Friday, August 15, 2025

Hughes 369D, N173AL, fatal accident occurred on August 7, 2025, near Alton, Illinois

  • Location: West Alton, MO 
  • Accident Number: CEN25FA307 
  • Date & Time: August 7, 2025, 10:59 Local 
  • Registration: N173AL 
  • Aircraft: Hughes 369D 
  • Injuries: 2 Fatal 
  • Flight Conducted Under: Part 133: Rotorcraft ext. load
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200732/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N173AL

On August 7, 2025, about 1059 central daylight time, a Hughes (MD Helicopters) 369D helicopter, N173AL, was destroyed when it was involved in an accident near West Alton, Missouri. The pilot and crewmember were fatally injured. The helicopter was operated as a Title 14 Code of Federal Regulations Part 133 external load flight.

According to the available Automatic Dependent Surveillance – Broadcast (ADS-B) data for the helicopter, the pilot departed from the north bank of the river about 1025. He appeared to make three trips to the powerline support tower on the south bank of the river and then return to the original position on the north bank. The final ADS-B data point was recorded at 1035. No further ADS-B data was recorded.

A witness located on the tow vessel reported that the helicopter pilot and lineman appeared to be attempting to attach a safety marker (orange ball) to one of the power lines. The lineman appeared to be standing on the left skid, wearing a safety harness. On the second attempt, as the pilot brought the helicopter closer to the power lines at which time the tail of the helicopter struck the line.

From the witness’ vantage point, it appeared that the tailboom partially separated from the airframe with a portion of it “dangling.” The helicopter then pivoted, and the cockpit hit the line which caused sparks similar to when an electrical transformer fails. The helicopter then fell onto the barge deck and a postimpact fire ensued. The witness did not recall seeing the helicopter on fire during flight, only the sparks when the fuselage struck the line. The crew moved the tow vessel alongside the barge and used its pilothouse fire station to extinguish the fire. A subsequent inspection of the barge did not reveal any structural damage or any release of the barge contents.

The helicopter main wreckage consisted of the fuselage, engine, main rotor transmission, main rotor hub, and forward portion of the tail boom (fragmented into two sections). One main rotor blade was located about 150 ft from the main wreckage. A 7-foot segment of a second main rotor blade was located about 176 ft from the main wreckage. Finally, a main rotor blade tip, about 6-inches in length, was located about 26 ft from the main wreckage. The remaining main rotor blades and the aft portion of the tail boom, including the tail rotor and horizontal stabilizer, were not present with the wreckage and presumed to have landed in the river.

The video data recorder onboard the tow vessel was retained for examination and download. A search of the river bottom in the vicinity of the accident site using side-scan sonar equipment is planned. The helicopter wreckage was retained for possible further examination.

Beechcraft M35 Bonanza, N951T, fatal accident occurred on August 13, 2025, near Des Moines, New Mexico

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N951T

- History of the Flight:
On August 13, 2025, at about 2300 local time, a Beechcraft M35 Bonanza, N951T, registered to an airline transport pilot out of Frederick, Colorado, was destroyed when it was involved in an accident near Des Moines, New Mexico. The pilot and passenger sustained fatal injuries. The cross-country flight originated from Pueblo Memorial Airport (PUB/KPUB), Pueblo, Colorado, at about 2210 LT, and was destined to an unknown location (at the time of this writing).

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, earlier in the day, at about 1940 LT, the airplane departed Erie Municipal Airport (EIK/KEIK), Erie, Colorado, on a flight to Pueblo. The airplane landed at 2050 LT. About 1h20m later, the airplane departed runway 8L at KPUB and entered a climbing right turn to an inflight cruising  altitude 8,000 ft. The airplane was tracking south and the flight appeared uneventful.

At roughly 2253, the airplane's track stopped about 17 miles north of the Sierra Grande on both the Flightaware and ADS-B Exchange sites. However, Flightradar24 continued tracking the airplane south. At roughly 2255 LT, the airplane descended to an altitude of 7,500 ft. At 2258 LT, the airplane initiated a climb, which stopped at 7675 ft when it flew into the Sierra Grande, an extinct stratovolcano that has an elevation of 8,723 ft (see figure 1, 2, and 3).

Figure 1: Flightradar 24 end of track

Figure 2: Flightradar 24 end of track

Figure 2: The Sierra Grande (photo via wiki)

- Pilot Information:
The pilot's identity is unknown at this point. However, the current registered owner holds an airline transport certificate, with a most recent issue/update date of 7/10/2004, with a rating for airplane multi-engine land, and commercial privileges for airplane single-engine land. He also held a flight instructor certificate and a Airframe and Powerplant (A&P) certificate. His third class FAA medical was issued on July 2025.

- Aircraft Information:
The accident aircraft, serial number D-6341, was manufactured in 1960. The Beechcraft Bonanza Model M35 is a five seat, retractable gear, single engine airplane. It is powered by a Continental Motors IO-470-N, 260 horsepower engine.

According to the Pilot Operating Handbook (POH):
This airplane is approved for the following type operations when the required equipment is installed and operational as defined here in 
1. VFR day and night
2. IFR day and night
3. FAR 91 operations when all pertinent limitations and performance considerations are complied

- Wreckage and Impact Information:
unknown

- Weather:
(1) METARs:
METAR KCAO 140455Z AUTO 18008KT 10SM CLR 21/13 A3009 RMK AO2 SLP105 T02060128

METAR KRTN 140453Z AUTO 34006KT 10SM CLR A3017 RMK AO2 SLPNO

(2) NWS Info:
According to the National Weather Service Area Forecast Discussion Issued by NWS Albuquerque, NM, at 536 PM MDT Wed Aug 13 2025:

...New AVIATION...

.KEY MESSAGES...
Issued at 1133 AM MDT Wed Aug 13 2025

- Minor to moderate risk of flash flooding below burn scars
  through the work week, the becoming high this weekend into
  early next week.

- After decreasing coverage of showers and thunderstorms today,
  monsoon moisture will begin to increase again near the Arizona
  border late Thursday, and over western and central New Mexico
  Friday. Fairly rich monsoon moisture will then remain in place
  across much of the forecast area through the first half of the
  coming work week with daily rounds of scattered to numerous
  showers and thunderstorms. There will also be a risk of isolated
  flash flooding outside of burn scars Friday through next Wednesday.
Also...
.SHORT TERM...
(This evening through Thursday night)
Issued at 1133 AM MDT Wed Aug 13 2025

A downtick in shower and thunderstorm coverage with slightly above
average high temperatures is expected this afternoon and evening
due to the 593 to 594 dam upper high centroid moving from north
central AZ to western NM. Isolated coverage is expected across the
north central and Sacramento Mountains with scattered to numerous
coverage across the Gila Mountains near Glenwood and Pleasanton where
higher PWATs of around 0.9 inches will be present. Some of these
showers and storms could move into the nearby highlands resulting in
gusty and erratic winds at locations like Raton, Las Vegas and
Gallup. Any shower and thunderstorm activity in the state will taper
off after sunset with lingering mid level clouds across western and
central NM heading into the dawn.

The 592 to 593 dam upper high moves east to over the NM, CO, OK, and
TX borders Thursday afternoon. This along with a trough entering the
Pacific coast will allow for a traditional monsoon flow to setup
across AZ with far western NM on the eastern edge of this flow.
Scattered to numerous showers and storms will favor the mountains
and nearby highlands along and west of the Continental Divide, where
PWATs will be around 0.7 to 0.95 inches, with isolated to at most
scattered showers and thunderstorms across the north central
mountains and Sacramento Mountains. High temperatures will be 5 to 9
degrees above average areawide. Showers and thunderstorms taper off
around sunset with activity lingering longest near the AZ/NM
border

&&

.AVIATION...
(00Z TAFS)
Issued at 529 PM MDT Wed Aug 13 2025

Lingering SHRA/TS will focus over southwest NM this evening where
strong and erratic outflow wind gusts up to 40KT are likely. This
includes the KGUP area. Thicker mid and upper level clouds tonight
will persist thru sunrise with light winds overnight. A slightly
greater crop of SHRA/TS is expected Thursday after 1pm in the
vcnty of the high terrain and west of the Cont Dvd. This activity
will drift erratically southwest thru sunset with more strong wind
gusts and brief rain.
(3) Sun and Moon Data:
According to the United States Naval Observatory, the official sunset occurred at 1948, end of civil twilight at 2015. At the time of the accident the Sun was -32 degrees below the horizon, and the Moon was -4 degrees under the horizon.

- Additional Information:
no

Thursday, August 14, 2025

Cessna 172L Skyhawk, N2860Q, fatal accident occurred on August 14, 2025, near Lawton, Oklahoma

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N2860Q

Lawton Metropolitan Area Airport Authority


- History of the Flight:
On August 14, 2025, at about 0935 local time, a Cessna 172 Skyhawk, N2860Q, registered to the Lawton Metropolitan Area Airport Authority out of Lawton, OK, was destroyed when it was involved in an accident near Lawton, Oklahoma. The sole pilot onboard sustained fatal injuries. The local flight originated from Lawton Municipal Airport (LAW/KLAW), Lawton, Oklahoma. The exact purpose of the flight is unknown at the time of writing.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 0833 LT, the airplane departed runway 17 at KLAW and entered a climbing left turn to an altitude of 3,500 ft. At 0841 LT, the airplane started doing several loops southeast of Lawton, which continued until the end of the flight. The last ADS-B return was recorded at 0934:39 LT, the airplane was at 2375 ft, tracking north at a heading of 355.0°, 128 knots groundspeed, and descending -1600 fpm. The reported accident site was located 3.80 miles north of the last recorded data point. (figure 1)

Figure 1: ADS-B Track

- Pilot Information:

The pilot, aged 55, held an airline transport certificate, with a most recent issue/update date of 6/7/2018, with a rating for airplane multi-engine land, and commercial privileges for airplane single-engine land. He also held a flight instructor certificate and a remote pilot certificate. His third class FAA medical was issued on February 2025, with a note about wearing corrective lenses to meet vision standards at all distances. He also held a CE-500 jet type rating (SIC only).

- Aircraft Information:

The accident airplane was a 1971 Cessna 172L, Skyhawk, serial number 17259860. The Cessna Skyhawk is an all-metal airplane that incorporates a semi-monocoque fuselage and empennage design. The airplane is equipped with externally braced wings, wing flaps, a fixed-pitch propeller, and a fixed tricycle landing gear. The airplane is configured to seat four occupants and has a certified maximum takeoff weight of 2,300 lbs.

The airplane was equipped with a 150 horsepower Lycoming O-320-E2D engine. The airplane was equipped for IFR flight.

- Wreckage and Impact Information:

The airplane impacted an open field and there was no post crash fire. The initial impact was identified by a small impact crater which proceeded to the main wreckage. Several broken pieces were located in the debris path leading to the main wreckage. The main wreckage consisted of the fuselage, both wings, and tail. The fuselage and both wings sustained extensive impact damage. The wreckage was oriented on a 180° heading opposite to the initial impact point.

Photo: KSWO news edited by me

- Weather:
The departure airport reported the following conditions at the time:

METAR KLAW 141353Z 15005KT 10SM CLR 26/22 A3000 RMK AO2 SLP143 T02610222

METAR KLAW 141453Z VRB06KT 10SM CLR 29/22 A2999 RMK AO2 SLP143 T02890222 50007

Uncontained engine failure: Lancair Legacy 2000, N707MM, registered to Air Horse LLC, and being operated by Michael Patey, incident occurred on July 20, 2023, near Rochester, Minnesota

  • Location: Rochester, Minnesota
  • Incident Number: ENG23LA034
  • Date & Time: July 20, 2023, 14:42 Local
  • Registration: N707MM
  • Aircraft: HALL LESTER R LEGACY
  • Aircraft Damage: Minor
  • Defining Event: Uncontained engine failure
  • Injuries: 2 None
  • Flight Conducted Under: Part 91: General aviation - Air race/show
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/192877/pdf

https://data.ntsb.gov/Docket?ProjectID=192877

On July 20, 2023, at about 1:42pm local time, a Lancair Legacy airplane, registration number N707MM, powered by a single Pratt & Whiteny Canada PT6A-42 turbo-propeller engine experienced an uncontained engine failure while enroute from the Rapid City Regional Airport (KRAP), South Dakota to the Rochester International Airport (KRST), Minnesota. The pilot declared an emergency, started a gliding descent into KRST, and made a successful landing without power. The airplane was operated as a Title 14 Code of Federal Regulations (CFR) Part 91 flight. The pilot and passenger reported no injuries.

The teeth of the 1st stage sun gear in the reduction gearbox were ground away in the plane of the mating gear teeth of the 1st stage planet gears. The mating gear teeth of the three planet gears were battered and fractured.

Distress of the 1st stage sun gear teeth released the torque normally transferred to the propeller, causing the power turbines to overspeed and the power turbine blades to release in tension and become uncontained.

It was unknown when the last inspection of the reduction gearbox was performed. During the post incident examination of the engine at the P&WC facility, the engine was found to be in poor overall condition with missing surface protective paint and surface corrosion noted throughout the external and internal surfaces of the engine.

A review of the purchase documentation revealed that the operator knowingly purchased the engine in unserviceable condition and only performed a periodic inspection before flight.

- Probable Cause: Mechanically distressed reduction gears causing an engine overspeed and turbine blade tensile overload and subsequent uncontainment. Contributing to the uncontainment was the operator’s use of the engine after knowingly purchasing the engine in an unserviceable condition and only conducting a periodic inspection before flight.

Cessna 425 Conuest I, N425D, accident occurred on July 17, 2025, near Round Rock, Arizona

  • Location: Round Rock, AZ
  • Accident Number: WPR25LA218 
  • Date & Time: July 17, 2025, 16:00 Local 
  • Registration: N425D 
  • Aircraft: Cessna 425 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Instructional
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200588/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N425D

On July 17, 2025, about 1600 mountain daylight time, a Cessna 425, N425D, was substantially damaged when it was involved in an accident near Round Rock, Arizona. The pilot receiving instruction and the flight instructor were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The pilot under instruction and the flight instructor reported that they were about 1.5 hours into the flight from Centennial Airport (APA), Denver, Colorado to Phoenix Dear Valley (DVT), Phoenix, Arizona. They reported that during cruise flight at an altitude of about 26,000 ft msl, they heard a loud noise from the left engine, followed by an immediate and total loss of engine power. While troubleshooting the left engine, the right engine lost total power, as confirmed by the torque and engine temperature gauges. They declared an emergency with air traffic control and attempted to restart the right engine, but the primary flight display “flickered for a moment” followed by a total loss of electrical power. The pilot initiated a forced landing to an open desert area and during the landing sequence on a dry, rough surface, the main landing gear separated. The airplane came to rest upright, and the left wing sustained substantial damage.

The airplane was recovered to a secure facility for further examination

Ayres S-2R-G6 Turbo Thrush, N2239V, accident occurred on August 6, 2025, near Slayton, Minnesota

  • Location: Slayton, MN 
  • Accident Number: CEN25LA304 
  • Date & Time: August 6, 2025, 13:00 Local 
  • Registration: N2239V 
  • Aircraft: AYRES CORPORATION S2R-G6 
  • Injuries: 1 Serious 
  • Flight Conducted Under: Part 137: Agricultural

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200724/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N2239V

On August 6, 2025, about 1300 central daylight time, a Ayres Corporation S2R-G6, airplane, registration N2239V, was substantially damaged when it was involved in an accident near Slayton, Minnesota. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 agricultural flight.

The operator stated the weather conditions were favorable with clear skies and less than 10 knots of wind. The airplane was lightly loaded to about 30-40% of its total capacity. The pilot had flown about 40-50 hours in the accident airplane and had reported no previous maintenance issues. Nothing was noted in the morning pre-flight inspection of the airplane.

The pilot told the operator he was about 200 ft above the ground in a fairly flat left turn, getting lined up for the first spray pass of the flight, when the controls locked up and he could not return them to center using both hands. The pilot tried to use rudder inputs but did not have enough altitude to make the recovery. The pilot stated he had engine power and was at about 120 knots and was adamant that the airplane did not stall.

The airplane impacted terrain in a left wing low attitude and cartwheeled to a stop, which resulted in substantial damage to the fuselage, empennage, and wings.

The accident site was documented, and the airplane will be recovered to a secure facility for further examination.

Air Tractor AT-502, N9193V, accident occurred on August 10, 2025, at Klein-O'Neal Airport (IL16), Lawrenceville, Illinois

  • Location: Lawrenceville, IL 
  • Accident Number: CEN25LA313 
  • Date & Time: August 10, 2025, 13:21 Local 
  • Registration: N9193V 
  • Aircraft: AIR TRACTOR INC AT-502 
  • Injuries: 1 Minor 
  • Flight Conducted Under: Part 137: Agricultural

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200746/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N9193V

On August 10, 2025, about 1321 central daylight time, an Air Tractor AT-502, was substantially damaged when it was involved in an accident near Lawrenceville, Illinois. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 agricultural flight.

The pilot stated he was taking off with a load of product and everything seemed normal until he went to rotate; at which time the airplane did not seem to be making full power. The pilot recalled looking down at the torque gauge and saw 1,400 not the usual 1,700 and he immediately pushed forward on the throttle. He attempted to jettison the load of product, but the rubber handgrip had migrated upward on the control handle preventing easy access to the switch that normally protruded from the handgrip. He described “forcing the airplane” into the air out of ground effect to gain enough altitude to clear the road and any passing traffic off the end of the runway. Unable to maintain altitude the airplane impacted the moisture laden bean field on the opposite side of the road and came to rest inverted. The impact resulted in substantial damage to the fuselage, empennage, and wings.

The airplane was recovered back to the airport and will be examined further at a later date.