installed in accordance with the installation requirements, with proper left and right steering springs installed and tensioned. A discrepancy with the tailwheel leaf spring not being centered was noted, but the airplane manufacturer representative reported to the FAA inspector that condition would have negligible effect on taxi operations.

- Probable Cause: The pilot’s failure to maintain directional control during the landing roll, resulting in the on-ground collision with trees.

Loss of control on ground: Cub Crafters CC19-180 XCub, N508XC, accident occurred on May 3, 2025, at Montgomery-Gibbs Executive Airport (MYF/KMYF), San Diego, California


  • Location: San Diego, California 
  • Accident Number: WPR25LA150 
  • Date & Time: May 3, 2025, 15:45 Local 
  • Registration: N508XC 
  • Aircraft: CUB CRAFTERS INC CC19-180 
  • Aircraft Damage: Substantial 
  • Defining Event: Loss of control on ground 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200124/pdf

https://data.ntsb.gov/Docket?ProjectID=200124

The pilot of a tailwheel equipped airplane reported that during landing roll, as he transitioned to taxiing, he mistakenly applied the incorrect crosswind correction. The airplane ground looped to the left and the right wing impacted the runway surface, resulting in substantial damage to the right wing and aileron. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. At the time of the accident, the pilot was landing on runway 28R with the wind from 230° at 8 knots. 

- Probable Cause: The pilot's failure to maintain directional control during landing roll.