Tuesday, September 02, 2025

Piper PA-28-180 Cherokee, N8307W, fatal accident occurred on September 1, 2025, near Dayton, Wyoming

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=N8307W

- Hitstory of Flight:
On September 1, 2025, at about 1657 local time, a Piper PA-28-180 Cherokee, N8307W, registered to a private individual out of Sheridan, WY, was substantially damaged when it impacted trees and terrain near Dayton, Wyoming. The pilot and two passengers sustained serious injuries, and one passenger sustained fatal injuries. The personal flight originated from Sheridan Airport (SHR/KSHR), Sheridan, Wyoming, and was destined to an unknown location.

According to flighttracking history, on August 30, 2025, the airplane departed Sheridan and flew to Boise Airport (BOI), Boise, Idaho, then flew another leg to Nampa Municipal Airport (MAN/KMAN), Nampa, Idaho, before returning to Boise later in the day. On August 31, 2025, the airplane departed Boise and arrived at KSHR following a 4-hour flight.

According to automatic dependent surveillance-broadcast (ADS-B) data, at 1602 LT, the airplane departed 33 at KSHR and entered a climbing left turn to an altitude of 6,300 ft. The last ADS-B return was recorded at 16:10:50 about 13.70 miles from the departure end of runway 33, the airplane was climbing through 6,700 ft. 88 knots groundspeed, with an average rate of +600 feet per minute (fpm) towards mountainous terrain. (Figure 1)

Figure 1: ADS-B data (flightaware) on Google Earth Pro

Local media reported that the aircraft was subject of an ALNOT and located sometime later in an area west of Big Mountain. The last data point was recorded roughly 2.50 miles west of Big Mountain (Figure 2). While preliminary ADS-B data can be erroneous, the available data suggests there were no attempts to avoid the mountainside.

Figure 2: Final ADS-B data point location and Big Mountain

- Pilot Information:
The pilot, aged 54, held an airline transport pilot certificate (issued/updated 11/7/2022) with a rating for airplane multi-engine land, and commercial privileges in airplane single-engine land, airplane single-engine sea, rotorcraft/helicopter and instrument helicopter. He also held a flight instructor certificate and a ground instructor certificate. His first class FAA medical was issued on July 2025. The pilot held type ratings in the Casa CA-212, DHC-8, and Dornier DO-228.

The pilot was previously a pilot for the U.S. Department of Interior. In 2012, he was involved in an incident with the potential for loss of life while flying a helicopter for the DOI, which caused approximately $120,000.00 in damage to the helicopter.

On June 30, 2016, the pilot was giving instruction to an airline transport certificated airplane multi-engine (only) pilot in the left seat when they were involved in a hard landing at Ely Airport (ELY/KELY), Ely, Nevada. Check the "additional information" section for NTSB report for the accident.

As a result of the 2016 aircraft mishap, the Office of Aviation Services (“OAS”) convened a Pilot Review Board (“PRB”) to investigate his involvement, as he was the pilot-in-command at the time of the incident. A PRB is an administrative, fact-finding proceeding, convened to assist the OAS Director in examining information relevant to the continued qualification, disqualification or reinstatement of any DOI pilot. (Dkt. 20-8 at 5.) The PRB was convened in accordance with DOI aviation policy, and Operational Procedures Memorandum 24 (OPM 24). (Dkt. 20-10.)4 The PRB was comprised of two DOI pilots and one air safety investigator

Following deliberations, on July 17, 2017, the PRB issued a unanimous recommendation in a 481-page report that the pilot authorization to fly for the DOI be permanently revoked and that he be disqualified from future service as a DOI pilot.

(Source: U.S. Courts, District of Idaho, Case No. 1:23-cv-00466-CWD)

- Airplane Information:
The accident aircraft, serial number 28-2476, was manufactured in 1965. It was a 4-seat, low-wing, powered by a single Lycoming O&VO-360 SER engine.

- Wreckage and Impact Information:
none

- Airport Information:
Sheridan Airport is a public airport located about 2 miles southwest of Sheridan, Wyoming. The airport field elevation was 4021.1 ft. The airport features two asphalt runways, runway 15/33 (8301 x 100 ft) and runway 6/24 (5039 x 75).

- Weather:
(1) Brief:

The reported weather at KSHR, at 1653 (about 5 minutes before the accident) included: winds 060 at 9 knots, 10 statute miles visibility, no clouds under 12,000 ft (CLR), a temperature of 31° C, a dew point of 4° C, and a barometric altimeter setting of 30.21 inches of mercury. The calculated density altitude was 6578 ft.

(2) METARs:

METAR KSHR 012153Z AUTO VRB04KT 10SM CLR 31/03 A3021 RMK AO2 SLP200 T03110028

METAR KSHR 012253Z AUTO 06009KT 10SM CLR 31/04 A3021 RMK AO2 SLP199 T03110039 <<

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

METAR KGEY 012153Z AUTO 02005KT 10SM CLR 32/01 A3018 RMK AO2 RAB15E24 SLP185 P0000 T03220006

METAR KGEY 012253Z AUTO 06007KT 10SM CLR 33/M01 A3016 RMK AO2 SLP179 T03281011

(3) Area Forecast Discussion:

Area Forecast Discussion
National Weather Service Billings MT
240 PM MDT Mon Sep 1 2025

.KEY MESSAGES...

- Dry and warm through Tuesday with hazy skies.

- Late Tuesday cold front brings breezy winds and a few light
  showers east into Tuesday night, and cooler temps for
  Wednesday.

- Increasing wildfire smoke Tuesday night into Wednesday.

- Breezy to windy conditions Thursday.

&&

.DISCUSSION...

Through Wednesday Night...

Satellite imagery shows strong/dry ridge over the northern
Rockies and an upstream cut off low just off the WA coast, the
latter of which is spreading some high clouds to the west half of
MT. More importantly for us is a shortwave moving through
northern Alberta that will eventually evolve into a deep upper
trough over southern Ontario/Great Lakes region. This feature will
bring us modest backdoor cooling behind a late Tuesday cold
front.

For our forecast area, conditions through Tuesday will be warm
and dry with temps in the mid 80s to lower 90s, not hot enough to
threaten daily records but still 5-10F above normal. Winds will
pick up a bit late Tuesday (15-25 mph gusts) as that cold front
drops into the high plains. Though we`ve had a stretch of "humid"
days and fairly widespread precip in recent days, the brief warm
stretch and frontal passage could promote somewhat better wildfire
activity. There may be a low risk of high-based t-storms Tuesday
afternoon, followed by a bit better chance of light showers over
the eastern half of our forecast area Tuesday night as the cooler
air backs in and combines with a hint of mid level frontogenesis
in the NW flow. However, the chance of any significant rain is
negligible for most locations with only 0.05" or less locally.

Wednesday should be cooler behind Tuesday evenings cold front with
a northeast wind prevailing. Highs will range from mid 80s west to
near 70 along the Dakota borders.

For those with wildfire smoke sensitivities...there are a large
number of active wildfires across the NW Territories of northern
Canada, with plenty of smoke. Tuesday evenings cold front could
spread some near-surface smoke into eastern MT Tuesday night into
Wednesday as winds shift to the NE-E. BT

Thursday through Sunday...

Ridge axis shifts over the Northern Rockies on Thursday. A surface
cold front will sweep through the area Thursday. This will bring
breezy to windy conditions, with wind gusts in the 20 to 40 mph
range (highest gusts in the south and east). Below normal
temperatures are forecast Thursday through Saturday, with highs
in the 70s and low 80s. Friday will be the coolest thanks to the
frontal passage on Thursday.

An upper level disturbance is depicted by deterministic models
moving under the ridge, Saturday into Sunday. There is uncertainty
on whether or not the chance for precipitation will increase.
Surface slow is shown to be south-southeasterly, but the mid-upper
level wind flow will be west-southwesterly. The surface flow from
the plains looks to be drier than the mid-upper level flow which
has monsoonal moisture. Currently, the chance for precip is low
for much of the area Saturday and Sunday. The western mountains
and foothills are the exception, with a low to moderate chance for
showers and weak thunderstorms.

High temperatures will climb back into the mid 80sF beginning
Sunday and continuing into the start of next week.

Matos
&&

.AVIATION...

VFR conditions will prevail through the forecast period. Slant
range visibility will be reduced at times due to regional wildfire
smoke. BT

(4) Sun and Moon Data:

The sun’s position at the time of the accident was about 29° above the horizon on an azimuth of 127° SE.

- Additional Information:
- 2016 Accident NTSB report:

  • NTSB Identification: GAA16CA362
  • 14 CFR Public Use
  • Accident occurred Thursday, June 30, 2016 in Ely, NV
  • Probable Cause Approval Date: 08/31/2016
  • Aircraft: CESSNA U206, registration: N9304R
  • Injuries: 3 Uninjured.

NTSB investigators used data provided by various entities, including, but not limited to, the Federal Aviation Administration and/or the operator and did not travel in support of this investigation to prepare this aircraft accident report.

The flight instructor reported that during a public-use flight in a single-engine airplane, he was providing instruction to an airline transport pilot who was only rated for multi-engine airplanes. The flight instructor further reported that the pilot receiving instruction was the pilot flying and was "fast" on final approach. During the landing flare, the airplane ballooned and bounced once. After the bounce, the flight instructor applied aft flight control pressure because he believed the airplane was going to touch down nose wheel first. The subsequent landing roll was completed without further incident. 

After loading additional passengers, the flight instructor completed the return flight to their domicile without further incident. During a post-flight inspection damage was found to the tail hook and aft fuselage area. 

Further inspection revealed that the airplane sustained substantial damage to the aft bulkhead, which was likely the result of a tail strike during the bounced landing during the previous flight. The flight instructor reported that he did not hear the tail strike during the bounced landing and he did not inspect the empennage before departing for the terminating destination. 

The flight instructor did not report any mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Probable Cause: The flight instructor's incorrect pitch control during the landing flare, which resulted in a tail strike.

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/93543/pdf

https://data.ntsb.gov/Docket?ProjectID=93543

Cessna 172N Skyhawk II, N1293F, incident occurred on September 1, 2025, near Pocatello, Idaho

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=N1293F

T-Craft Aero Club


On September 1, 2025, at about 1129 local time, a Cessna 172N Skyhawk II, N1293F, registered to 
T-Craft Aero Club out of Nampa, ID, experienced a loss of engine power and a subsequent forced landing in a field near Pocatello, Idaho. The pilot and two passengers were not injured. The cross-country personal flight originated from Logan-Cache Airport (LGU/KLGU), Logan Utah, at about 1052 LT.

Cessna 172M Skyhawk II, N61657, and Extra EA-300/LC, N330AN, fatal accident occurred on August 31, 2025, at Fort Morgan Municipal Airport (FMM/KFMM), Fort Morgan, Colorado

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=N61657

Bell Ornithopters Flying Club Inc

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N330AN

333AN LLC

- Hitstory of Flight:
On August 31, 2025, at about 1040 local time, 
a Cessna 172 Skyhawk, N61657, and an Extra EA-300/LC, N330AN, were destroyed when they were involved in a mid-air collision at Fort Morgan Municipal Airport (FMM/KFMM), Fort Morgan, Colorado. One of the occupants onboard the Extra sustained fatal injuries. The second occupant and two occupants of the Cessna survived with reported minor injuries. The Cessna was registered to Bell Ornithopters Flying Club Inc out of Eastlake, Colorado, and the Extra was registered 333AN LLC out of Castle Rock, Colorado. Both airplanes were being operated under the provisions of 14 Code of Federal Regulations (CFR) Part 91 as local personal flights. The Cessna departed Broomfield-Rocky Mountain Metropolitan Airport (BJC/KBJC), Broomfield, Colorado, and was destined to KFMM. The Extra was being operated on a local flight out of KFMM. Visual meteorological conditions prevailed.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 0943 LT, the Cessna departed runway 30R and entered a climbing right turn to an inflight cruising altitude of 7,600 ft. At 1028:26, the airplane reached waypoint DEKTE and turned right (flying the RNAV (GPS) runway 14 approach). At 1033:47, the airplane reached waypoint ECUDI and turned right and was on course with runway 14. At 1039:26, the airplane was 2 miles short of runway 14, descending through 4800 ft, 98 knots groundspeed, with an average rate of -250 feet per minute (fpm). The last ADS-B return was recorded at 1040:06, the airplane was at 4500 ft, 100 knots groundspeed, and -1344 fpm.

According to preliminary (ADS-B) data from the Extra, at 1030:06, it departed runway 36 at KFMM and proceeded to fly around the airport. At about 1039:41, the airplane joined the left pattern for runway 14. At 1040:05, the airplane was at 4975 ft, 111 knots groundspeed, when it began a base-to-final (left) turn. The last ADS-B return was recorded at 1040:19 about 0.42 miles from the runway. The airplane was at 4700 ft, 101 knots grounspeed, and descending 1400 fpm. (see figure 1)

Figure 1: ADS-B Track, note blurred out data is from Extra's departure from runway 36

The Sheriff's Office reported that the Cessna was on final approach to the airport when it was struck mid-air by the Extra.

- Wreckage and Impact Information:
The first identified point of impact was the Cessna's left wing which came to rest on the right side of the runway 14 threshold markings. There was a burnt ground scar leading to the main wreckage was measured about 175 ft. The main wreckage consisted of both airplanes, which came to rest to on the grass in the right side of the runway. Both airplanes were consumed by the post crash fire. The Extra came to rest infront of the Cessna on an 
approximately 200° heading. The entire airframe, including both wings and tail were consumed by the fire. The Cessna came to rest on its left side and on a approximately 330° heading. The fuselage (including cockpit/passenger cabin) were consumed by the post crash fire. The tail came to rest on its left and sustained impact and thermal damage. The right wing came to rest inverted to the left side of the fuselage and sustained impact damage, but appeared free of thermal damage.

Figure 2: Main Wreckage

The state of both aircraft suggests (this part is speculation) the Extra struck the left side of the Cessna and both aircraft became entangled together. The Cessna lost control and impacted the runway in a left wing low altitude, afterwards, both aircraft rotated about 180° before coming to rest and getting consumed by the post crash fire. (figure 3)

Figure 3: Likely collision course (own work/speculation)

- Pilot Information:
unknown.

- Aircraft Information:
- Cessna:

The first aircraft, serial number 17264706, was manufactured in 1975. It was a four-seat, high-wing aircraft powered by a single 160 HP Lycoming O-320-E2G engine. According to the operator's website, some equipment onboard:

Garmin G5 ADI (Attitude Display Indicator)
Garmin G5 HSI (Horizontal Situation Indicator)
Garmin GFC 500 2-Axis (Pitch & Roll) Autopilot
Garmin GAD29B GPS/Navigation Data Interface
Garmin GSB15 dual A/C USB ports two each
Garmin GTN 650 GPS/Nav/Comm System
Garmin GTX 345 Digital Transponder w/WAAS
Bendix/King KX-155 NAV/COM
PMA 6000B Audio Selector Panel w/intercom and marker beacon receiver
Digital Volt Meter
Emergency locator transmitter (ELT)
Analog exhaust gas temperature (EGT) gage
Engine pre-heater
LED taxi & landing light
Dual wing tip strobe lights
Located at hanger 168, Rocky Mountain Metropolitan Airport, (BJC) Broomfield

- Extra:

The second aircraft, serial number LC051, was manufactured in 2015. It was a two-seat, low-wing aerobatic monoplane powered by a Lycoming AEIO-580-B1A engine.

- Airport Information:
Fort Morgan Municipal Airport is a non-towered public airport located about 5 miles north of Fort Morgan, Colorado. 
The airport field elevation was 4595.3 ft. The airport was served by a single asphalt runway, runway 14/32 (5731 x 75 ft.) and two turf runways, runway 17/35 (5216 x 80 ft) and runway 8/26 (2468 x 100 ft).

A review of the Notice to Airmen (NOTAMs) system for the airport revealed there were no relevant NOTAMs to the operation of the IAC contest at the airport.

- Weather:
(1) Brief:

The reported weather at KFMM, at 1035 (about 5 minutes before the accident) included: variable winds at 5 knots, 10 statute miles visibility, no clouds under 12,000 ft (CLR), a temperature of 21° C, a dew point of 12° C, and a barometric altimeter setting of 30.31 inches of mercury. The calculated density altitude was 5999 ft.

The reported weather at KFMM, at 1055 (about 15 minutes after the accident) included: winds 000 at 0 knots gusting 10 knots, 10 statute miles visibility, no clouds under 12,000 ft (CLR), a temperature of 22° C, a dew point of 11° C, and a barometric altimeter setting of 30.31 inches of mercury.

(2) METARs:

METAR KFMM 311635Z AUTO VRB05KT 10SM CLR 21/12 A3031 RMK AO2

METAR KFMM 311655Z AUTO 00000G10KT 10SM CLR 22/11 A3031 RMK AO2

(3) Sun and Moon Data:

The sun’s position at the time of the accident was about 46° above the horizon on an azimuth of 127° SE.

- Additional Information:
no

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.