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.

Rockwell Commander 112A, N112EF, accident occurred on July 23, 2025, at Patrick Leahy Burlington International Airport (BTV/KBTV), Burlington, Vermont

  • Location: Burlington, VT 
  • Accident Number: ERA25LA292 
  • Date & Time: July 23, 2025, 13:00 Local 
  • Registration: N112EF 
  • Aircraft: ROCKWELL INTERNATIONAL 112 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200747/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N112EF

On July 23, 2025, about 1300 eastern daylight time, N112EF, a Rockwell International 112 airplane, was substantially damaged when it was involved in an accident near Burlington, Vermont. The pilot was not injured. The flight was conducted under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot/owner departed Patrick Leahy Burlington Airport (BTV), Burlington, Vermont, about 0840, with 48 gallons of fuel, and flew to Martha’s Vineyard Airport (MVY), Martha’s Vineyard, Massachusetts. He landed about 1020. The pilot said that he planned to purchase fuel in MVY, but the wait was too long and departed back to BTV about 1104. The pilot stated that he was on the downwind leg of the airport traffic pattern for runway 10 at BTV when the engine suddenly lost power. He attempted to reach the runway but landed about 15 ft short and impacted a berm resulting in substantial damage to the left wing spar.

The airplane wreckage was retained for further examination.

Grumman G-164B AgCat, N8834H, accident occurred on July 1, 2025, near Lockport, Louisiana

  • Location: Lockport, LA 
  • Accident Number: CEN25LA231 
  • Date & Time: July 1, 2025, 11:45 Local 
  • Registration: N8834H 
  • Aircraft: GRUMMAN ACFT ENG CORSCHWEIZER G-164B 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 137: Agricultural
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200448/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?NNumberTxt=N8834H

On July 1, 2025, about 1145 central daylight time, a Grumman G-164B airplane, N8834H, was substantially damaged when it was involved in an accident near Lockport, Louisiana. The pilot received minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

The pilot reported that on the morning of the accident he had flown two previous aerial application flights in the accident airplane without issue. The outside air temperature and humidity had increased since the first two flights. During the accident flight the airplane contained about 35 gallons of fuel and about 160 gallons of liquid applicant in the hopper. The pilot descended into the target field and completed one spray pass. As he approached the end of the field he ascended and “noticed the plane not climbing as normal.” The engine gauges all showed normal indications, but the airplane would not turn or climb as expected. The airplane descended as he approached a highway, and he did not want to dump the hopper over the highway or the adjacent bayou, so he continued forward. The airplane cleared a set of powerlines next to the highway and landed hard in a field, then nosed over. The pilot egressed the airplane without further incident.

The responding FAA inspector reported that the airplane came to rest inverted in a field. The engine and propeller were mostly separated from the firewall. The upper and lower wings remained attached to the fuselage and sustained leading edge damage.

The airplane has been retained for further examination.

Piper PA-24-250 Comanche, N7412P, accident occurred on August 28, 2025, near Richmond Field Airport (69G), Gregory, Michigan

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=N3806Y

- Hitstory of Flight:
On August 28, 2025, at about 1548 local time, a Piper PA-24-250 Comanche, N7412P, registered to Espyess Aviation LLC out of Sylvania, Ohio, was destroyed when it was involved in an accident near Richmond Field Airport (69G), Gregory, Michigan. The sole pilot onboard sustained serious injuries. The personal flight originated from Charlevoix Municipal Airport (KCVX), 
Charlevoix, Michigan, and was destined to Lambertville-Toledo Suburban Airport (KDUH), Lambertville, Michigan.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 1439 LT, the airplane departed runway 27 at KCVX and proceeded to an inflight cruising altitude of 4,900 ft. At about 1546:15, the airplane entered a descent towards 69G. At 1546:55, the airplane conducted a right turn. At 1547:36, the airplane entered a tight descending 270 turn towards the south runway (runway 36) at Richmond Field. The last ADS-B return was recorded at the end of the turn as the aircraft was descending through 1150 ft, 60 knots groundspeed, with an average rate of -700 feet per minute (fpm). (figure 1)

Figure 1: ADS-B Exchange with Google Earth Pro

The airplane impacted trees and open field terrain short of the runway and was consumed by a post crash fire. The wreckage consisted of the entire airplane, which came to rest upright about 0.30 miles from the approach end of runway 31. Both wings and tail remained attached to the airframe. Downed trees near the airplane suggests it descended into trees in a wings level and nose level altitude. One propeller blade was visible in published photos from the accident site, the damage to the propeller suggests it was making little to no power on impact.

The accident aircraft, serial number 24-2600, was manufactured in 1961. It featured an all-metal monoplane of semimonocoque construction with tricycle retractable landing gear a single-engine and 4 seats. It was powered by a Lycoming O-540 reciprocating 250 hp engine.

Richmond Field Airport is a public airport located 2 miles southeast of Gregory, Michigan. It features a single turf runway 18/36 which is 2471 x 100 ft. The airport field elevation was 921 ft.

The reported weather at KOZW, at 1535 (about 13 minutes before the accident) included: wind 340° at 5 knots, 10 statute miles visibility, a scattered (SCT) ceiling at 2,700ft AGL, a broken (BKN) ceiling at 3,800ft AGL and 6,000ft AGL, a temperature of 22° C, a dew point of 15° C, and a barometric altimeter setting of 30.02 inches of mercury. The calculated density altitude was 1869 ft.

The reported weather at KOZW, at 1555 (about 7 after before the accident) included: wind 300° at 7 knots, 10 statute miles visibility, a scattered (SCT) ceiling at 2,900ft AGL, a broken (BKN) ceiling at 3,600ft AGL and 4,800ft AGL, a temperature of 22° C, a dew point of 14° C, and a barometric altimeter setting of 30.01 inches of mercury. The calculated density altitude was 1879 ft.

Thursday, August 28, 2025

Cessna 210D Centurion, N3806Y, fatal accident occurred on August 27, 2025, near Kearney Municipal Airport (EAR/KEAR), Kearney, Nebraska

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=N3806Y

- Hitstory of Flight:
On August 27, 2025, at about 2057 local time, a Cessna 210D Centurion, N3806Y, registered to Onion Crest Air LLC out of Arcadia, NE, was destroyed when it impacted terrain while on approach to Kearney Municipal Airport (EAR/KEAR), Kearney, Nebraska. The airline transport pilot and one private pilot were fatally injured. The cross-country personal flight originated from Bakko Aviation Airport (MN71), Glenwood, Minnesota, and was destined to KEAR.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 1843 LT, the airplane departed MN71 and climbed to an inflight cruising altitude of 8,000 ft. At 2034:00, the airplane started its descent towards Kearney. At 2050:12, the airplane conducted a right turn and entered a short "zigzag" motion. At 2053:29, the airplane conducted a left turn and started a descent from 4,200 ft. At 2056:08, the last ADS-B return was recorded at 3,500 ft, 124 knots groundspeed, with an average rate of -900 feet per minute (fpm). Flightaware was able to track the airplane for another minute. The last data point on that site was recorded 6 miles north of the approach end of runway 13 at 2,500 ft, 135 knots groundspeed, an average rate of -2000 fpm. (figure 1)

Figure 1: ADS-B Exchange data on Google Earth Pro

There were no known witnesses to the accident. The airplane was subject of an ALNOT and located 12 hours later.

- Pilot Information:
The first occupant, aged 77, held a private pilot certificate (issued /updated 9/26/2022) with a rating for airplane single-engine land and an instrument rating. There was no available information regarding a FAA medical/BasicMed

The second occupant, aged 72, held an airline transport pilot certificate (issued/updated 8/8/2006) with a rating for airplane multi-engine land, and commercial privileges in airplane single-engine land. His first class FAA medical was issued on January 2025, with a note that he must wear corrective lenses to meet vision standards at all required distances.

- Aircraft Information:
The accident airplane, serial number 21058306, was manufactured in 1964. It was six-seat, high-performance, retractable-gear, single-engined, high-wing airplane powered by a Continental O-470 engine.

According to the Pilot Operating Handbook (POH), "Operations Authorized" section:

"With standard equipment, the airplane is approved for day and night operation under VFR. Additional optional equipment is available to in- crease its utility and to make it authorized for use under IFR day and night. An owner of a properly equipped Cessna is eligible to obtain ap- proval for its operation on single-engine schedule airline service under VFR. Your Cessna Dealer will be happy to assist you in selecting equipment best suited to your needs."

- Wreckage and Impact Information:
unknown

- Airport Information:
Kearney Municipal Airport is a non-towered public airport located 4 miles northeast of Kearney, Nebraska. The airport field elevation was 2131.8 ft msl. The airport had two runways: runway 18/36 (7094 ft by 100 ft, concrete) and runway 13/31 (4498 ft by 75 ft, asphalt).

- Weather:
(1) Brief:

The reported weather at KGPH, at 2056 (about 1 minutes before the accident) included: wind 150° at 8 knots, 10 statute miles visibility, an overcast (OVC) ceiling at 500 ft, a temperature of 18° C, a dew point of 18° C, and a barometric altimeter setting of 30.11 inches of mercury.

(2) METARs:

METAR KEAR 280056Z AUTO 16006KT 9SM OVC007 18/18 A3011 RMK AO2 SLP187 T01830178

METAR KEAR 280113Z AUTO 16007KT 10SM OVC005 18/18 A3010 RMK AO2 CIG 004V008 

METAR KEAR 280156Z AUTO 15008KT 10SM OVC005 18/18 A3011 RMK AO2 SLP185 T01830178 <<< 

METAR KEAR 280225Z AUTO 16008KT 7SM OVC003 18/18 A3011 RMK AO2

METAR KEAR 280256Z AUTO 16007KT 6SM BR OVC003 18/18 A3013 RMK AO2 SLP192 T01780178 53008

(3) Area Forecast Discussion:

According to the Area Forecast Discussion released by the National Weather Service for Hastings NE on 625 PM CDT Wed Aug 27 2025:

.KEY MESSAGES...

- Unseasonably cool for the whole 7 day forecast. Highs
  generally in the 70s, briefly warmer Tuesday, but still below
  normal.

- Low clouds and fog potential tonight especially for areas
  along and southwest of a line from Broken Bow, NE to Beloit,
  KS. Some areas could see dense fog (<1/4 mile), especially
  along and west of Highway 183 in Nebraska and Kansas.

- Scattered off and on rain chances for much of the area.
  Tonight, Rain/thunderstorms will largely stay south of the
  Kansas and Nebraska border. 50% chance of scattered showers
  for Saturday and Sunday across the area.

&&

.DISCUSSION...
Issued at 220 PM CDT Wed Aug 27 2025

Weak upper level flow is present across the Central Plains and
across the West. The area remains under northwesterly flow,
allowing any weak disturbance that moves across the area to
bring a potential for weak scattered showers or thunderstorms.
At the surface, forcing is generally weak as well, providing
generally light winds. Lee troughing this afternoon is the
biggest contributor, but that will weaken this evening as the
system slides southward.

Cloud cover will dominate the next 24 hours for most.  This evening
thunderstorms are expected to develop in the high plains of eastern
Colorado and the Nebraska Panhandle, before tracking eastward
overnight, primarily across Kansas.  There is some potential (30-
50%) that areas between I-80 and the NE/KS state line could see some
rain, but by far the best chance (>70%) will reside south of the
KS/NE state line.  MUCAPE is generally less than 500 J/kg, so severe
storms are not expected.

Tonight, the main hazard to be aware of is the potential for fog,
some of it could be dense.  Reduced visibilities are possible
primarily along and southwest of a line from Broken Bow, NE to
Beloit, KS.  Dense fog is possible with less than a quarter mile
along and west of Highway 183 in Nebraska and Kansas.

Rain chances increase for the weekend, as a disturbance slides
southeast across the area.  Without strong upper level forcing, this
disturbance will impact the area throughout the weekend. Generally
speaking, there is a 30-50% chance of showers impacting the whole
area Saturday and Sunday, peaking Saturday night into Sunday
morning. Rainfall amounts will generally be between 0.25-0.50
inches, with only a 25-33% chance of rainfall amounts exceeding
1.00 inch.

Labor Day will be near 80 degrees with clearing clouds and light
winds.  Enjoy the day.  The warmest day in the current forecast
period is Tuesday with highs in the low 80s.  Temps are generally
near to slightly below normal for the rest of the work-week before
warming for the next weekend.

&&

.AVIATION /00Z TAFS THROUGH 00Z FRIDAY/...
Issued at 621 PM CDT Wed Aug 27 2025

For KGRI/KEAR Airports:

MVFR ceilings already into both KEAR and KGRI this
evening and those will continue to lower through the
night with IFR to LIFR conditions by morning. Fog will
also develop, probably favoring the Kearney area more
so than Grand Island, but visibilities will also
drop to less than 2 miles or even 1 mile at times
after midnight. A slightly steadier south winds will
become light and variable overnight. No precipitation
is expected though there may be a few sprinkles to the
west of Kearney this evening.
(3) Sun and Moon Data:
According to the United States Naval Observatory, the official sunset occurred at 2015, end of civil twilight at 2045. At the time of the accident the Sun was -8 degrees below the horizon, and the Moon was 11 degrees over the horizon.

- Additional Information:
no

Piper J3C-65 Cub, N5050R, fatal accident occurred on July 25, 2025, at Dillingham Airport (DLG/PADL), Dillingham, Alaska

  • Location: Dillingham, AK 
  • Accident Number: ANC25FA079 
  • Date & Time: July 25, 2025, 09:16 Local 
  • Registration: N5050R 
  • Aircraft: Piper J3C-65 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200633/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N5050R

On July 25, 2025, about 0916 Alaska daylight time, a Piper J3C-65 airplane, N5050R, was substantially damaged when it was involved in an accident near Dillingham, Alaska. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to witnesses, shortly after performing a touch-and-go landing on the gravel surface adjacent to Runway 19 at the Dillingham Airport, as the airplane climbed to an altitude of about 200 ft above the runway, the engine experienced a momentary loss of power, followed by an engine restart. The nose of the airplane then pitched up, slowed, and the left wing stalled, resulting in an uncontrolled, nose-down, vertical descent. During the descent, the airplane engine reportedly experienced another loss of power.

The airplane impacted the runway approximately 680 feet northeast of the departure end of Runway 19 and came to rest inverted, resulting in substantial damage to the fuselage and wings. (See figure 1)

A witness captured a portion of the accident sequence on a cell phone video. See figures 2A and 2B.

The wreckage has been moved to a secure location and a detailed NTSB examination is pending.

Wednesday, August 27, 2025

Cessna 340A RAM VI, N888MT, fatal accident occurred on August 27, 2025, near Midwest National Air Center Airport (GPH/KGPH), Mosby, Missouri

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=N888MT

- History of Flight:

On August 27, 2025, at about 1157 local time, a Cessna 340A, N888MT, registered to Spelts Mark Warren Trustee out of Chico, California, was destroyed when it impacted terrain while on approach to land at Midwest National Air Center Airport (GPH/KGPH), Mosby, Missouri. The pilot and passenger were fatally injured. The personal flight originated from Washington Regional Airport (FYG/KFYG), Washington, Missouri, and was destined to KGPH.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 1058 LT, the airplane departed runway 33 at KFYG and entered a climbing left turn to an inflight cruising altitude of 4,200 ft. The flight appeared uneventful. At 1148:10 LT, the airplane started its descent towards KGPH. At 1156:46, the entered the traffic pattern at KGPH while on a left crosswind for runway 18. The airplane was decelerating through 120 knots ground speed as it entered the traffic pattern. At 1157:28, the airplane entered a descending left base turn toward runway 18. During the descending turn, the airplane decelerated to 87 knots groundspeed and achieved a maximum descent rate of about 1,200 feet per minute (fpm). At 1157:42, the final ADS-B data point was recorded about 0.73 nm from the runway 18 threshold. At that time, the airplane was at 675 ft msl, 85 knots groundspeed. The airplane had a 263.9° heading. (figure 1)

Figure 1: ADS-B exchange data ran on Google Earth

- Pilot Info:

The pilot(s) flying was/were not identified at the time of this writing. However, the current registered owner holds a private pilot certificate (issued/updated on 11/2/2012) with a rating for airplane single-engine land rating, an airplane multi-engine land rating, and an instrument rating. He held a third class FAA medical issued on July 2023, with a note stating he is not valid for any class after July 31, 2025. The individual did hold a BasicMed Course, dated 9/12/2023.

- Aircraft Info:

The accident airplane, serial number 340A0763, was manufactured in 1979. It was a pressurized twin-engine, low-wing, all-metal airplane, featuring retractable tricycle landing gear. The airplane was equipped with two Continental TSIO-520-NB engines modified with the RAM conversion, which increased the engine horsepower to 335 horsepower. These engines drove two Hartzell 3-blade, all-metal, constant speed propellers. The airplane was equipped with vortex generators indicated, which increased the airplane's maximum gross weight to 6,290 pounds. The vortex generators decreased the airplane's minimum controllable airspeed to 71 knots indicated airspeed.

According to the original Pilot Operating Handbook (POH):

"The stall characteristics of the airplane are conventional. Aural warning is provided by the stall warning horn between 5 and 10 KIAS above the stall in all configurations. The stall is also preceded by a mild aerodynamic buffet which increases in intensity as the stall is approached. The power-on stall occurs at a very steep pitch angle with or without flaps. It is difficult to inadvertently stall the airplane during normal maneuvering."

The following is the stall speed charts from the Ram VI version POH:

- Wreckage and Impact Information:

The airplane came to rest in an open field north of the airport. There was a small path leading to the main wreckage. The wreckage consisted of the entire airplane, which was consumed by a post crash fire. Both wings and tail remained attached to the airframe. The impact appears consistent with a low altitude aerodynamic stall/spin entry.

- Airport Information:

Midwest National Air Center Airport is an uncontrolled (no tower) public airport located one mile north of Mosby Missouri. The airport features a single asphalt runway 18/36 that is 5502 x 100 ft. The airport field elevation was 777.2 ft.

- Weather:

The reported weather at KGPH, at 1155 (about 2 minutes before the accident) included: wind 230° at 5 knots, 10 statute miles visibility, no clouds under 12,000 ft (CLR), a temperature of 25° C, a dew point of 10° C, and a barometric altimeter setting of 30.23 inches of mercury. The calculated density altitude was 1838 ft.

METAR KGPH 271635Z AUTO 22006KT 10SM CLR 24/11 A3023 RMK AO2

METAR KGPH 271655Z AUTO 23005KT 10SM CLR 25/10 A3023 RMK AO2

METAR KGPH 271715Z AUTO 21006KT 10SM CLR 25/10 A3022 RMK AO2

Unknown or undetermined: Mikoyan-Gurevich MiG-23UB, N23UB, accident occurred on August 13, 2023, near Willow Run Airport (YIP/KYIP), Belleville, Michigan

  • Location: Belleville, Michigan 
  • Accident Number: CEN23FA361 
  • Date & Time: August 13, 2023, 16:10 Local 
  • Registration: N23UB 
  • Aircraft: Mikoyan Gurevich MIG-23UB 
  • Aircraft Damage: Destroyed 
  • Defining Event: Unknown or undetermined 
  • Injuries: 2 Serious 
  • Flight Conducted Under: Part 91: General aviation - Air race/show
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/192855/pdf

https://data.ntsb.gov/Docket?ProjectID=192855

On August 13, 2023, about 1610 eastern daylight time, a Mikoyan Gurevich MiG-23UB airplane, N23UB, was destroyed when it was involved in an accident near Belleville, Michigan. The pilotin-command (PIC) and pilot-rated observer (PRO) received serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 air show exhibition flight.

Both the front-seat pilot-in-command (PIC) and the rear-seat pilot-rated observer (PRO) of the Russian-manufactured fighter jet reported that the airplane’s engine did not respond to application of afterburner power during a display pass at an air show. According to the PIC, the engine was operating in a degraded power condition that was insufficient to sustain altitude and airspeed. The PIC maneuvered the airplane back toward the airport while he attempted to restore engine power.

The PIC believed that his corrective measures would have restored engine power; however, the PRO activated the crew ejection system before engine power was restored. The PRO reported that he inquired about ejection with the PIC but did not hear a response before he activated the ejection system; however, the PIC reported that he replied “no” in response to the PRO’s ejection inquiry and that he was ejected from the airplane while he was troubleshooting the loss of engine power and still flying the airplane. Although the PIC was completing corrective actions, engine power was not restored by the time of the crew ejection and, therefore, the investigation was unable to determine if his corrective efforts would have been successful.

According to the PRO, the ejection system was activated about 350 ft above ground level (agl) and below 200 kts. Both pilots were ejected from the airplane, with the PRO ejected first, followed by the PIC. The airplane continued in a left bank and descended into the ground about 1.7 miles from the runway. The airplane impacted the ground adjacent an apartment building and was destroyed by impact forces and a post impact fire.

Other than the PIC’s mechanic, the NTSB was unaware of any independent engine shop or manufacturer within the United States with the appropriate tooling and expertise to perform a teardown examination of the Tumansky R27F2M-300 engine. The PIC’s written statement addressed potential sources for degraded engine performance; however, the NTSB could not validate the PIC’s opinion of the reason for the loss of engine power. Based on photographic evidence, the engine was producing some power at impact; however, the level of power output could not be determined. Due to investigative support limitations and the extend of damage, the investigators were unable to determine the reason for the loss of engine power. 

The airplane flight manual indicated that during a descent, the minimum safe altitude for crew ejection is calculated based on the airplane’s rate of descent and is equal to the rate of descent multiplied by 5. Based on the 350 ft agl altitude at ejection provided by the PRO, this altitude would be appropriate for ejection at a maximum rate of descent of 70 feet per minute (fpm). Although the airplane’s actual rate of descent was not known, it was likely significantly higher than the 70 fpm limitation at the time of crew ejection. Additionally, video evidence showed that the ejection seat parachutes did not fully deploy until the occupants had descended to just above treetop level. Therefore, the timing of the crew ejection was not premature. Given the serious injuries received by both occupants, crew ejection at a higher altitude may have reduced the severity of their injuries. Likewise, had the crew ejection been further delayed, the occupant injuries may have been more severe.

- Probable Cause: A reported partial loss of engine power while maneuvering for reasons that could not be determined.

Piper PA-46-500TP M500, N819MA, fatal accident occurred on July 20, 2025, near Lancaster Airport (LNS/KLNS), Lititz, Pennsylvania

  • Location: Lititz, PA
  • Accident Number: ERA25FA272 
  • Date & Time: July 20, 2025, 08:00 Local 
  • Registration: N819MA 
  • Aircraft: Piper PA46-500TP 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200578/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N519MA

On July 20, 2025, about 0800 eastern daylight time, a Piper PA-46-500TP Meridian airplane, N819MA, was substantially damaged when it was involved in an accident in Lititz, Pennsylvania. The pilot was the sole person on board and was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Prior to the accident flight, the airplane was towed from its hangar by line service personnel and the fuel tanks topped off with 74 gallons of Jet A and Prist fuel additive, for a total of approximately 170 gallons. Shortly afterward, airport surveillance video showed the instrument-rated private pilot arriving at the airplane. He performed a brief preflight inspection of the airplane, then entered the airplane and closed the main cabin door.

The engine was started and preliminary air traffic control (ATC) data showed that the pilot called for his instrument flight rules (IFR) clearance from Lancaster Regional Airport (LNS), Lancaster Pennsylvania to State College Regional Airport (UNV), State College Pennsylvania. The readback of the clearance instructions to the clearance controller was correct and the pilot was cleared to taxi to the runway.

Upon arrival at the hold-short line for departure, the ATC recording indicated that the tower controller advised the pilot to hold short while they waited for his IFR release. Three minutes later, the release was received, and the pilot was cleared for takeoff with a left turn on course. There was no readback of this instruction, and the surveillance video showed the pilot enter the runway and start his takeoff roll.

Preliminary Automatic Dependent Surveillance-Broadcast (ADS-B) data showed that the airplane reached rotation speed and lifted off. As the airplane cleared the departure end of the runway, having climbed to 650 ft mean sea level at a ground speed of 136 knots, the airplane suddenly pitched down to a descent rate of -1600 feet per minute. Approximately 9 seconds later, the airplane impacted a corn field 1/4 mile from the end of the runway on an estimated heading of 070° and a descent angle of approximately 39°and the left wing slightly down. The estimated flight time from the moment the wheels left the runway to impact was approximately 20 seconds. Nineteen seconds after takeoff, the control tower attempted to establish communication with the pilot multiple times without result.

The airplane came to rest 164 ft beyond the point of impact. The airframe was compressed due to impact forces. The engine and propeller created an impact crater 11 ft long, 6 ft wide, and 20 inches deep. The leading edges of the wings left an impression mark in the soil at the base of angle-cut corn stalks 3-6 inches deep along the entire wingspan. The surrounding corn throughout the debris field from the point of impact forward to the end of the debris field showed evidence of fuel blight with a strong odor of jet fuel throughout the accident site.

All flight surfaces were accounted for at the accident site. The left wing, wing-flap, and left aileron were fragmented into multiple sections. The left wing separated from the fuselage at the wing root and was found laying on top of the engine. The right wing remained attached to the airframe. The leading edge was found 20 ft behind the main airplane wreckage. The tail section was intact with the left horizontal spar broken but still attached. The vertical stabilizer remained attached and upright with leading edge damage.

The propeller, propeller shaft and forward reduction gear box broke free of the engine. The propeller shaft separated from the propeller and was found in the corn several feet beyond the propeller. The propeller was found 60 ft forward and to the right of the impact crater. It exhibited rotational damage including the separation of one of the four blades with two of the blades fractured at their midpoint.

The recorded weather at LNS, at 0753, included: wind from 200° at 3 knots, 5 miles visibility, broken clouds at 400 ft agl and 900 ft agl, mist, temperature 25° C, dew point 24° C, and an altimeter setting of 30.03 inches of mercury.

According to Federal Aviation Administration (FAA) records, the pilot held a private pilot certificate with ratings for airplane single-engine land and instrument airplane. His most recent FAA third-class medical certificate was issued on September 19, 2024. He reported on that date that he had accrued approximately 2,350 total flight hours.

According to FAA and airplane maintenance records, the accident airplane was manufactured in 2015. The airplane's most recent annual inspection was completed on March 14, 2025. At the time of the inspection, the airplane had accrued approximately 1,336 total hours of operation.

The wreckage was retained for further examination.

Cessna 172S Skyhawk SP, N5203H, fatal accident occurred on August 26, 2025, near Los Banos, California

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=N5203H


- History of Flight:
On August 26, 2025, at about 1905 local time, a Cessna 172S Skyhawk SP, N5203H, registered to Tegridy Equipment Leasing LLC out of Aurora, Oregon, was destroyed when it was involved in an accident near Los Banos, California. The sole pilot onboard sustained fatal injuries. The personal flight originated from San Jose-Reid-Hillview Airport (RHV/KRHV), San Jose, California, and was destined to an unknown location.

The exact purpose of the flight is unknown at the time of this writing.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data (Figure 1), at 1511 local time, the airplane departed runway 31R at KRHV and conducted a climbing right turn to an inflight cruising altitude of about 5,000 ft. At about 1556 LT, the airplane reached the Dos Palos area and began a series of circling orbits with altitudes ranging between 6,700 ft and 5,700 ft. At about 1630 LT, the airplane flew north and began another series of circlcing orbits over the Los Banos Wildlife area (Figure 2). At about 1701 LT, the airplane flew east and conducted 3 low altitude orbits before climbing to an altitude of 6,000 ft and proceeding to the south. At about 1713 LT, the airplane conducted 3 orbits and descended to an altitude of 3100 ft, heading southwest. At about 1741 LT, the airplane began a series of erratic circling orbits south of Los Banos. At about 1810 LT, the airplane flew northwest towards the area of the Wright Solar Park. At about 1826 LT, the airplane, for another time, began a series of circling orbits, which increased in intensity until the end of the track. The last series of orbits were conducted at altitudes lower than 3,000 ft. The last ADS-B return was recorded at 1905:02, the airplane was at 625 ft, 57 knots groundspeed, and descending 15,000 feet per minute (fpm), see figure 3.

Figure 1: ADS-B Exchange data of initial portion of accident flight up to 1701 LT

Figure 2: ADS-B Exchange data ran through Flysto (initial portion up to 1701 LT)

Figure 3: ADS-B Exchange data ran through Flysto (1701 LT up to end of track)

Figure 4: Altitude Profile from Flysto (1701 LT up to end of track)

Figure 5: Vertical Speed from Flysto (1701 LT up to end of track)

Figure 6: Turn Rate from Flysto (1701 LT up to end of track)

According to preliminary information, the airplane encountered issues shortly after takeoff from San Jose and was in contact with air traffic control during the entire accident flight. The pilot reported severe control issues. Additionally, another airplane was following the accident aircraft.

Witnesses said the airplane "nosed-dived" into the ground.

- Pilot Information:
unknown at this point

According to unconfirmed sources, the pilot held a certificated pilot license and owned an aircraft. The accident aircraft was a rental.

- Aircraft Information:
The accident aircraft, serial number 172S9732, was manufactured in 2004. It was powered by a Lycoming IO-360 180 horsepower engine. The airplane had a total of 53 gallons useable fuel.

The airplane was involved in an accident on August 3, 2016 in Palm Springs, California, when a student pilot lost control during an aborted landing, which resulted in a nose over.

- Wreckage and Impact Information:
The wreckage was located inverted in an open field in the area of the last ADS-B return. The airplane was heavily fragmented by impact forces. There was no post crash fire. Both wings and tail remained attached to the airframe. The impact appears consistent with a wings level, nose down impact.

- Weather:
METAR KMCE 270053Z AUTO 31006KT 10SM CLR 35/15 A2981 RMK AO2 SLP092 T03500150
METAR KMCE 270153Z AUTO 29005KT 10SM CLR 34/16 A2980 RMK AO2 SLP089 T03390161
METAR KMCE 270253Z AUTO 28006KT 9SM CLR 31/16 A2982 RMK AO2 SLP096 T03110161 55002

- Additional Information:
no