Monday, September 01, 2025

Piper PA-28R-200 Cherokee Arrow II, N1147X, fatal accident occurred on August 31, 2025, near Alta, Utah

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=N1147X

Pax Flyers LLC

- Hitstory of Flight:
On August 31, 2025, at about 1721 local time, a Piper PA-28R-200 Cherokee Arrow II, N1147X, registered to Pax Flyers LLC out of Hollywood, Maryland, was substantially damaged when it was involved in an accident near Alta, Utah. One occupant sustained fatal injuries, and the second occupant sustained serious injuries.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 1655 LT, the airplane was observed climbing through 5,500 ft near Toole, Utah. The airplane was flying east and appeared to be tracking the Dwight D. Eisenhower highway. At about 1706, the airplane turned south and was still following the highway. The last ADS-B return was recorded at 1710 LT. The airplane crashed about 10 minutes later and 15 miles east of the final recorded data point. (figure 1)

Figure 1: ADS-B Exchange track on Google Earth, note presumed flight path is not confirmed.

According to two witnesses who were in the middle of their wedding save-the-date photo-shoot, they saw the airplane flying at low altitude, and stated "We couldn’t hear the engines. He was gliding and then, like, tried to pull up, and he went behind the tree lines and nothing, and just, you see a big cloud of dust."

- Pilot Information:
None

- Aircraft Information:
The accident aircraft, serial number 28R-7535259, was a 4-seat, low wing, retractable landing gear airplane manufactured in 1975. It was powered by a Lycoming IO-360-C1C engine rated at 200 hp. The certified gross weight was 2,650 lb.

According to the damage history, in 2014, the aircraft suffered loss of oil in flight and the engine was replaced with a re-manufactured engine in Jan 2016.

- Wreckage and Impact Information:
The accident site elevation was 9135.8 ft, at an estimated cords of 40.589890,-111.6202 (see figure 1).

Figure 1: Accident (left) and Google Maps (right)

The airplane came to rest upright in wooded mountainous terrain surrounded by multiple mountain tops and canyons (figure 2). There was no post crash fire. The left wing remained attached to the airframe and sustained impact damage. The right wing was impact damaged and separated and located in the debris path leading to the aircraft. The tail remained attached to the fuselage.

Given the witness accounts and the state of the wreckage (speculation/my opinion), the impact appears consistent with a box entry low altitude stall/spin/turn.

Figure 2

- Airport Information:
None

- Weather:
(1) Brief:

The reported weather at KHCR, at 1715 (about 6 minutes before the accident) included: wind 330° at 8 knots, 10 statute miles visibility, no clouds under 12,000 ft (CLR), a temperature of 29° C, a dew point of 0° C, and a barometric altimeter setting of 30.22 inches of mercury.

The reported weather at KSVR, at 1715 (about 6 minutes before the accident) included: wind 330° at 13 knots, 10 statute miles visibility, no clouds under 12,000 ft (CLR), a temperature of 30° C, a dew point of 5° C, and a barometric altimeter setting of 30.19 inches of mercury.

The calculated density altitude from the first paragraph is KHCR 12604 ft. The calculated density altitude from the second paragraph is 12753 ft. The estimated elevation of the accident site was 9135.8 feet.

(2) METARs:

METAR KSVR 312255Z AUTO 34010KT 10SM CLR 31/05 A3019 RMK AO2

METAR KSVR 312315Z AUTO 33013KT 10SM CLR 30/05 A3019 RMK AO2 <<

METAR KSVR 312335Z AUTO 33011KT 10SM CLR 30/05 A3018 RMK AO2

------------------

METAR KHCR 312255Z AUTO 26005KT 10SM CLR 29/01 A3022 RMK AO2 T02940006 $

METAR KHCR 312315Z AUTO 33003KT 10SM CLR 29/M00 A3022 RMK AO2 T02891001 $ <<

METAR KHCR 312335Z AUTO VRB04KT 10SM CLR 29/00 A3022 RMK AO2 T02930003 $

(3) Area Forecast Discussion:

According to the Area Forecast Discussion released by the NWS, Salt Lake City UT 1540 MDT Sun Aug 31 2025:

.SYNOPSIS...A warming and drying trend will continue through at
least Monday, bringing pleasant weather for the holiday weekend.
Moisture gradually increases through the week, with chances for
showers and thunderstorms increasing late in the week into next
weekend.

&&

.SHORT TERM (Through 12Z/6AM Tuesday)...Mid level ridging
centered across the Intermountain region will maintain a mild and
dry airmass through the short term period. Temperatures will
trend slightly warmer heading into Labor day, running slightly
above climo for early September. With this daytime heating,
cumulus development can be expected across the higher terrain,
and a stray afternoon shower or thunderstorms can`t be ruled out
most likely over the Uintas.

.LONG TERM (After 12Z/6AM Tuesday), Issued 405 AM Sunday...Dry,
quiet conditions will transition to more active weather as
moisture gradually increases through the long-term period,
particularly across southern Utah. On Tuesday, the ridge overhead
will shift slightly eastward as a shortwave trough well to our
west draws moisture northward mainly into eastern NV. Being on the
fringe of this moisture, southwestern Utah could see isolated
thunderstorms as early as Tuesday afternoon, with dry microbursts
as the main threat.

Moisture will continue to gradually increase across the forecast
area through the week, with PWATs reaching 110-130% of normal by
Thursday across western and central Utah. Model guidance continues
to hint at a secondary moisture increase over the weekend, though
plenty of uncertainty remains regarding its magnitude and overall
timing. As is common with monsoonal surges, the main weather
impacts will transition from dry microbursts into more of a flash
flood threat later in the week and into the weekend.

&&

.AVIATION...KSLC...The SLC terminal will see VFR conditions
through the evening with mostly clear skies. Northwest winds are
expected to shift to the southeast between 03Z and 05Z.

.REST OF UTAH AND SOUTHWEST WYOMING...The airspace will see VFR
conditions through the evening with some scattered cumulus over
the higher terrain through the early evening. Winds will be
generally light and diurnally driven.

- Additional Information:

According to the NTSB's Safety Alert, "Mastering Mountain Flying", training is essential for mountain flying safety...

The problem:

  • Pilots with limited or no training in mountain flying can be surprised about their aircraft’s different performance at high density altitude, often leading to serious or fatal accidents. 
  • Wind and other weather phenomena interacting with mountainous terrain often lead unsuspecting pilots into situations that are beyond their capabilities. 
  • Should a crash occur, a pilot who survives the crash but does not have emergency or survival gear immediately accessible may not survive the harsh environment until rescuers are able to reach the location.
What can pilots and flight instructors do? 
Through training, pilots can develop skills and techniques that will allow them to safely fly in mountainous terrain. When planning flights in mountainous terrain, pilots and flight instructors should do the following to enhance safety: 
  • Flight instructors should encourage their students to attend a quality mountain flying course before attempting flight in mountainous terrain or at high density altitudes. 
  • Pilots should consult with local flight instructors before planning a flight into mountainous terrain. Even experienced mountain pilots may not be familiar with local conditions and procedures for safe operations. 
  • Pilots should be aware that weather interacting with mountainous terrain can cause dangerous wind, severe turbulence, and other conditions that may be unsafe for aircraft, especially light GA aircraft. 
  • Pilots should consider specialized emergency and survival equipment (such as personal locator beacons in addition to a 406 emergency locator transmitter) before flying in mountainous terrain, and develop a plan for immediate access to the equipment in the event of a postaccident fire. 
  • FBO staff should be alert for customers who appear to be planning flight into mountainous terrain who could benefit from mountain flying instruction.

Friday, August 29, 2025

North American T-28B Trojan, N28XT, fatal accident occurred on August 11, 2025, near Monticello, Iowa

  •  Location: Monticello, IA 
  • Accident Number: ANC25FA086 
  • Date & Time: August 11, 2025, 15:05 Local 
  • Registration: N28XT 
  • Aircraft: North American T-28B 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200763/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N28XT

On August 11, 2025, about 1505 Central daylight time, a North American T-28B airplane, N28XT, was substantially damaged when it was involved in an accident near Monticello, Iowa. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to witnesses, the pilot reported, over the Monticello Regional Airport’s Common Traffic Advisory Frequency (CTAF), that he was experiencing a propeller governor failure, and he was returning to the airport. Shortly thereafter, he reported a total loss of engine power, and that he was attempting an emergency landing in a bean field about 2 miles Southeast of the airport (See figure 1).


During the subsequent emergency landing in the bean field, with the landing gear in the retracted position, the airplane continued along the wreckage path for about an additional 275 ft from the initial impact point.

The main fuselage, and associated debris path was oriented on about a 217° heading. The debris path between the initial impact point and the main wreckage site displayed signs of extensive fuselage fragmentation. Debris consisting of an engine oil tank and oil cooler, a propeller blade, and the accident airplane’s Wright R-1820 Cyclone 9 engine, were all found in the debris path. The airplane came to rest inverted, which resulted in substantial damage to the fuselage and wings (See figure 2).


An investigator from the National Transportation Safety Board's (NTSB) Alaska Regional Office, along with an NTSB aviation piston engine specialist, responded to the accident site and examined the airplane wreckage on August 12-14. During the detailed on-scene examination, the investigative team retained various components for additional examination and testing, and results are pending.

The wreckage has been moved to a secure site and additional postaccident examinations are pending. 

North American T-28C Trojan, N9748Y, accident occurred on August 7, 2025, near West Wendover, Utah

  • Location: West Wendover, NV
  • Accident Number: WPR25LA244 
  • Date & Time: August 7, 2025, 15:32 Local 
  • Registration: N9748Y 
  • Aircraft: North American T-28C 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200754/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N9748Y

On August 07, 2025, at 1532 Pacific daylight time, a North American T-28C, N9748Y, was substantially damaged when it was involved in an accident near West Wendover, Utah. The pilot and the passenger were seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The passenger stated that they had arrived earlier in the week for Bonneville Speed Week and the purpose of the accident flight was to return home. Prior to departure they received full fuel, and the pilot started the engine, letting it run at idle while waiting for a helicopter to depart. They departed to the southeast and the pilot initiated a gradual climb. The pilot then began a right turn to head west toward mountainous terrain.

At an estimated 700–800 feet above ground level, the airplane began to shudder, which the passenger described as feeling the vibration emanating from the front of the airplane. He did not recall any reduction in power after takeoff, and he did not smell fuel, oil, smoke, or anything unusual, nor did he hear any abnormal sounds. As the shuddering worsened, the pilot continued the right turn, which the passenger interpreted as an attempt to return to the airport. When the airplane was heading back toward the airport, the vibration became severe.

The airplane descended and impacted the ground hard, bouncing several times before coming to rest about 1.5 miles from the airport. Dust immediately filled the cockpit, obscuring his view of the pilot. The pilot was bleeding from a head wound, but regained responsiveness after a couple of minutes. Both occupants had worn seat belts, but did not wear helmets.

The airplane was manufactured in 1956 by North American as model T-28C, and was designated serial number 140551. The airplane was powered by a Wright R1820-86B 9-cylinder radial engine rated at 1,425 horsepower and equipped with a Hamilton Standard 3-bladed constant speed propeller.

Investigators conducted a post-accident examination at the recovery facility. Oil had coated the left side of the airplane, with the origin at the engine breather tube (see figure 1 below). 

An external examination of the engine revealed no evidence of an uncontained failure. Oil was observed lightly coating cylinders Nos. 1, 2, 3, and 4. The No. 4 cylinder pushrods were bent with the pushrod housing nut on the exhaust valve displaced (see figure 2 below). 

Removal of the forward spark plugs revealed that cylinders Nos. 4, 6, and 7 were oil-soaked. The No. 6 forward spark plug was not torqued in the cylinder bore and was loose to rotate out of the cylinder. Investigators were unable to rotate the engine by applying force on the propeller blades. Investigators removed cylinder No. 4, providing an internal view of the crankcase. The articulating rods for Nos. 4, 5, and 6 were fractured at the master rod end. The corresponding cylinder skirts were damaged with grooves similar in dimension to the respective articulating rod, consistent with repeated contact between the skirt wall and the broken rod in the same plane. The articulating-rod journals on the master rod were not oil-covered (dry). The counterweights showed gouges on the outer portion of the shoe. Metallic debris was present on the aft side of the pistons and throughout the case.

The cylinder No. 4 articulating rod remained attached to the piston pin (see figure 3 below). The No. 4 piston face was dark with carbon, consistent with normal operation. The valves appeared normal with no evidence of piston-to-valve contact. The valve reliefs on the exhaust valve displayed a gouge consistent with the radius. The No. 4 piston was stuck in place and could not be freed.

The oil reservoir tank contained only a trace amount of oil with slight metallic debris on the bottom. The Cuno oil filter was removed and revealed fine metallic particles. The high-pressure oil strainer screen was removed and revealed coarser metallic particles (see figure 4 below). The metallic debris was both ferrous and non-ferrous, with mostly non-ferrous debris, indicative of aluminum, and there was additionally gold color flecks. The airplane was not equipped with an after-market “clean kit” or Whittaker valve, nor was it required.

The oil sump pump was removed; the gears were intact, and rotational scoring was noted on the gear vanes and surrounding housing with metallic particles present. The sump chip detector was coated with metallic particles. The chip detector on the supercharger had fine particles, but the screen was clean. Continuity was obtained on both chip detectors. The oil chip light in the cockpit was intact with no stretch noted in the filament. Continuity was obtained between the light and the cannon plug to the sump gear detector, indicating that it would have been operational. The oil shutoff poppet valve and spring on the oil pump housing appeared intact and operational.

Van's RV-6A, N692AC, accident occurred on August 19, 2025, near Centerview, Missouri

  • Location: Centerview, MO 
  • Accident Number: CEN25LA327 
  • Date & Time: August 19, 2025, 16:40 Local 
  • Registration: N692AC 
  • Aircraft: MARSHALL ALLEN L RV6A 
  • Injuries: 1 Minor, 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200826/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N692AC

On August 19, 2025, at 1640 central daylight time, a Vans RV-6A airplane, N692AC, was substantially damaged when it was involved in an accident near Centerview, Missouri. The commercial pilot sustained minor injuries and the passenger was uninjured. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 personal flight.

The pilot stated there were no issues with the engine runup prior to the accident flight. He stated that this was his first flight in the make and model of accident airplane which was to familiarize himself with the airplane. After performing several maneuvers at 4,500 ft msl, he began to fly towards Skyhaven Airport (RCM), Warrensburg, Missouri. He said the engine sounded normal, but it was not producing power. He planned on continuing the flight to RCM where he now planned on performing a magneto check and to “recheck the engine.” About 3 miles from RCM, he performed the before landing checklist, changed the fuel tank selection, turned the fuel pump on, and confirmed the fuel mixture control was in the rich position. He reduced the throttle control about ¼ inches, heard a “slight pop,” and the engine lost power. He then changed the fuel tank selection, confirmed the fuel pump was on, and adjusted the engine throttle control, but was unable to regain engine power. He then changed fuel tank selection to the right fuel tank, added wing flaps, and performed a forced landing to a cornfield. He stated that the airplane, which was not equipped with a stall warning system, stalled above the corn during landing, and the airplane impacted the ground. The airplane sustained substantial damage to the fuselage.

The airplane was retained for examination.

Piper PA-18-150 Super Cub, N476SM, accident occurred on August 14, 2025, in Joliet, Illinois

"Yeah he can't park there" - Beau Klingbeil; FAA Inspector; Chicago, IL"

  • Location: Joliet, IL
  • Accident Number: CEN25LA322 
  • Date & Time: August 14, 2025, 17:14 Local 
  • Registration: N476SM 
  • Aircraft: Piper PA-18-150 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Banner tow 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200810/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N476SM

On August 14, 2025, at 1714 central daylight time, a Piper PA-18-150 airplane, N476SM, was substantially damaged when it was involved in an accident near Joliet, Illinois. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 banner tow flight.

The pilot reported that he fueled the airplane and departed for a planned 3-hour banner tow flight in and around the Joliet area. About two hours into the flight, he heard a “loud bang” from the engine, which resulted in strong vibrations and a gradual loss of engine power. Shortly after, the engine experienced a total loss of power, and the pilot executed a forced landing to a field. During the landing roll, the airplane ground looped and impacted a fence, which resulted in substantial damage to the left elevator.

The responding FAA inspector reported that there was engine oil on the bottom of the fuselage from the engine cowling to the empennage. There was also oil leaking from the engine exhaust pipe.

Postaccident examination of the engine revealed that the No. 2 cylinder exhaust valve failed. Most of the valve stem remained inside the valve guide while the valve head was destroyed inside the cylinder. There were no other engine mechanical malfunctions or anomalies that would have precluded normal operation.  

Cirrus SR22 GTS G2, N412DJ, accident occurred on August 7, 2025, near Jaroso, Colorado

  • Location: Jaroso, CO
  • Accident Number: CEN25LA310
  • Date & Time: August 7, 2025, 09:35 Local
  • Registration: N412DJ
  • Aircraft: CIRRUS DESIGN CORP SR22
  • Injuries: 2 Serious, 1 Minor
  • Flight Conducted Under: Part 91: General aviation - Instructional

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200736/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N412DJ

On August 7, 2025 at 0935 mountain daylight time, a Cirrus SR22 airplane, N412DJ, was substantially damaged when it was involved in an accident near Jaroso, Colorado. The pilot receiving instruction and a passenger were seriously injured, and the flight instructor was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 instructional flight.

The pilot reported that the purpose of the flight was to perform engine lean test procedures. During cruise flight at an altitude of 10,500 ft msl, the pilot reported they had already completed one lean test per the instructions and were starting a second test when the engine suddenly lost power. The instructor attempted to restart the engine by performing the emergency loss of engine power checklist but was unsuccessful in restarting the engine. They chose to activate the Cirrus Airframe Parachute System (CAPS) due to the lack of nearby airports. The CAPS deployed the parachute about 1,500 ft agl, and the pilot reported they were under canopy for about 20 seconds before the airplane landed hard which resulted in substantial damage to the fuselage and both wings.

The airplane was retained for further examination.

Van's RV-4, N595BS, accident occurred on August 6, 2025, near Elgin, Illinois

  • Location: Elgin, IL
  • Accident Number: CEN25LA309 
  • Date & Time: August 6, 2025, 19:25 Local 
  • Registration: N595BS 
  • Aircraft: Vans RV4 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200735/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N595BS

On August 6, 2025, about 1925 central daylight time, a Vans RV4 airplane, N595BS, was substantially damaged when it was involved in an accident near Elgin, Illinois. The pilot and passenger were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot reported that during cruise flight at 1,000 ft above ground level, he noticed an increase in electrical voltage. He turned the airplane toward the departure airport and noted the voltage indicated 20 volts before the entire instrument panel lost power, and then the engine lost power. He also noticed a small smoke plume from behind the instrument panel. The pilot made a forced landing to a golf course during which the airplane sustained substantial damage to the fuselage and engine mount.

The engine was equipped with two E-Mag electronic ignition systems. Both magnetos were retained for further examination.

Devices capable of recording data were sent to the NTSB Vehicle Recorders Laboratory for further analysis.

The airplane was retained for further examination.