Tuesday, March 17, 2026

Aero Commander 500B, N444CA, fatal accident occurred on March 17, 2026, at Spirit of St. Louis Airport (SUS/KSUS), St Louis, 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=N444CA

- History of Flight:
On March 17, 2026, at 0324 local time, an Aero Commander 500B, N444CA, registered to Central Airlines Inc and doing business as Central Air Southwest, was destroyed when it was involved in an accident at Spirit of St. Louis Airport (SUS/KSUS), St Louis, Missouri. The sole pilot onboard was fatally injured. The cross-country Part 135 cargo flight originated from KSUS and was destined to New Century AirCenter (JCI/KIXD), 
Olathe, Kansas.

According to preliminary automatic dependent surveillance-broadcast (ADS-B) data, at 0321:51, the airplane was observed departing runway 26L about 2,700 ft down the 7,486 ft runway when it entered a climbing right turn over the airport to an altitude 600 ft. The groundspeed was sluggish and averaging about 60 knots. At 0322:40, the airplane started a climb to 675 ft which was followed by a descent to 600 ft and another climb, this time to 850 ft, the groundspeed started averaging around 80 knots at this point. At 0323:28, the airplane was at 900 ft and 80 knots groundspeed when it began a descent for runway 26L. At 0323:57, the last ADS-B return was recorded about 0.24 mile from the runway threshold. The airplane was at 500 ft, 60 knots groundspeed, with an average rate of -5300 feet per minute (fpm).

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

Figure 2: ADS-B exchange data for accident flight.

There were no known witnesses to the accident at the time of this writing.

- Pilot Information:
Unknown.

- Airplane Information:
The airplane, serial number 1458-162, was a high wing, two-engine airplane manufactured in 1964. It was powered by two 300-horsepower Continental Motors IO-520 engines. Each engine drove a metal, three-bladed, variable pitch, Hartzell fullfeathering propeller.

The minimum control speed for this aircraft type, which is the minimum speed at which the airplane is controllable in flight, with sudden failure of one engine and takeoff power on the other engine is 61 knots. 

According to the airplane flight manual, the stall speed in level flight with the wing flaps extended was 59 knots (68 miles per hour).

- Wreckage and Impact Information:
The airplane came to rest upright and was consumed by a post crash fire. The fire spread to both wings and tail.

- Airport Information:
Spirit of St Louis Airport is a public airport located 17 miles west of St Louis, Missouri. The airport field elevation is 463.3 ft. The airport features two runways, runway 8R/26L concrete/grooved in good condition which is 7486 x 150 ft, and runway 8L/26R asphalt/rubberized friction seal coat in good condition which is 5000 x 75 ft.

- Weather:
(1) Brief:
The reported weather at KSUS at 0254 LT, included: Winds 310 at 8 knots, 10 mile visibility, no clouds under 12,000 ft (CLR), temperature -7 °C, dewpoint -14 °C, and an altimeter setting of 30.18 inches of mercury.

(2) METARs:

METAR KSUS 170754Z AUTO 31008KT 10SM CLR M07/M14 A3018 RMK AO2 SLP230 T10671139 $

METAR KSUS 170854Z AUTO 29005KT 10SM CLR M07/M13 A3019 RMK AO2 SLP234 T10721133 53007 $

(3) Area Forecast Discussion:

Area Forecast Discussion
National Weather Service Saint Louis MO
211 AM CDT Tue Mar 17 2026

.KEY MESSAGES...

- Today`s temperatures will be slightly milder than Monday, but remain
  around 20 degrees below normal with highs in the 30s to low-
  40s.

- Light snow is expected over sections of northeast Missouri and west-
  central Illinois tonight. Accumulations remain under an inch.

- Temperatures warm significantly from Wednesday through the end
  of the week with highs expected to be well above normal.


&&

.SHORT TERM...  (Through Late Wednesday Afternoon)
Issued at 205 AM CDT Tue Mar 17 2026

Skies have cleared out over much of the area with the only semblance
just now exiting the eastern fringes of the CWA. Surface
observations show gusts continuing to subside with sustained winds
dropping below 10 mph over central Missouri. This eastward will
continue through early morning, which may allow low temperatures to
cool a bit more efficiently that previously thought. Mornings lows
could be trimmed just a hair, but negligible in sensible terms. Most
locations wake up to the teens with a few single digit readings in
northeast Missouri.

Subtle warming is expected today after such a cold start. Calling it
a warm-up may be more insulting that truthful with highs largely in
the 30s to near 40 degrees. We`re ahead of a weak clipper system
that will bring additional clouds to the region through the
afternoon. How quickly this occurs could stymie diurnal trends,
mainly over central and northeast Missouri. The favored northern
track, quick pace, and lack of moisture will keep winter hazards at
bay. An added benefit is that precipitation chances largely lie
between sunset tonight and sunrise Wednesday morning.

The clipper rides along a wing of strong warm air advection with
surface temperatures at or above freezing from Kirksville to St.
Louis through Mt. Vernon (IL) through tonight. The warm nose
continues to cut into northeast fringes of the CWA between 09z-11z
prior to sunrise, resulting in slowly rising temperatures between
06z-12z tonight into early Wednesday morning. Even the coldest
locations across the northeast fringes of the CWA only bottom out in
the low-30s. HREF spreads have been consistently showing around
0.05" of QPF from KUIN through K3LF. There`s also reassurance in the
LPMM data that shows an inch of accumulation in these areas.
Realistically, maybe an inches is achieved north of KUIN with less
than an inch elsewhere. Moisture depth decreases southwest from
there with a more notable dry layer in the surface to mid-level
layer. What moisture is available is likely to be very light and in
liquid form. No hazards are expected at this time.

There is high confidence in a significant warm-up starting Wednesday
as a ridge axis crosses the region, shifting winds out of the
southwest. H8 temperatures climb about 10C with highs largely in the
60s.


Maples

&&

.LONG TERM...  (Wednesday Night through Monday)
Issued at 205 AM CDT Tue Mar 17 2026

The later half of the week features much warmer temperatures that
will compare closer to the first half of May. NBM IQR provides high
confidence in the warm-up with just a few degrees of separation
between the 25th/75th percentiles. Global deterministic guidance
shows mid-level temperatures inching upward through this stretch,
starting out at 10-15C Thursday and near 20C Saturday. This will
bring temperatures into the 60s/70s Thursday and well into the 70s
Friday. Saturday is a touch warmer than Friday, which includes low-
80s over sections of central and southeast Missouri. Prominent flow
at the surface is more westerly than southwesterly and therefore
does not indicate much potential for over-performance. NBM output
looks reasonable with IQR remaining tightly clustered through
Saturday.

Sunday remains the biggest question with relation to a cold front
that brings cooler air to the region. This morning`s deterministic
ECMWF/GFS are in fair agreement with the surface front arriving in
the early morning over northern Missouri/west-central Illinois, mid-
morning along I-70, and by 18z over the southern stretch of the CWA.
NBM spreads around 30 degrees persist, which is largely playing off
the warmer ECMWF solutions from prior runs. This spread also shows
up in the HREF ensembles, but I suspect this will begin to tighten
over the next couple of run as we draw closer to the weekend. That
being said, most areas along and north of I-70 likely reach their
high temperatures in the early part of the day, then follow a non-
diurnal trend through the afternoon. 70s are most favored across
southeast Missouri and southwest Illinois as 20-25C H8 air is
compressed along and just ahead of the boundary with some time for
normal diurnal processes to have greater influence on temperatures.
Considering the surface ridge remains to our southwest ahead of the
front, moisture return is lacking until the front approaches the
Missouri/Arkansas border. Thus, a dry FROPA is favored.

A strong surface ridge builds eastward through the north-central
U.S. early next week. NBM spreads aren`t terribly large (~10
degrees) with the most notable characteristic being an initial drop
in temperature Monday with modest moderation thereafter.


Maples

&&

.AVIATION...  (For the 06z TAFs through 06z Tuesday Night)
Issued at 1232 AM CDT Tue Mar 17 2026

Skies have cleared and winds continue to die off at all terminals
early this morning. A quick-moving clipper system passes over the
region tonight with light rain/snow possible, mainly around KUIN.
Surface to mid-levels become increasingly dry southwest of KUIN,
including central Missouri/metro terminals. The lack of moisture
and quick pace of this system may not provide much opportunity to
overcome the dry layer. Therefore, the only mention of -SN is at
KUIN. Even in this instance cloud bases remain VFR with MVFR
skimming northeast of KUIN through central Illinois.

- Additional Information:
No

Friday, March 13, 2026

Falconar F12A Cruiser, N30P, fatal accident occurred on February 26, 2026, near Rogers, Arkansas

  • Location: Rogers, AR 
  • Accident Number: CEN26FA126 
  • Date & Time: February 26, 2026, 13:30 Local 
  • Registration: N30P 
  • Aircraft: PECK JODEL-F12
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202558/pdf

https://registry.faa.gov/aircraftinquiry/Search/NNumberResult?NNumbertxt=N30P

On February 26, 2026, about 1330 central standard time, a Peck Jodel-F12, N30P, experimental airplane, was destroyed when it was involved in an accident near Rogers, Arkansas. The pilot sustained fatal injuries. The airplane was operated under Title 14 Code of Federal Regulations as a Part 91 as a personal flight.

According to the owner of the Ozark Aerodrome (AR11), Rogers, Arkansas, the airplane had not flown for about 2 – 2 ½ years, and the pilot had performed maintenance on the airplane in preparation for the accident flight. The pilot planned on moving the airplane due to the closure of AR11 in April 2026. The pilot departed from Ozark Aerodrome (AR11), Rogers, Arkansas, about 1327, to move the airplane to Springdale Municipal Airport (ASG), Springdale, Arkansas, due to the planned closure.

AR11, the accident site, and the location of witness 1, who was located at a private airstrip, are shown in Figure 1.

Witness 1 stated that he heard the airplane with what sounded like a rough running engine, as if it had a magneto problem, west of the accident site. As the airplane approached the witness’s location, the engine sound became louder and continued to run with the same roughness. The witness stated that a westerly wind was present at the time of the accident. The witness stated that an airplane soon appeared from the west and headed east over his property, which had a private east/west runway (1,000 ft by 50 ft, turf) in useable condition. The airplane was high and fast, but the witness thought it may have been trying to land. The airplane looked as if it was going to side slip, but the engine did not slow down. The airplane descended to about 25 ft above the runway but did not touch down. When the airplane was over the end of his property, it started to climb and turned slightly right to a south heading as it flew out over Beaver Lake, Rogers, Arkansas. The turn initially appeared shallow, and the engine was still running rough. The airplane’s right turn looked as if it increased and the airplane’s right roll increased as it entered a nose-down descent into Beaver Lake.

The airplane wreckage was recovered from Beaver Lake and retained for further examination.

Cessna T210M Turbo Centurion, N19FB, fatal accident occurred on March 4, 2026, in Deerfield, Illinois

 

  • Location: Deerfield, IL 
  • Accident Number: CEN26FA132 
  • Date & Time: March 4, 2026, 21:45 Local 
  • Registration: N19FB 
  • Aircraft: Cessna T210M 
  • Injuries: 1 Fatal 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202602/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N19FB

On March 4, 2026, about 2145 central standard time, a Cessna T210M airplane, N19FB sustained substantial damage when it was involved in an accident near Deerfield, Illinois. The pilot was fatally injured. The airplane was operated under Title 14 Code of Federal Regulations Part 91 as a personal flight.

The airplane departed from an unknown location; however, the first ADS-B data for the airplane began southeast of Necedah Airport (DAF), Necedah, Wisconsin, about 2040. According to the pilot’s logbook, he had flown to DAF in the months preceding the accident. The pilot was en route to Chicago Executive Airport (PWK), Chicago, Illinois, about 150 nautical miles (nm) southeast of DAF. The flight began as a visual flight rules flight, and the pilot filed an in-flight instrument flight rules flight plan about 2049.

The pilot was conducting the RNAV 16 approach to PWK when air traffic control (ATC) issued a low altitude alert about 6 nm northwest of PWK. The pilot acknowledged the low altitude alert, and the airplane climbed about 100 ft but then began to descend. ATC issued another low altitude alert, and the pilot acknowledged the alert again, and said, “I am climbing back.” ATC then alerted the pilot that he was drifting west of course, and there were no further transmissions from the pilot.

The airplane impacted 50 ft tall trees and then the roof of a townhouse before coming to rest inverted into a residential backyard. The townhouse resident was sitting in the second floor bedroom at the time of the accident, and she reported that the engine was loud and operating before the airplane impacted the roof.

The debris field was measured about 550 ft long and on a magnetic heading of about 050°. Multiple tree branches displayed cuts at 45° angles and a broom straw appearance. At the beginning of the debris field was the left wingtip and part of the left aileron. The debris field consisted of fragmented sections of the outboard left and right wings. The propeller assembly separated from the engine and was located in the debris field. All three propeller blades were twisted and exhibited rotational scoring. Two of the propeller blades had gouges in the leading edges. The main wreckage consisted of the fuselage, inboard portions of the wings, and the empennage. The fuel tanks, including the auxiliary tanks, were compromised, and the total fuel at the time of the accident could not be verified. First responders reported a strong smell of aviation fuel on the ground when they arrived. The fuel strainer was removed, and the strainer bowl contained fuel. The fuel selector was on the right tank. The instrument panel was crushed, and the altimeter’s barometric pressure setting in the Kollsman Window displayed 30.04 inHg.

The airplane was retained for further examination

Piper PA-46-350P Malibu Mirage, N91MK, accident occurred on January 24, 2026, near Sioux Gateway Airport (SUX/KSUX), Sioux City, Iowa

  • Location: Sioux City, IA 
  • Accident Number: CEN26LA100 
  • Date & Time: January 24, 2026, 07:12 Local 
  • Registration: N91MK 
  • Aircraft: PIPER AIRCRAFT INC PA 46-350P 
  • Injuries: 2 None 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202341/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N91MK

On January 24, 2026, about 0712 central daylight time, a Piper PA-46-350P airplane, N91MK, was substantially damaged when it was involved in an accident near Sioux City, Iowa. The pilot and passenger were uninjured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that after the initial climb and immediately after leveling off at 2,500 ft mean sea level, he felt the airplane make two “thugs” and observed the manifold pressure fluctuate. He subsequently observed a drop in engine oil pressure. He stated that he told the Air Traffic Control tower controller that he was going to turn back toward the airport. Once the airplane was on a north heading, a loud “boom” was heard, and a subsequent loss of engine power occurred.

The pilot executed a forced landing to a field. During the forced landing, the airplane’s engine and left wing impacted terrain and were separated. The forward fuselage and right wing sustained substantial damage.

The pilot stated that on a previous flight, four days before the accident flight, a similar “thug” was observed, but it did not result in any other abnormal indications.

The wreckage was retained for further examination.

Aerodynamic stall/spin: Cirrus SR20, N1108T, accident occurred on March 1, 2024, at Ocean Reef Club Airport (07FA), Key Largo, Florida

  • Location: Key Largo, Florida 
  • Accident Number: ERA24LA126 
  • Date & Time: March 1, 2024, 12:43 Local 
  • Registration: N1108T 
  • Aircraft: CIRRUS DESIGN CORP SR20 
  • Aircraft Damage: Substantial 
  • Defining Event: Aerodynamic stall/spin 
  • Injuries: 1 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/193867/pdf

https://data.ntsb.gov/Docket?ProjectID=193867

On March 1, 2024, about 1243 eastern standard time, a Cirrus SR20, N1108T was substantially damaged when it was involved in an accident in Key Largo, Florida. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. 

The pilot was attempting to land on a 4,451-ft-long, 70-ft-wide asphalt runway. A right 60° quartering crosswind prevailed at 10 knots, gusting to 16 knots. The pilot reported that he selected full flap extension (100%) and turned onto the final leg of the airport traffic pattern at 600 ft. Just above touchdown, while in the landing flare, the airplane drifted to the left due to a wind gust. He announced and initiated a go-around and gained altitude. The propeller and landing gear then struck the top of a tree and he lost control of the airplane. The airplane subsequently came to rest on a golf course adjacent to the runway.

Data downloaded from the airplane’s remote data module, and a postaccident examination of the wreckage, did not reveal evidence of any preimpact mechanical malfunctions. Review of airport security video revealed the airplane in about a 45° left crab to the runway, at very low altitude, with flaps fully retracted, as it entered an aerodynamic stall to the left and impacted terrain. The airplane’s flight manual indicated that the flaps should be set at 50% extension for a go-around procedure. Based on this information, the pilot’s full retraction of the flaps during the attempted go-around resulted in a loss of lift, sink, and aerodynamic stall at an altitude too low for recovery.

- Probable Cause: The pilot’s improper go-around technique, which resulted in an aerodynamic stall at an altitude too low for recovery.

Thursday, March 12, 2026

Cessna A185F Skywagon, N7574N, fatal accident occurred on February 15, 2026, near Everglades City, Florida

  • Location: Everglades City, FL 
  • Accident Number: ERA26FA115 
  • Date & Time: February 15, 2026, 11:55 Local 
  • Registration: N7574N 
  • Aircraft: Cessna A185 
  • Injuries: 1 Fatal, 1 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal 

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202436/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N7574N

On February 15, 2026, about 1155 eastern standard time, a Cessna A185F, N7574N, was substantially damaged when it was involved in an accident near Everglades City, Florida. The pilot was seriously injured, and the passenger was fatally injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

According to preliminary ADS-B data, the airplane departed from Marco Island Executive Airport (MKY), Marco Island, Florida at 1116 and flew southeast toward the coastline. The airplane followed the coastline and performed multiple turns until it reached Pavilion Key, Florida. After flying over Pavilion Key, the airplane turned northwest and proceeded back up the coastline. About 5 miles west of Everglades City, Florida, the airplane made multiple low altitude maneuvers while flying over the Ten Thousand Islands portion of the Everglades National Park. The last ADS-B data point was about .5 mile east of the accident site.

The airplane was located in the Ten Thousand Islands portion of the Everglades National Park upside down in the water. At high tide, it was observed that only the floats of the airplane were above the water line, during low tide, the floats and about half of the airplane’s fuselage were above the water line. The airplane was equipped with amphibious landing gear which was found in the “UP” (water landing) position. The water rudders were also found in the “UP” position. During the recovery of the wreckage, the airplane was turned upright, onto its floats, and towed to shore. The floats supported the weight of the airplane for several hours during the tow. After recovery, a postaccident examination of the wreckage revealed the airplane had sustained substantial damage to the fuselage, with the majority of the damage contained to the forward portion of the airplane.

Flight control continuity was established from the cockpit to all associated flight controls by manipulating the cockpit controls and observing corresponding surface movement. Binding was noted in the rudder pedals consistent with damage to the right water rudder sustained during recovery. No other flight controls exhibited unusual resistance. The flap handle was impact damaged and found in the 1st detent which is equal to 10° of flaps; however, the flaps operated normally. The horizontal stabilizer trim jack screws were measured to be 5.5 inches and was near the nose up stop.

The airplane was equipped with a 3-point shoulder harness seatbelt system for the front seats. The pilot side restraint remained attached to its installation points and was undamaged. The belt buckle was found unlatched and operated normally during testing. The copilot side restraint system remained attached to its attach points, and one of the harness restraints was cut. The belt buckle was found unlatched and operated normally during testing. The pilot seat was equipped with the inertia reel secondary seat stop, which functioned normally during testing.

The wreckage was retained for further examination.

Pipistrel Taurus 503, N414HG, accident occurred on February 9, 2026, at Willis Gliderport (FA44), Boynton Beach, Florida

  • Location: Boynton Beach, FL 
  • Accident Number: ERA26FA110 
  • Date & Time: February 9, 2026, 15:14 Local 
  • Registration: N414HG 
  • Aircraft: Pipistrel TAURUS 503 
  • Injuries: 1 Serious 
  • Flight Conducted Under: Part 91: General aviation - Personal

https://data.ntsb.gov/carol-repgen/api/Aviation/ReportMain/GenerateNewestReport/202421/pdf

https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=N414HG

On February 9, 2026, about 1514 eastern standard time, a Pipistrel Taurus 503 motorglider, N414HG, was substantially damaged when it was involved in an accident at Willis Gliderport (FA44), Boynton Beach, Florida. The pilot was seriously injured. The motorglider was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

Video with audio from a Ring camera captured the motorglider taxiing to the west end of the gliderport where it stopped facing east with the engine running for about 2 minutes and 10 seconds. The audio captured the sound of the engine rpm increasing followed by the motorglider beginning the takeoff roll. The video captured the motorglider rotating about 570 ft down the runway, the motorglider exited the camera’s field of view but the audio continued to record.

A pilot rated witness located inside his residence on the north side of the gliderport about 1,900 ft east of the western edge of the runway reported hearing the motorglider depart. When the motorglider was past his house he heard the engine quit. He went outside and observed it flying in a westerly direction about 350 ft south of the runway at an altitude of between 200 and 300 ft. He noted the engine was extended but was not running. The motorglider continued to the west a “few hundred feet” before banking to the right; the right wing dropped, and the glider descended in a nose-low attitude while rotating to the right. The motorglider impacted the ground in a near vertical position and fell back, coming to rest upright.

Postaccident examination of the motorglider which was equipped with an airframe rescue parachute revealed it was not deployed and a safety pin was in the emergency parachute release handle.

The wreckage was retained for further examination.