Friday, May 01, 2026

Piper PA-32R-301T Saratoga II TC, N4190E, fatal accident occurred on April 8, 2026, at Marana Regional Airport (AVQ/KAVQ), Marana, Arizona

  • Location: Marana, AZ
  • Accident Number: WPR26FA151
  • Date & Time: April 8, 2026, 17:10 Local
  • Registration: N4190E
  • Aircraft: Piper PA-32R-301T
  • Injuries: 2 Fatal
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202782/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N4190E

On April 08, 2026 at 1710 mountain standard time, a Piper PA-32R-301T, N4190E, sustained substantial damage when it was involved in an accident near Marana, AZ. The pilot and passenger sustained fatal injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

A review of ADS-B data revealed that the pilot and passenger were returning from a long crosscountry flight they had made several days before the accident. They departed at 0712 and while en route back to Marana, they made two stops, refueling at each location. On the accident leg of the trip, the airplane departed Springerville, Arizona about 1550 and proceeded west, climbing to about 10,500 ft mean sea level (msl) while gradually heading toward the south-west. About 1630, the airplane proceeded south toward Marana and then began a gradual descent while continuing south toward Marana.

At 1701 the pilot transmitted over the Marana traffic Unicom frequency that he was 11 miles from the airport and intended to land on runway 21 using a left traffic pattern. Immediately thereafter, another airplane departing Marana made radio calls stating that they departed runway 21 and were leaving the area.

ADS-B data showed that the accident airplane crossed over the town of Marana and at1704 the pilot reported that he was just north of the airport and was adjoining the downwind leg for runway 03 using a left traffic pattern. The airplane then continued around the traffic pattern and on the final approach leg, about 1.5 nm from the runway threshold, the airplane was 950 ft above ground level (agl), maneuvering about 120 kts true airspeed (TAS). The airspeed temporarily increased to 130 ft and then decreased to 105 as the airplane crossed the runway threshold. About 7 seconds later, after the airplane likely touched down and reached the lowest speed of 96 kts, the speed began to increase consistent with pilot aborting the landing with 1,975 ft of runway remaining. 

The pilot transmitted that he had performed a go-around and then made two separate radio calls stating that he was turning onto the base and final approach legs of the traffic pattern for runway 03. The airplane made a closer pattern than the first approach and was maneuvering about 350 to 425 ft agl. After slightly overshooting the final approach course, the airplane adjoined the leg about 3,200 ft from the runway threshold while maneuvering at 130 kts (see figure 1 below).


The airplane’s airspeed temporarily increased to 135 kts and then decreased, reaching 116 kts as the airplane crosses the runway threshold (see figure 2 below). The airplane touched down an estimated 1,500 ft from the runway threshold and bounced back airborne several times. The ground speed decreased to 80 kts with about 1,300 ft of runway remaining and continued to gradually decrease reaching the end of the runway surface at 54 kts. The last recorded speed of about 44 kts was adjacent to the accident site (see figures 3 and 4 below).


The main wreckage came to rest in and around a concrete drainage culvert set into an embankment. A majority of the airframe was consumed by fire with only the aft empennage and left wing tip remaining intact. The concrete on the top of the culvert was broken and there were blue paint transfers consistent with the lover nose section making contact. The threebladed propeller was separated at the mounting flange at the engine crankshaft and found above the culvert.

Main landing gear and nose landing gear tire marks were visible on runway 03. The first detectable main landing gear and nose landing gear marks began on the runway surface about 495 ft from the main wreckage, which was about 230 ft from the end of the runway surface. The tracks on the runway veered to the right and continued through the soft dirt area, between the runway edge lights. The tracks were not present in several areas of the dirt, the longest of which was when the terrain sloped down to the drainage consistent with the airplane leaving the ground just prior impacting the concrete culvert. 

Marana Regional Airport was an uncontrolled airport equipped with four runways. Runway 03 was equipped with a 2-light PAPI (precision approach path indicator) system with an approach slope of 2.9° located to the left. The runway was equipped with MIRL (medium intensity runway lighting system) which outlined the runway with lights. The runway measured 3,892 ft long by 75 ft wide, with a displaced threshold of 494 ft, which provided a landing distance available of 3,398 ft (see figure 5 below). There was a Notice to Airman (NOTAM) active for the airport stating that runways 12 and 30 (6,901 ft in length) were closed between April 6th and 13th.

Cessna 172M Skyhawk, N61972, accident occurred on April 5, 2026, at Lakeland Linder International Airport (LAL/KLAL), Sanford, Florida

  • Location: Lakeland, FL 
  • Accident Number: ERA26LA159 
  • Date & Time: April 5, 2026, 00:07 Local 
  • Registration: N61972 
  • Aircraft: Cessna 172M 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202755/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N61972

On April 05, 2026, at 0007 eastern daylight time, a Cessna 172M airplane, N61972, was substantially damaged when it was involved in an accident near Lakeland, Florida. The pilot and certified flight instructor (CFI) rated passenger were uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he was conducting touch-and-go landings at Lakeland Linder International Airport (LAL), Lakeland, Florida. About 3 to 4 seconds after his ninth takeoff, the airplane pitched up uncontrollably to an unusually high attitude. The pilot attempted to pitch the nose of the airplane down; by applying full forward pressure to the control yoke. Realizing the flap switch was in the down position, he moved it up but still struggled to correct for the nose high attitude.

The CFI rated passenger assisted the pilot on the airplane’s flight controls, and together they were able to obtain a level flight attitude. The CFI rated passenger then retarded the throttle to idle, and believing the engine was no longer producing power, declared an emergency with the air traffic control tower. He then maneuvered the airplane toward a lighted airport cargo ramp near the departure end of the runway. The airplane landed hard between the cargo ramp and a taxiway, impacted a berm and nosed over, coming to rest inverted.

Surveillance video captured the accident sequence and showed that after touchdown, the airplane bounced, impacted the nose wheel on the ground, before nosing over and coming to rest inverted. The airplane sustained substantial damage to the firewall, wings and vertical stabilizer.

The airplane was equipped with an Electronics International Incorporated CGR-30 engine monitor.

The airplane and its engine monitoring system were retained for further examination.

Just Highlander, N563JA, accident occurred on April 8, 2026, near Great Falls, Montana

  • Location: Great Falls, MT 
  • Accident Number: WPR26LA152
  • Date & Time: April 8, 2026, 11:06 Local 
  • Registration: N563JA 
  • Aircraft: Just Aircraft Highlander 
  • Injuries: 1 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202787/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N563JA

On April 8, 2026, about 1106 mountain daylight time, an experimental amateur built Just Aircraft Highlander, N563JA, was substantially damaged when it was involved in an accident near Great Falls, Montana. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that after he departed Great Falls International Airport (GTF), Great Falls, Montana, he intended to land on a private grass surface airstrip about 5.5 nautical miles to the southwest. While on the final approach to the grass airstrip, he applied right rudder pedal to enter a left wing low slip to perform a steep approach along with reducing the throttle to idle to minimize the airspeed.

The pilot stated that when he decreased the throttle to idle, the engine lost total power. He aligned the nose of the airplane with the runway heading at the threshold, but the airplane’s airspeed was too fast. The airplane touched down in the last 1/3rd of the airstrip with the control stick full aft and he applied the brakes. Ground scars revealed that the nose of the airplane contacted the turf surface and skidded about six ft before the airplane nosed over near the departure end of the airstrip, which extended to the edge of the Missouri river.

A review of the airplane’s maintenance logs indicated that a condition inspection was completed on December 8, 2025, and a new SkyTrax propeller speed reduction unit and friction clutch upgrade was installed on January 18, 2026.

The wreckage has been recovered to a secure facility for further examination. 

Cessna 421C Golden Eagle II, N291AN, fatal accident occurred on April 30, 2026, near Wimberley, Texas

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=N291AN

- History of Flight:
On April 30, 2026, at about 2302 local time, a Cessna 421C Golden Eagle II, N291AN, registered to KB Flies LLC out of Amarillo, TX, was destroyed when it impacted terrain near Wimberley, Texas. The pilot and four passengers were fatally injured. The flight originated from River Falls Airport (H81), Amarillo, Texas, at 2111, and was destined to New Braunfels Regional Airport (BAZ/KBAZ), 
New Braunfels, Texas.

According to flight tracking history, on April 20, 2026, at 1516, the airplane departed H81 on a short flight to Hereford (KHRX), Texas. At 1731, the airplane returned to H81. On April 24, 2026, at 1319, the airplane departed H81 on a flight to Lubbock (KLBB), Texas. The following day, at 0922, the airplane flew back to H81. On April 30, 2026, the airplane departed H81 on the accident flight, with the presumed destination at this point being KBAZ.

According to Automatic dependent surveillance-broadcast (ADS-B) data, the airplane entered a climbing left turn to an inflight cruising altitude of 17,000 ft. The flight appeared uneventful. At 2246:09, the airplane was tracking east, but there was weather activity present ahead of the aircraft, so a right turn was started towards the south. At about 2247:37, the airplane entered a descent from cruise altitude, and based on early flight tracking imagery, occurred at the same time as the aircraft started encountering weather activity. Several airports in the area were reporting lightning and rain. At about 2250, the airplane appeared to be in a little "zig-zag" motion with notable turns as it was descending through 15,000 ft. At 2300:00, the airplane entered a 5000 feet per minute (fpm) average rate while descending through 14,000 ft. At about 2300:46, the airplane turned right and was tracking west when it stopped the descent and entered a 7000 fpm climb back to 14,000 ft and started tracking south. However, at 2301:23, the airplane was observed again in a -7000 average rate descent back towards 11,800 ft. At about 2301:30, the airplane entered a climbing right hand turn towards 14,000 ft, but at 2301:57, the airplane was now observed on a descending right hand spiral, which the airplane did not recover from. The last ADS-B data point was recorded at 6,800 ft towards the conclusion of the spiral, the airplane was at 87 knots groundspeed with a reported average rate of -11,100 feet per minute (fpm) rate.

Figure 1: ADS-B exchange data around time airplane started descent from cruise altitude

Figure 2: Data around time started first right hand descent

Figure 3: Rapid climb

Figure 2: Second rapid descent

Figure 3: Climbing right turn before spiral

Figure 4: Final ADS-B data point after spiral

Figure 5: ADS-B exchange data ran through Flysto, note that "4XS9" was automatically assigned by Flysto

Figure 2: Data around the time the airplane started a descent from cruise altitude

Figure 3: Initial left hand descent

Figure 4: Final turn

- Pilot Information:
Unknown at this point.

- Airplane Information:
The low-wing, retractable-landing-gear, pressurized, multiengine, 8-seat airplane, serial number (S/N) 421C0242, was manufactured in 1977. It was powered by two Continental Motors GTSIO-520 engines fitted with a RAM Conversion. The airplane was also equipped with RAM winglets and VG spoilers.

According to an old sale listing, the airplane had no damage history and was equipped for IFR flight, with the reported following avionics:

"Garmin 530 w/ XM Weather , TCAS I , Garmin 430 w/ Mode S Transponder Traffic Displayed , RDR 2000 Color Radar , Stormscope , Alt Preselect , Yaw Damp, Insight Graphic Engine Mon. , Hoskins digital Fuel Flow ,Fire detect/exting Known Ice , Fact Air"

- Wreckage and Impact Information:
Local authorities reported: "Preliminary information indicates the plane was traveling at a high rate of speed at the time of impact, and that there is no indication of a mid-air collision."

Post-accident photos revealed that the main wreckage consisted of the fuselage, both wings, and tail, which were in a wooded area and was consumed by a post crash fire. The wreckage was oriented upright and there were no angular cuts in the trees surrounding the main wreckage.

The on-scene photos suggests the main wreckage came down flat, with little to no forward speed. It is unknown if the aircraft suffered an inflight breakup during the out of control spiral, which may have led to the main wreckage coming down in this way.

- Weather:
(1) Brief:

The reported weather conditions at KHYI at 2256 included: Winds 010 at 13 knots, 10 miles visibility, an overcast ceiling at 1,100ft AGL, temperature 19°C, dewpoint 18°C, an altimeter setting of 29.91 inches of mercury, with additional remarks of distant lightning to the southeast, and nearby rain.

The reported weather conditions at KAUS at 2253 included: Winds 030 at 13 knots, gusting 22 knots, 10 miles visibility, light rain, a scattered ceiling at 900ft AGL, a broken layer at 1,400 ft AGL, an overcast ceiling at 2,600ft AGL, temperature 19°C, dewpoint 18°C, an altimeter setting of 29.89 inches of mercury, with additional remarks of distant and occasional lightning to the east, and nearby rain.

The reported weather conditions at KBAZ at 2251 included: Winds 060 at 14 knots, gusting 21 knots, 10 miles visibility, an overcast ceiling at 1,300ft AGL, temperature 19°C, dewpoint 17°C, an altimeter setting of 29.85 inches of mercury, with additional remarks of distant lightning to the southeast, and nearby rain.

A review of the NWS Area Forecast Discussion for the San Antonio, Texas, showed that there were reports of isolated to scattered thunderstorms for the night into early Friday evening, with locally heavy rain.

(2) METARs:

METAR KHYI 010356Z 01013KT 10SM OVC011 19/18 A2991 RMK AO2 LTG DSNT SE RAB04E20 SLP123 P0000 T01940178

METAR KHYI 010456Z 05014KT 10SM -RA OVC011 19/17 A2989 RMK AO2 LTG DSNT SE RAB46 SLP115 P0000 T01890172

METAR KAUS 010353Z 03013G22KT 10SM -RA SCT009 BKN014 OVC026 19/18 A2989 RMK AO2 LTG DSNT E RAB11 CIG 010 RWY17R SLP118 OCNL LTG DSNT E P0001 T01890178

METAR KAUS 010453Z 03010G19KT 10SM BKN007 18/17 A2990 RMK AO2 RAE19 SLP120 P0000 T01830172

METAR KBAZ 010444Z AUTO 05012G20KT 10SM BKN013 OVC020 19/17 A2987 RMK AO2 RAB17E39 P0000 T01890172

METAR KBAZ 010451Z AUTO 06014G21KT 10SM OVC013 19/17 A2985 RMK AO2 LTG DSNT SE RAB17E39 PRESFR SLP101 P0000 T01890172

METAR KBAZ 010551Z AUTO 04017G22KT 10SM -TSRA SCT011 OVC017 19/17 A2989 RMK AO2 LTG DSNT ALQDS RAB43 TSB40 SLP115 P0001 60001 T01890167 10233 20189 402500161 53001

(3) Additional:

WSUS32 KKCI 010355

SIGC 

CONVECTIVE SIGMET 11C

VALID UNTIL 0555Z

TX

FROM 60WNW LFK-30SW LFK-20SSW IAH-40S SAT-20NW SAT-60WNW LFK

AREA TS MOV FROM 25035KT. TOPS TO FL360.

OUTLOOK VALID 010555-010955

FROM INK-ACT-IAH-PSX-LRD-DLF-MRF-INK

WST ISSUANCES EXPD. REFER TO MOST RECENT ACUS01 KWNS FROM STORM

PREDICTION CENTER FOR SYNOPSIS AND METEOROLOGICAL DETAILS.

(4) Area Forecast Discussion:

529
FXUS64 KEWX 302342
AFDEWX

Area Forecast Discussion
National Weather Service Austin/San Antonio TX
642 PM CDT Thu Apr 30 2026

...New AVIATION...

.KEY MESSAGES...

- Isolated to scattered thunderstorms are forecast for the rest of today
  into early Friday evening. Some could be strong to marginally
  severe.

- Locally heavy rain is forecast to affect some locations across
  South Central Texas through early Friday evening and a Flood
  Watch has been issued.

- Dry and cooler weather for the weekend with a warming trend
  forecast for the work week.

&&

.SHORT TERM...
(Tonight through Friday night)
Issued at 114 PM CDT Thu Apr 30 2026

Latest visible imagery shows cloudy skies across most of South
Central Texas with some breaks over the Coastal Plains. A mid to
upper level shortwave moving across the Hill Country is helping
shower and thunderstorm activity across the Hill Country especially
over portions of Burnet, Blanco, and soon over Travis counties as
of 1 PM CDT. This activity could be enhanced as the afternoon
progresses with more activity expanding over parts of the southern
Edwards Plateau. Main hazards are large hail, strong to damaging
wind gusts, and localized heavy rain. We may have a lull in
activity later this afternoon into the early evening, but showers
and thunderstorms return over the Rio Grande mid to late evening
and then move eastward overnight into Friday afternoon and
possibly through early Friday evening. These storms will have the
support of an upper level short wave pushing from Baja California
into northern Mexico into west Texas and then over our local area
throughout the day Friday. There is a moderate to high confidence
on locally heavy rain across a good portion of South Central Texas
late this evening through Friday evening as several rounds of
heavy rain affect the local area. A Flood Watch is in effect from
9 PM CDT this evening through 9 PM CDT Friday. Rainfall amounts of
2 to 4 inches are forecast with isolated 6 inches for the
duration of the Flood Watch. Remember to promote the following:
Stay weather aware and away from flooded areas. As the wave moves
to the east of the local area Friday afternoon through the
evening, rain chances come to an end from west to east. Breezy
north winds are forecast to prevail late Friday afternoon through
the overnight hours with gusts of 30 to 40 mph.

&&

.LONG TERM...
(Saturday through next Thursday)
Issued at 114 PM CDT Thu Apr 30 2026

By Saturday morning, dry and cooler weather conditions are in store
as a surge of cooler airmass pushes from the north resulting in lows
around the mid 40s over the Hill Country to mid 50s across the
Coastal Plains. Saturday`s highs are forecast to range from the
upper 60s to mid 70s. A surface high pressure system over South
Central Texas Saturday evening pushes to the east overnight into
Sunday and brings back a southerly flow to the local area. With the
return flow in place, a warming trend begins on Sunday with forecast
highs in the mid to upper 70s to low 80s along the Rio Grande.
The warming trend and dry weather conditions continue at least
through next Wednesday.

&&

.AVIATION...
(00Z TAFS)
Issued at 640 PM CDT Thu Apr 30 2026

Over the next 24 hours, several fast-moving clusters and bands of
TSRA/SHRA are expected to move west to east across the region.
Activity is forecast to be most numerous between 09Z-21Z. The 00Z
TAFs provide a general sketch of the more favored periods for TS,
but the main takeaway is that the weather will be quite active.
Rounds of more intense TSRA may be separated by SHRA or BR, with
broad lowering to IFR CIGs expected tonight. Periods of LIFR CIGs
are possible between 09Z-15Z at all TAF sites, but confidence was
too low to highlight in the TAFs. Prevailing winds will increase
towards gusty northeasterlies at KAUS/KSAT/KSSF, mainly after 17Z
with peak gusts occurring around 00Z. Hi-res models suggest gusts
of about 28-33 kt are likely. CIGs may slowly improve during the
day, especially following the last round of storms in the mid- to
late-afternoon, with the slowest improvement at KAUS and vicinity
compared to other sites.


&&

.PRELIMINARY POINT TEMPS/POPS...
Austin Camp Mabry              60  63  53  74 /  90  90  20   0
Austin Bergstrom Intl Airport  61  64  51  73 /  90 100  20   0
New Braunfels Muni Airport     61  66  52  74 /  90 100  10   0
Burnet Muni Airport            56  60  50  71 /  90 100  20   0
Del Rio Intl Airport           65  73  54  74 /  90  90  10   0
Georgetown Muni Airport        59  61  50  72 /  90 100  20   0
Hondo Muni Airport             63  66  50  72 /  90  90  10   0
San Marcos Muni Airport        61  65  52  73 /  90 100  20   0
La Grange - Fayette Regional   63  67  53  73 /  90 100  30   0
San Antonio Intl Airport       63  66  52  73 /  90  90  10   0
Stinson Muni Airport           64  67  54  73 /  90  90  10   0

&&

.EWX WATCHES/WARNINGS/ADVISORIES...
Flood Watch through Friday evening for TXZ171>173-183>194-
202>209-221-223.

&&

$$

SHORT TERM...17
LONG TERM....17
AVIATION...Tran

- Additional Information:
No

Sys/Comp malf/fail (non-power): Consolidated PBY-5A Catalina, N222FT, accident occurred on October 31, 2025, at Mark Anton Airport (2A0), Dayton, Tennessee

  • Location: Dayton, Tennessee
  • Accident Number: ERA26LA028
  • Date & Time: October 31, 2025, 18:00 Local
  • Registration: N222FT
  • Aircraft: Consolidated Vultee 28-5ACF
  • Aircraft Damage: Substantial
  • Defining Event: Sys/Comp malf/fail (non-power)
  • Injuries: 3 None
  • Flight Conducted Under: Part 91: General aviation - Flight test

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/201944/pdf

https://data.ntsb.gov/Docket?ProjectID=201944

The airplane had been out of service for six months due to leaking hydraulic sequence valves. Following installation of the repaired components, maintenance personnel cycled the landing gear multiple times through its full range of travel. System pressure was maintained and no leaks were observed. The airplane was subsequently serviced with fuel, oil, and hydraulic fluid in preparation for a maintenance test flight. 

The pilot reported that a preflight inspection was completed, and the three crew members boarded the airplane for departure. The before takeoff checks, including a full power run-up of both engines, were completed with no anomalies noted. After takeoff and following the selection of the landing gear to the up position, at about 300 ft above ground level (agl), the flight engineer noticed they were losing hydraulic fluid from the right main landing gear. The left main and nose landing gear had fully retracted; however, the right main landing gear was partially retracted and not in its wheel well. The auxiliary hydraulic pump was selected on, followed by the selection of the landing gear to the down position. The left main gear subsequently indicated down and locked with the green gear position light illuminated; however, the nose gear was in the up position, and the right main landing gear was down but not locked. 

The flight crew climbed the airplane to about 1,500 ft agl and circled the airport, while the emergency landing gear extension procedure was performed. Following completion of the procedure, the three landing gear green position lights were illuminated indicating that the landing gear was down and locked, and the hydraulic system indicated no system pressure. The flight crew conducted a low pass over the airport while communicating with ground personnel who visually confirmed that three landing gear were in the down position.

The airplane returned for landing, and the before landing checklist was completed. Upon touchdown, about 1,500 ft down the runway, the left main landing gear slowly retracted, and the airplane began to veer left. The pilot applied right brake and full right rudder in an attempt to correct for the veer, to no avail. The airplane departed the left side of the runway, the left wing struck a sign before impacting the ground, which resulted in substantial damage to the left wing and hull. 

Postaccident examination of the airplane revealed that all three green landing gear position lights were illuminated; however, the left main landing gear had collapsed. Further examination revealed that the left main landing gear hydraulic actuator attachment bolt had sheared at the lower actuator attach point. In addition, the right wheel well was coated in hydraulic fluid, and the leak appeared to be from a hydraulic line that ran from the bottom of the actuator to the sequence valve. 

Examination of the failed landing gear bolt revealed reverse bending fatigue resulting from bending loads. The fractured surface exhibited a distinct overstress region with beach marks visible on both sides.

- Probable Cause: The collapse of the left main landing gear due to the fatigue fracture of the lower landing gear actuator bolt.

The Airplane Factory Sling LSA, N166TW, fatal accident occurred on April 9, 2026, in Avalon, California

  • Location: Avalon, CA 
  • Accident Number: ANC26FA024 
  • Date & Time: April 9, 2026, 12:24 Local 
  • Registration: N166TW 
  • Aircraft: AIRPLANE FACTORY (PTY) LTD THE SLING 
  • Injuries: 2 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202790/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N166TW

On April 09, 2026, about 1224 Pacific daylight time, an Airplane Factory (Pty) Ltd. Sling 2 airplane, N166TW, was substantially damaged when it was involved in an accident near Avalon, California. The pilot and pilot-rated passenger were fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The pilot and pilot-rated passenger departed Zamperini Field Airport (TOA), Torrance, California, at 1153 on a personal flight to Santa Catalina Island, California. Preliminary Automatic Dependent Surveillance-Broadcast (ADS-B) data showed that the airplane departed TOA, crossed open water and arrived over Santa Catalina Island at Blue Cavern Point. The airplane then crossed a ridge and flew southbound through a canyon east of Little Harbor Road before crossing another ridgeline, intersecting the Trans Catalina Trail north of Shark Harbor. The airplane subsequently followed the southern coastline before the ADS-B signal was lost about a mile southwest of the accident site.


A witness, located on the ground hiking the Trans Catalina Trail, reported seeing a low flying airplane dip into Little Springs Canyon, cross over the ridgeline that the trail traversed, and continue a southwesterly heading. The witness noted that the airplane appeared to be less than 50 ft above the ridgeline and was never seen flying more than 100 ft above the ground. ADS-B data, cross-referenced with GPS unit data provided by the hiker, indicated that the airplane witnessed was likely N166TW. This encounter occurred about 11 minutes before the time of the accident, about 9 miles northwest of the accident site.


The airplane impacted terrain and came to rest on the down sloping side of a steep canyon, about 400 ft southwest of the intersection of Divide Road and Avalon Canyon Road. All four corners of the airplane were accounted for at the accident site. The wreckage was oriented with the nose low and empennage elevated at a high angle above the terrain. The tail section from the forward horizontal stabilizer sustained impact damage and remained attached to the aft fuselage only by the elevator push pull tube. The engine compartment and lower fuselage, to about mid-fuselage, were compressed upward and aft into the firewall and instrument panel. This impact damage, combined with the difficult terrain, prevented the confirmation of flight control continuity at the scene. The ignition switch was on, and the fuel selector was positioned to the left tank. The flap setting cockpit indications and the position of the flaps indicated that they were fully retracted at the time of impact. The ballistic parachute rocket, installed in the airplane, had not been deployed. 

Data cards and motherboards from avionics, along with other electronic devices aboard the accident airplane, were retained and sent to the NTSB Recorders Lab in Washington D.C. for flight data extraction. 

The wreckage has been recovered to a secure facility for further examination.

Piper J3C-65 Cub, N92480, accident occurred on April 10, 2026, near Crestview, Florida

  • Location: Crestview, FL 
  • Accident Number: ERA26LA168 
  • Date & Time: April 10, 2026, 17:00 Local 
  • Registration: N92480 
  • Aircraft: Piper J3C-65 
  • Injuries: 1 Serious, 1 Minor 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202816/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N92480

On April 10, 2026, about 1700 eastern daylight time, a Piper J3C-65, N92480 was substantially damaged when it was involved in an accident near Baker, Florida. The pilot sustained minor injuries, and the passenger was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot stated that before the first flight, he performed a preflight inspection and added .5 quart of oil to bring the quantity to about 3.5 quarts. He then taxied to the fuel pump and topped off the fuel with about 9 gallons of 100LL aviation fuel. According to the Piper J3C-65 owner’s manual, the fuel tank capacity is 12 US gallons.

The pilot departed Skypark Estates Owners Assoc Airport (18FD) in Baker, Florida, about 1600 and flew for about 35 minutes to perform local pattern work. He subsequently landed and parked the airplane, remaining on the ground for about 30 minutes, before performing a preflight inspection with no anomalies noted. About 1700 the pilot departed with a passenger seated in the front seat. After takeoff, the airplane climbed to about 1,500 ft above ground level (agl) and proceeded to Long Branch Farms Airport (2FA3) in Baker, Florida, a flight of about 10 minutes.

Upon arrival at 2FA3, the pilot descended to 1,000 ft agl with a slight reduction in power and crossed mid-field to enter the airport traffic pattern on a left downwind leg for runway 27. Carburetor heat was turned on, and engine power was reduced to about 1,500 rpm during the descent on the base and final legs of the pattern. On short final, carburetor heat was turned off, and the engine was advanced to cruise power as the airplane leveled off at about 50 ft agl to conduct a low approach to inspect runway conditions.

Following the low approach, the pilot applied full power for a normal climb at about 60 mph. About 200 ft agl the engine lost all power. The pilot confirmed the throttle lever was full forward, lowered the nose, and turned toward a field, attempting to fly through a small gap in the trees near its edge. The pilot observed power lines crossing the field and tightened the turn to avoid them. The right wing contacted a tree, which resulted in a significant yaw to the right and a decrease in airspeed. The airplane then yawed back to a forward direction and impacted the ground at a steep downward angle. The airplane sustained substantial damage to the fuselage and wings.

The wreckage was retained for further examination.