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Accidents · NTSB CEN26LA161 · Final report

Flight Design GMBH CTSW accident near Seguin, Texas, April 7, 2026

On April 7, 2026 at about 1:00 am local time, a 2006 Flight Design GMBH CTSW, registered N249CT, was substantially damaged in an accident during landing (landing roll) near Seguin, Texas (Huber Airpark Civic Club LLC airport). It was an instructional flight under general aviation rules (Part 91). No one was hurt; 2 people were on board or involved. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

The failure of the landing gear weldment that resulted in separation of the right main landing gear.

Source: NTSB aviation accident database, copy made November 2, 2026. Docket and reports at the NTSB.

What the record shows

Date
April 7, 2026 · about 1:00 am local time · cases in 2026
Place
Seguin, Texas · Huber Airpark Civic Club LLC · cases near this airport · map
Type
Accident
Injuries
No one was hurt; 2 people were on board or involved.
Weather
visual conditions (good weather)
Aircraft
Flight Design GMBH CTSW, built 2006 · all CTSWs on the register
Registration
N249CT · registry record · serial 06-11-14
Damage
Substantial damage
Flight
Instructional flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

The student pilot reported that during the instructional flight the first landing was normal. The second approach and landing were also normal, but the airplane began to veer to the right during the landing rollout. The flight instructor took control of the airplane and performed an aborted landing. After communicating with another pilot who was on the ground at the airport, they determined that the right main landing gear wheel had separated from the airplane. On the subsequent landing, the airplane landed in the grass short of the paved runway, the remnants of the right main landing gear dug into the ground, and the airplane yawed sharply to the right. The airplane sustained substantial damage to the left wing and fuselage. Examination of the airplane after the accident revealed that the welded structure that held the wheel and wheel axle to the round landing gear leg had fractured. The lower portion of the weldment, along with the wheel and brake assembly, were found on the runway. Examination of the weldment showed a buckled portion of tube below the attachment to the round gear leg. The buckling was consistent with a hard landing occurring at some point in the life of the part. There was a complete fracture of the tube just above the buckled section and the interior of the tube was corroded. The fracture surfaces had features consistent with overstress failure. Based on the student pilot’s account and the physical evidence it is likely that the landing gear weldment had previous damage that went undetected until failure during the accident flight.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Landing gear collapse during landing (landing roll) defining event

The NTSB's findings

Pilot

  • Certificate: student
  • Flight time: 40 hours in all; 25 in this make and model
  • Medical certificate: Sport Pilot
  • Seat: left
  • Injury: no injuries

Flight instructor

  • Certificate: flight instructor, commercial pilot
  • Ratings: multi-engine land; single-engine land; instructor: airplane single-engine; instructor: instrument airplane; instrument: airplane
  • Flight time: 330 hours in all; 26 in this make and model; 45 in the last 90 days; 32 in the last 30 days; 186 as pilot in command; 35 on instruments
  • Last flight review: February 5, 2026
  • Medical certificate: Class 1 (without waivers/limitations)
  • Seat: rgt
  • Injury: no injuries

The aircraft

  • Airframe total time: 3,635 hours
  • Last inspection: condition inspection, February 12, 2026; 31 hours since
  • Maximum gross weight: 1,320 lb
  • Seats: 2
  • Landing gear: fixed
  • Engine: Rotax 912ULS (piston); 2,077 hours total

The flight

  • Flight plan: none
  • Runway 18/3, 3,415 ft by 50 ft
  • A second pilot was aboard

Weather at the time

  • Light: dusk
  • Wind: from 040° at 6 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 66°F (19°C), dew point 37°F (3°C)
  • Altimeter: 30.13 inHg
  • Observation at 7:51 pm from KBAZ, 7 miles away

Weather report (METAR): METAR KBAZ 070051Z AUTO 04006KT 10SM CLR 19/03 A3013 RMK AO2 SLP199 T01890033=

Injuries

FatalSeriousMinorNone
Flight crew2

Documents from the investigation the NTSB's docket: the evidence folder behind the report

The NTSB has not released the docket for this case yet. The docket, the folder of records gathered during an investigation (maintenance records, photographs, witness statements, examinations), is usually released when the investigation is nearly complete, and the list here is refreshed when it appears. Check at the NTSB.

Connections how this case links to the rest of the register

Aircraft
Place

The whole map of how records connect · these connections as data: /graph/accident/CEN26LA161.json.

The bigger picture in Aviation Analytics: accidents over time since 1982, by model, by phase of flight and conditions, by place and on the map.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text does not name anyone involved, its policy at this time. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.