Tuesday, August 19, 2025

Cessna P210N Pressurized Centurion II, N92MS, accident occurred on August 13, 2025, near Zapata, TX

  • Location: Zapata, TX
  • Accident Number: CEN25LA317 
  • Date & Time: August 13, 2025, 18:35 Local 
  • Registration: N92MS 
  • Aircraft: Cessna P210 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200779/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N92MS

On August 13, 2025, about 1835 central daylight time, a Cessna P210N airplane, N92MS, was substantially damaged when it was involved in an accident near Zapata, Texas. 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 the flight was normal until he turned the airplane to return back to the McAllen International Airport, McAllen, Texas. During the return, he felt a severe vibration from the engine and noticed a partial loss of engine power. The engine instruments displayed 0 inches of manifold pressure, high oil temperature, low oil pressure, and high temperatures on the No. 4 and 5 cylinders. While diverting to the Zapata County Airport, Zapata, Texas, the engine lost total power, and the pilot was unable to glide the airplane to the runway. He then performed an off-field landing on a dirt road. During the landing roll on the dirt road, the airplane’s left wing collided with a tree, turning the airplane to the left into a tree line. Both wings sustained substantial damage.

The airplane was retained for further investigation.

Centrair 101A Pegase, N99KG, accident occurred on August 16, 2025, near Springfield, Vermont

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=N99KG

NTSB ERA25LA303

On August 16, 2025, at about 1330 local time, a privately-registered Centrair 101A Pegase glider, N99KG, sustained substantial damage when it was involved in an accident near Springfield, Vermont. The pilot sustained unknown injuries.

The FAA reported that the glider was released from the tow and experienced loss of control and impacted terrain.

Monday, August 18, 2025

Bailey-Moyes Dragonfly, N4010E, accident occurred on July 13, 2025, near Charleston, New Hampshire

  • Location: Charlestown, NH
  • Accident Number: ERA25LA265 
  • Date & Time: July 13, 2025, 19:15 Local 
  • Registration: N4010E 
  • Aircraft: MOYES LITEFLITE PTY LTD C DRAGONFLY 
  • Injuries: 1 Serious 
  • Flight Conducted Under: Part 91: General aviation - Glider tow
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200524/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N4010E

On July 13, 2025, about 1915 eastern daylight time, a Moyes Liteflite Model C Dragonfly airplane, N4010E, was substantially damaged when it was involved in an accident near Charleston, New Hampshire. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 glider tow flight.

The pilot reported that the accident flight was his fifth tow flight of the day. There were no anomalies noted during preflight inspection or before the takeoff engine runup checks. The airplane departed with about 4-gallons of fuel onboard. After reaching an altitude of 3,500 ft, the glider released and the pilot reduced engine power to idle and entered a routine spiraling descent to land. During the descent, the airplane experienced a total loss of engine power which the pilot did not observe until he advanced the throttle, and the engine did not respond.

A witness at the departure airport recorded a video of the airplane as it descended. The video showed the airplane in a left turning descent before it entered a shallow right spiraling descent. The airplane remained in the right turn until it impacted the ground. The airplane came to rest in an upright position in a grass field about one-half mile from the departure airport.

Postaccident examination of the airplane by an Federal Aviation Administration inspector revealed that the tubular structure of the fuselage exhibited deformation and fractures from impact forces. Flight control continuity was established from the cockpit to all of the flight control surfaces. The engine remained attached to the fuselage and the throttle control cables remained attached and were continuous to the throttle control lever. The fuel tank contained about 2-gallons of fuel and the fuel filter was free of contamination.

The airplane was retained for further examination. 

Cessna 140, N89447, fatal accident occurred on August 17, 2025, near Shelter Cove Airport (0Q5), Shelter Cove, 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=N89447

- History of The Flight
On August 17, 2025, at about 1521 local time, a privately-registered Cessna 140, N89447, sustained substantial damage when it was involved in an accident near Shelter Cove Airport (0Q5), Shelter Cove, California. The pilot sustained fatal injuries, and passenger sustained serious injuries. The airplane was operated under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

Preliminary information indicates the airplane departed Shelter Cove (unknown which runway at this point) and "turned west, and shortly after plunged into the ocean approximately 100 yards offshore."

According to preliminary ADS-B data, the airplane arrived at Shelter Cove at about 1300 LT, after a flight from Charles M. Schulz–Sonoma County Airport (STS/KSTS), Santa Rosa, California. The accident flight was not captured by any tracking sites.

- Pilot Information:
Unknown at this point.

According to online FAA records, the current registered owner holds a student pilot certificate, issued on 5/10/2021, and a second class FAA medical that was issued on June 2024.

- Aircraft Information:
The accident aircraft, serial number 8479, was manufactured in 1946. It was a single-engine, two-seat, conventional landing gear airplane powered by a Continental C-85 engine.

- Airport Information:
Shelter Cove Airport (0Q5) is a publicly-owned airport located 1 mile west of Shelter Cove, California. The airport field elevation was 73.4 ft. The airport features a single asphalt runway 12/30 that is 3407 ft long and 60 ft wide.

According to one of the airport remarks...

"EXPECT CROSSWINDS, DOWNDRAFTS AND EXTDD PERIODS OF FOG YEAR-ROUND."

- Weather:
(1) METAR:
The nearest weather station located at Rohnerville Airport (KFOT), Fortuna, California, reporting the following conditions:

At 1515 (6 minutes before the accident) noted: winds 350 at 8 knots, visibility 10 statute miles, few clouds under at 2,700ft AGL, an overcast (OVC) layer at 3,300ft AGL, temperature 19°C, dew point 15°C, and an altimeter setting of 30.04 inches of mercury (inHg).

At 1535 (14 minutes after the accident) noted: winds 010 at 8 knots, visibility 10 statute miles, few clouds under at 2,700ft AGL, an overcast (OVC) layer at 3,300ft AGL, temperature 20°C, dew point 14°C, and an altimeter setting of 30.03 inches of mercury (inHg).

METAR KFOT 172155Z AUTO 32009KT 10SM OVC031 19/14 A3004 RMK AO1
METAR KFOT 172215Z AUTO 35008KT 10SM FEW027 OVC033 19/15 A3004 RMK AO1 <<<<
METAR KFOT 172235Z AUTO 01008KT 10SM SCT027 OVC033 20/14 A3003 RMK AO1 <<<<
METAR KFOT 172255Z AUTO 35011KT 10SM OVC031 19/14 A3003 RMK AO1

(2) Area Forecast Discussion:

AREA FORECAST DISCUSSION
National Weather Service Eureka CA
210 PM PDT Sun Aug 17 2025

.SYNOPSIS...A chance for showers and isolated thunderstorms over
eastern Trinity County today. A gradual drying and warming trend
will develop this week, with further warming late in the week.

&&

.DISCUSSION...After the frontal passage and light precipitation
observed Saturday, extensive stratus remains today. Early afternoon
satellite shows the low level clouds blanketing most of Humboldt
and Del Norte counties, with also a good portion of Mendocino
covered. This is due to a greatly deepened marine layer. There
was lower level shallow moisture contributing to patchy locally
dense fog, but that generally mixed out. Chances for fog are lower
tonight, with less coverage expected.

Soundings continue to show moisture at the 700 mb area with some
instability today, and forcing exists from passing shortwave
energy. Satellite imagery this early afternoon also shows some
billowing cumulus over the Yolla Bolly region and through eastern
Trinity County. These areas are where isolated afternoon showers
and a 10-20% chance for thunderstorms are forecast.

Moisture and instability mostly depart to start the work week
Monday. This will also mark the start of a gradual warming trend. A
shortwave perturbation will clip the northern region Wednesday, but
is expected to have little impacts other suppressing the greater
inevitable warmup. Beyond the passing of the shortwave, temperatures
will indeed further warm late in the week. Probability for isolated
warmer valleys to exceed 100 increases Thursday. Chances for
temperatures over 100 are highest Friday (75%) for the interior
valleys. Chances begin slowly dropping thereafter with a weak
signal from clusters of some troughing influence, but the heat may
linger longer through the weekend.

There are hints of some monsoonal moisture getting pulled in from
the SE next weekend. This would increase chances for
thunderstorms, but the quality of moisture and instability look
poor at this time. /JJW


&&

.AVIATION...Low clouds along the coast have been scattering and
lifting as a shortwave approaches. Currently, VFR conditions with
OVC layer around 3500-4000 feet, accompanied by some SCT layer
around 005 feet at ACV and CEC. Expect fluctuations in conditions
at the coastal terminals through 18/03Z, before IFR/LIFR
conditions redeveloped along the coast with low clouds and
visibility in FG/mist. Winds from W at around 5 kts, becoming very
light and variable after 3Z.

For inland areas: VFR conditions persist at UKI through the period.
Surface winds very light and variable, after 22Z becoming NW at
around 10kts with higher occasional gusts. There is the potential
for some isolated SHRA/TSRA across the eastern portion of Trinity
County this afternoon and early evening. /ZVS

- Additional Information:
no

Saturday, August 16, 2025

Runway excursion: Schweizer SGS 1-26C, N9839E, accident occurred on June 1, 2025, at Sky Soaring Airport (55LL), Hampshire, Illinois

  • Location: Hampshire, Illinois 
  • Accident Number: CEN25LA202 
  • Date & Time: June 1, 2025, 15:00 Local 
  • Registration: N9839E 
  • Aircraft: Schweizer SGS 1-26C 
  • Aircraft Damage: Substantial 
  • Defining Event: Runway excursion 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200294/pdf

https://data.ntsb.gov/Docket?ProjectID=200294

The pilot reported that while maneuvering the glider for landing on runway 27, he encountered unexpected lift and then used a side slip maneuver to descend. He descended too low to continue the approach, so he maneuvered to land on runway 9 and landed about two-thirds of the way down the runway. The glider overran the departure end of the runway and impacted terrain, resulting in substantial damage to the left wing. The pilot reported that there were no preaccident mechanical malfunctions or failures with the glider that would have precluded normal operation.

- Probable Cause: The pilot's failure to maintain a proper altitude during the approach, which resulted in overshooting the landing area, a runway excursion, and impact with terrain.

Abnormal runway contact: Cessna 182M Skylane, N71149, accident occurred on June 2, 2025, at Charlevoix Municipal Airport (CVX/KCVX), Charlevoix, Michigan

  • Location: Charlevoix, Michigan 
  • Accident Number: CEN25LA195 
  • Date & Time: June 2, 2025, 11:30 Local 
  • Registration: N71149 
  • Aircraft: Cessna 182 
  • Aircraft Damage: Substantial 
  • Defining Event: Abnormal runway contact 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Business 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200270/pdf

https://data.ntsb.gov/Docket?ProjectID=200270

The purpose of the training flight was for the pilot, who was employed by the skydiving operator, to become familiar with the airplane, as he had never flown it before. During the takeoff, a witness observed the airplane bounce multiple times. During the second bounce, the witness heard a loud noise, and during the third and final bounce, the witness heard an even louder noise. The witness surmised that the third bounce was “so violent” that he thought the airplane as going to become inverted. The airplane became airborne and departed, while remaining in the traffic pattern. During the no flap landing, the pilot reported that as he began pulling back on the yoke to flare, he noticed that the nose of the airplane was not pitching up. The airplane landed on the nose landing gear, which sustained a flat tire. The airplane came to rest upright on the right side of the runway and the pilot was able to egress without further incident.

The airplane sustained substantial damage to the fuselage aft of the engine compartment and to the cockpit floor. Postaccident examination of the flight control system found an excessive amount of slack in the elevator control cables due to the fuselage damage sustained from the multiple bounces that occurred during the takeoff. The substantial damage resulted in excessive slack to the elevator control cables that resulted in the pilot not having adequate pitch control during the landing.

- Probable Cause: The pilot’s failure to maintain pitch control during the takeoff that resulted in multiple bounces and substantial damage to the fuselage.

Runway excursion: Dassault Falcon 10, N87RT, accident occurred on June 6, 2025, at Panama City-Northwest Florida Beaches International Airport (ECP/KECP), Panama City, Florida

  • Location: Panama City, Florida
  • Accident Number: ERA23LA261
  • Date & Time: June 6, 2023, 20:17 Local
  • Registration: N87RT 
  • Aircraft: DASSAULT-BREGUET FALCON 10 
  • Aircraft Damage: Substantial 
  • Defining Event: Runway excursion 
  • Injuries: 5 None 
  • Flight Conducted Under: Part 91: General aviation - Personal
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/192331/pdf

https://data.ntsb.gov/Docket?ProjectID=192331

On June 6, 2023, about 2017 central daylight time, a Dassault-Breguet Falcon 10, N87RT, was substantially damaged when it was involved in an accident near Panama City, Florida. The pilot, copilot, and three passengers were not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Upon arriving at the destination airport, the business jet touched down about 2,500 ft beyond the threshold of the 10,000-ft-long runway 16. The pilot extended the airplane's flight spoilers and attempted to activate the thrust reversers, but the airplane did not decelerate as expected and a warning horn sounded. The pilots then attempted to apply normal followed by emergency braking, both of which were ineffective in slowing the airplane. The airplane subsequently overran the runway and struck several approach lighting stanchions, coming to rest after the landing gear collapsed. The airplane's occupants were uninjured, but the airplane was substantially damaged during the accident sequence.

Following the accident, the captain noticed he had forgotten to move the thrust reverser emergency stow switches to their normal operating position after completing a preflight check. The warning horn heard during the landing was an indication of the stowed thrust reverser switches. The ineffective braking likely occurred because of the engines' increased thrust output due to the attempted application of the thrust reversers with the switches in the stowed position.

A postaccident examination of the wreckage confirmed that there was no evidence of any preimpact mechanical malfunctions or failures that would have precluded normal operation of the airplane. The airplane checklist found in the cockpit was marked “For Training Purposes Only' and for an airplane that was not equipped with thrust reversers.

Probable Cause: The flight crew's failure to appropriately configure the airplane for landing, which resulted in a failed attempt to utilize the thrust reversers during landing and the inability to stop the airplane using its brakes due to increased forward thrust. Contributing to the accident was the flight crew's failure to utilize the appropriate checklist for the thrust reverser equipped airplane.