Friday, May 29, 2026

Cessna 172 Skyhawk, N3984F, accident occurred on May 27, 2026, at Hiawatha Sportsmans Club Airport (MI69), Naubinway, 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=N3984F

- History of Flight:
On May 27, 2026, at about 1545 local time, a privately-registered Cessna 172 Skyhawk, N3984F, sustained substantial damage when it was involved in an accident at Hiawatha Sportsmans Club Airport (MI69), Naubinway, Michigan. The pilot suffered minor injuries.

The FAA reported: "Aircraft nosed over while landing on a grass strip and came to rest inverted." MI69 is the only airport located in Naubinway. There is no ADS-B data for the accident track.

The closest airport, KERY, was reporting winds from 350° at 12 knots, gusting 16 knots.

- Weather:

METAR KERY 271935Z AUTO 35012G16KT 10SM CLR 23/06 A3005 RMK AO2

METAR KERY 271955Z AUTO 02010G16KT 340V040 10SM CLR 23/07 A3006 RMK AO2

Gulfstream G600, N600WE, accident occurred on May 27, 2026, at Birmingham-Shuttlesworth International Airport (BHM/KBHM), Birmingham, Alabama

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=N600WE

- History of Flight:
On May 27, 2026, at about 1308 local time, a Gulfstream G600, N600WE, registered to Spring Creek Aviation LLC out of Newark, Delaware, sustained substantial damage when it was involved in an accident at Birmingham-Shuttlesworth International Airport (BHM/KBHM), Birmingham, Alabama. The pilot and fourteen passengers were not injured. The cross-ocean international personal flight originated from Kerry County Airport (KIR/EIKY), Farranfore, Ireland.

The FAA reported: "Aircraft veered off runway during landing damaging the right wing." The NTSB is investigating the event as an accident.

ADS-B data shows that the airplane departed the right side of runway 24 going about 115 knots groundspeed. At 1258, the winds were from 170 at 7 knots, with reported thunderstorms and occasional lightning.

Figure 1: ADS-B data

Figure 2: Close-up of data
- Weather:

METAR KBHM 271758Z 17007KT 10SM TS BKN033TCU 28/21 A3005 RMK AO2 TSB58 OCNL LTGCG S TS S MOV NE CB DSNT SE-SW MOV NE TCU NE-SE-SW T02830211

METAR KBHM 271809Z 18007KT 100V210 3/4SM +TSRA BR BKN033CB 27/22 A3006 RMK AO2 RAB00 TSB1758 OCNL LTGCG S TS S MOV NE CB DSNT SE-SW MOV NE TCU OHD AND NE-SE-SW P0003 T02720222 RVRNO

METAR KBHM 271834Z COR 09006KT 3SM +RA BR BKN033CB 24/22 A3005 RMK AO2 RAB00 TSB1758 CB NE-SE-S AND W MOV NE P0079 T02440217

Mooney M20M Bravo, N611DG, incident occurred on May 27, 2026, at Jack Mc Namara Field Airport (CEC/KCEC), Crescent City, 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=N611DG

- History of Flight:
On May 27, 2026, at about 1212 local time, a privately-registered Mooney M20M Bravo, N611DG, sustained unknown damage when it struck a runway edge light when it landed on runway 12 with a tailwind at Jack Mc Namara Field Airport (CEC/KCEC), Crescent City, California. The pilot and two passengers were not injured. The cross-country personal flight originated from Olympia Airport (OLM/KOLM), 
Olympia, Washington, at 1029.

At 1156, the winds were from 340° at 19 knots, gusting 29 knots.

Figure 1: ADS-B exchange data

- Weather:

METAR KCEC 271856Z AUTO 34019G29KT 9SM FEW100 14/10 A2982 RMK AO2 PK WND 34030/1843 SLP099 T01440100

METAR KCEC 271956Z AUTO 34016G34KT 8SM CLR 13/10 A2981 RMK AO2 PK WND 33034/1947 LTG DSNT SE SLP097 T01280100

Piper PA-44-180 Seminole, N935LT, incident occurred on May 27, 2026, at Orlando Sanford International Airport (SFB/KSFB), Sanford, Florida

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=N935LT

- History of Flight:
On May 27, 2026, at about 1315 local time, a Piper PA-44-180 Seminole, N935LT, registered to Aerosim Flight Academy and being operated by L3 Airline Academy, sustained unknown, but apparent minor damage when the left engine caught fire during engine start up, but fire extinguished on its own at Orlando Sanford International Airport (SFB/KSFB), Sanford, Florida. The instructor and student were not injured. The aircraft was being operated on a local instructural flight.

The aircraft continued normal operations out of KSFB the following day.

Cessna 170B, N2526D, incident occurred on May 27, 2026, at Bethel Airport (BET/PABE), Bethel, Alaska

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=N2526D

- History of Flight:
On May 27, 2026, at about 1650 local time, a privately-registered Cessna 170B, N2526D, sustained unknown damage when it suffered a left wing strike with the runway on landing at Bethel Airport (BET/PABE), Bethel, Alaska. The pilot was not injured.

- Weather:

METAR PABE 272353Z VRB04KT 10SM BKN042 11/02 A2965 RMK AO2 SLP040 T01110017 10117 20050 51006

METAR PABE 280053Z 02010KT 10SM SCT040 BKN050 OVC060 11/04 A2965 RMK AO2 SLP044 T01060044

METAR PABE 280115Z 13009KT 10SM -RA FEW033 OVC045 09/07 A2967 RMK AO2 WSHFT 0055 RAB06 P0000 T00890067

Thursday, May 28, 2026

Loss of control in flight: Cessna 150L, N1701Q, fatal accident occurred on May 15, 2024, near Godley, Texas


  • Location: Godley, Texas 
  • Accident Number: CEN24FA188 
  • Date & Time: May 15, 2024, 20:39 Local 
  • Registration: N1701Q 
  • Aircraft: Cessna 150L 
  • Aircraft Damage: Destroyed 
  • Defining Event: Loss of control in flight 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Instructional 
https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/194266/pdf

https://data.ntsb.gov/Docket?ProjectID=194266

On May 15, 2024, about 2039 central daylight time, a Cessna 150L airplane, N1701Q, was destroyed during an accident near Godley, Texas. The student pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 solo instructional flight.

The student pilot was conducting a local solo flight. Review of flight track data revealed that, during the final 6.5 minutes of the flight, the airplane completed several large deceleration-and-acceleration cycles between 1,000 and 1,700 ft above ground level (agl). During each of these cycles, the airplane’s airspeed decreased below aerodynamic stall speed before it increased again. The airspeed and altitude profiles during these maneuvers were consistent with the pilot practicing aerodynamic stalls.

Shortly before the accident, the airplane entered a rapid climb while the airspeed decreased below aerodynamic stall speed, consistent with an intentional power-on stall entry. There was a 6-second interruption in track data coverage after the airplane entered the aerodynamic stall, but when coverage resumed, the airplane was in a rapid descent that continued until the end of recorded data about 8 seconds later.

A witness reported seeing the airplane flying at slow speed, almost “hovering” in the air, before it suddenly entered a spiraling nosedive. The airplane completed at least 6 to 8 rotations in the descending spiral before it descended out of sight behind a hill. An extensive postimpact fire thermally damaged most of the airplane.

A wreckage examination revealed no evidence of a preimpact mechanical malfunction or failure that would have prevented normal airplane operation. The pilot’s autopsy and postmortem toxicology tests did not reveal any evidence of medical incapacitation or impairment. Based on the available information, the pilot likely did not maintain airplane control during the intentional power-on stall, which resulted in an inadvertent spin at an altitude from which he was unable to recover.

- Probable Cause: The student pilot’s failure to maintain airplane control while practicing a power-on stall, which resulted in an inadvertent spin at an altitude from which he was unable to recover.

VFR encounter with IMC: Air Tractor AT-802A, N331BS, fatal accident occurred on June 21, 2024, near Capitan, New Mexico

  • Location: Capitan, New Mexico 
  • Accident Number: WPR24FA202 
  • Date & Time: June 21, 2024, 10:58 Local 
  • Registration: N331BS 
  • Aircraft: AIR TRACTOR INC AT-802A 
  • Aircraft Damage: Destroyed 
  • Defining Event: VFR encounter with IMC 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Positioning

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/194523/pdf

https://data.ntsb.gov/Docket?ProjectID=194523

On June 21, 2024, about 1100 mountain daylight time, an Air Tractor AT-802A airplane, N331BS, was destroyed when it was involved in an accident near Capitan, New Mexico. The pilot was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 positioning flight.

A flight of three fire-fighting airplanes was being repositioned on a visual flight rules flight from Texas to Oregon. The flight crews planned a refueling stop at an airport in New Mexico. Before reaching the airport, they saw “a light rain shower” ahead of them near the Capitan Mountains in New Mexico. The pilots of the first two airplanes maneuvered to avoid the weather, and the lead pilot directed the other two airplanes to turn 30° and climb to reacquire visual contact with one another. However, one of the pilots observed the accident airplane maneuvering about 2,000 ft below the other airplanes, and the accident pilot subsequently reported that he had a visual flight rules (VFR) corridor through the weather. The pilot likely elected to continue through the VFR corridor rather than climb with the other airplanes. Because the airplanes had been cruising at about 9,500 ft mean sea level (msl), the accident airplane was operating at about 7,500 ft msl in mountainous terrain where elevations in the Capitan Mountain Range exceeded 10,000 ft msl.

After the first two airplanes landed at the planned refueling destination, the pilots realized that the accident airplane had not arrived and was missing. After the FAA issued an Alert Notice for the missing airplane, the wreckage was located about 9 miles east-northeast of the Capitan Mountains by another airplane.

All required flight control surfaces of the airplane were found at the accident site. The ground scars, tree impact signatures, and wreckage impact fragment distribution indicated that the airplane impacted rising terrain in a near-level flight attitude at high forward velocity, consistent with controlled flight into terrain. Although the airplane was highly fragmented, postaccident examination of the airplane revealed no evidence of preimpact malfunctions or failures that would have precluded normal operation. The impact signatures on the propeller blades were consistent with high RPM and engine power at the time of impact.

Weather information for the area indicated widespread mountain obscuration, low ceilings, and light rain near the accident site. The National Weather Service (NWS) had several AlRMETs that were current at the time of the accident for mountain obscuration in the area, and weather observations near the accident site reported instrument flight rules (IFR) and low IFR (LIFR) conditions. Satellite imagery, weather radar data, and model sounding data indicated extensive overcast clouds and saturated atmospheric conditions over the mountainous terrain surrounding the accident site

Although IFR and mountain obscuration conditions existed in the surrounding area, the available evidence suggests that the pilot was likely attempting to maintain visual meteorological conditions while maneuvering through an apparent VFR corridor. As the airplane approached the mountainous terrain, the apparent VFR corridor ahead likely deteriorated rapidly due to rising terrain and mountain obscuration. Given the airplane’s nearlevel, high-speed impact attitude, the pilot was likely unable to perceive and avoid the terrain in sufficient time to prevent the collision.

- Probable Cause: The pilot’s decision to continue the visual flight rules flight through an apparent visual corridor that rapidly narrowed due to rising terrain and mountain obscuration, resulting in momentary instrument meteorological conditions and the pilot’s subsequent controlled flight into the obscured terrain.