Tuesday, August 19, 2025

Landing gear collapse: Rutan Long-EZ, N58JB, accident occurred on September 5, 2025, at Laughlin/Bullhead International Airport (IFP/KIFP), Bullhead City, Arizona


  • Location: Bullhead City, Arizona
  • Accident Number: WPR23LA340 
  • Date & Time: September 5, 2023, 16:20 Local 
  • Registration: N58JB 
  • Aircraft: Rutan Long-EZ 
  • Aircraft Damage: Substantial 
  • Defining Event: Landing gear collapse 
  • Injuries: 1 None
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/193050/pdf

https://data.ntsb.gov/Docket?ProjectID=193050

On September 5, 2023, about 1620 Pacific daylight time, a Rutan Long-EZ experimental airplane, N58JB, was substantially damaged when it was involved in an accident near Bullhead City, Arizona. The private pilot, the sole occupant, was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that when he touched down, the main landing gear contacted the runway surface, followed by the nose gear. He instantly heard a loud “bang” as the nose gear collapsed and the nose continued to settle, sliding down the runway surface.

Examination of the nose gear revealed that the nose landing gear actuator failed due to the buckling and fracture of the ball screw, which resulted from compressive loads on the actuator assembly. These compressive loads were likely from vertical and/or aft loads on the nose wheel. The actuator was likely in the fully extended position, but the length of the accident actuator was longer than its design length at full extension. Issues with the actuator installation that might have contributed to the overextension could not be determined.

The examination further revealed that the nose landing gear likely sustained a relatively hard landing while in the fully extended position. However, the additional length in the overextended actuator assembly made the ball screw susceptible to buckling failure from lower compressive loads than designed. Additionally, since less length of the extension tube was constrained by the housing in the overextended assembly, the reduced constraint likely made the assembly susceptible to buckling at even lower loads. The assembly’s extension beyond its design length likely contributed to the failure, as the extension would have diminished the safety margin and increased the vulnerability to buckling failure under high landing loads.

- Probable Cause: The pilot’s improper flair resulting in a hard landing.

Piper PA-28RT-201T Turbo Arrow IV, N8423H, accident occurred on July 27, 2025, near Brookings, South Dakota

  • Location: Brookings, SD 
  • Accident Number: CEN25LA288 
  • Date & Time: July 26, 2025, 18:40 Local 
  • Registration: N8423H 
  • Aircraft: Piper PA-28RT-201T 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Other work use

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200636/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumberTxt=N8423H

Turbo Arrow LLC

On July 26, 2025, at 1840 central daylight time, a Piper PA-28RT-201T airplane, N8423H, was substantially damaged when it was involved in an accident near Brookings, South Dakota. The airline transport pilot and passenger were uninjured. The airplane was operated under Title 14 Code of Federal Regulations Part 91 as a work use flight.

The pilot stated that during a departure climb from runway 12 at Brookings Regional Airport (BKX), Brookings, South Dakota, the fuel flow gauge indication was fluctuating. He initiated a return to BKX for a precautionary landing and entered the left downwind for runway 17. The engine continued to operate and there were no abnormal sounds or other abnormal instrument indications. During the completion of the base to final turn for runway 17, the airplane experienced a total loss of engine power. The pilot then performed a forced landing to a field where the airplane impacted a fence and the field. The airplane sustained substantial damage to the left wing and both wing flaps.

The airplane was retained for further examination.

Lancair Evolution, N505RF, accident occurred on July 27, 2025, near Coeur d'Alene Airport/Pappy Boyington Field (COE/KCOE), Coeur d’Alene, Idaho

  • Location: Coeur d' Alene, ID
  • Accident Number: WPR25LA230 
  • Date & Time: July 27, 2025, 10:10 Local 
  • Registration: N505RF
  • Aircraft: BALLISODARE LLC LANCAIR EVOLUTION 
  • Injuries: 3 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/200658/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N505RF

On July 27, 2025, about 1010 Pacific daylight time, an experimental amateur-built Lancair Evolution airplane, N505RF, was destroyed when it was involved in an accident near Coeur d’Alene, Idaho. The pilot and two passengers sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported an uneventful takeoff and flew south to the north end of Coeur d’Alene Lake and then proceeded back towards the airport. During his turn to the base leg of the traffic pattern, he received a low oil pressure warning and then the engine lost all power. Unable to make it to the airport, the pilot made a forced landing on a road. The airplane then departed the left side of the road, the landing gear separated, and the airplane skidded before it came to rest. The occupants exited the airplane, and by the time they were at a safe distance, most of the airplane was consumed by postcrash fire.

The airplane was recovered to a secure facility for further examination. 

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