NTSB investigations, TX

30 cases where the sequence of events included Flight control sys malf/fail.

Cases per year

20082026
NTSB investigations, TX per year, 2008–2026: 30 cases
20082
20092
20101
20113
20122
20132
20152
20164
20183
20191
20201
20212
20232
20241
20251
20261

Latest cases

Query with SQL
duckdb -csv -c "SELECT c.\"ntsbNumber\", c.\"eventDate\", c.\"eventType\", c.\"eventCity\", c.\"eventStateOrRegion\", a.n_number, a.\"aircraftMake\", a.\"aircraftModel\", c.\"highestInjuryLevel\", c.\"totalFatal\", c.\"completionStatus\", c.report_url
  FROM 'https://openairdocs.org/data/latest/ntsb_case_detail.parquet' c LEFT JOIN 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' a ON a.case_mkey = c.\"mKey\" AND a.position = 1
  WHERE c.\"eventStateOrRegion\" = 'TX' AND c.\"eventCountry\" = 'USA'
    AND c.\"mKey\" IN (SELECT s.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' s WHERE s.\"tier2Number\" = '333' AND s.case_mkey IN (SELECT case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' WHERE \"isDefiningEvent\"))
  ORDER BY c.\"eventDate\" DESC, c.\"ntsbNumber\" DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

NTSB CEN26LA187Accident · No injuriesClass 3 · LimitedPreliminary reportCessna 172S · Denton, TXOn May 13, 2026, about 1815 central daylight time, a Cessna 172S, N2134M, sustained substantial damage when it was involved in an accident near Denton, Texas. The pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part…May 13, 2026 · N2134M · Substantial damageNTSB CEN25LA086Incident · No injuriesClass 3 · LimitedFinal reportAmerican Champion 7ECA · Longview, TXThe failure of the lower hinge barrel due to fatigue cracking. Contributing to the failure of the lower hinge barrel was increased stress from end face contact likely associated with worn bushings or displaced needle bearings.Jan 16, 2025 · N798L · Substantial damageNTSB CEN25LA043Accident · No injuriesClass 3 · LimitedFinal reportPitts S1E · Seguin, TXThe improper construction of the rudder cable assembly by the airplane builder, which resulted in the fatigue failure of the left rudder cable during the landing roll and the pilot’s subsequent inability to maintain directional control.Nov 17, 2024 · N52B · Substantial damageNTSB CEN23LA172Accident · Serious injuriesClass 3 · LimitedFinal reportPiper PA-34-200 · Coldspring, TXThe stabilator trim rod assembly separated from the stabilator link assembly due to a missing connecting bolt, which resulted in the pilot’s inability to maintain pitch control of the airplane.May 3, 2023 · N28HE · Substantial damageNTSB CEN23LA170Accident · No injuriesClass 3 · LimitedFinal reportLuscombe 8F · Palmer, TXThe installation of an unapproved rudder control cable, which resulted in a fatigue failure and subsequent loss of rudder control during cruise flight. Contributing to the accident was the mechanic’s inadequate inspection of the rudder control system.Apr 30, 2023 · N1113B · Substantial damageNTSB DCA22MA009Accident · Serious injuriesClass 2 · MajorFinal reportMcdonnell Douglas DC-9-87 (MD-87) · Brookshire, TXThe jammed condition of both elevators, which resulted from exposure to localized, dynamic high wind while the airplane was parked and prevented the airplane from rotating during the takeoff roll. Also causal was the failure of Everts Air Cargo, the pilots’…Oct 19, 2021 · N987AK · DestroyedNTSB CEN21LA346Accident · Serious injuriesClass 3 · LimitedFinal reportHpH, Spol. S.R.O. Glasflügel 304S · Briggs, TXThe overstress fracture of the elevator control tube due to reduced wall thickness from water intrusion and subsequent corrosion. Contributing to the accident was the lack of a drain hole at the bottom of the elevator control tube, which allowed the tube to…Jul 30, 2021 · N304AB · Substantial damageNTSB CEN20LA259Accident · Minor injuriesClass 3 · LimitedFinal reportSopwith Type 9400 · Van Alstyne, TXAn inflight loss of aileron control due to movement of a control connector.Jul 3, 2020 · N5539 · Substantial damageNTSB CEN19LA065Accident · Minor injuriesLimited investigationFinal reportRobinson R44 · Uvalde, TXThe slipping of the sprag clutch due to galling of the sprags and corresponding sprag contact surfaces within the clutch assembly, which rendered the helicopter uncontrollable.Jan 8, 2019 · N484AB · Substantial damageNTSB CEN18LA290Accident · Minor injuriesLimited investigationFinal reportBell 206 · Todd Mission, TXThe passenger’s inadvertent interference with the tail rotor pedals, which resulted in a loss of helicopter control during takeoff and the subsequent impact with terrain.Jul 20, 2018 · N352CT · Substantial damageNTSB CEN18LA195Accident · Minor injuriesClass 3 · LimitedFinal reportCirrus Design SR20 · Katy, TXThe loss of airplane control on takeoff due to the absence of the attachment bolt for the left aileron actuation arm.May 27, 2018 · N67Y · Substantial damageNTSB CEN18LA157Accident · Minor injuriesLimited investigationFinal reportHartline J Bon Hartline Kitfox III · Marathon, TXThe failure of the flaperon hinge attachment point during takeoff, which resulted in a loss of airplane control. Contributing to the accident was the lack of reinforcement of the hinge attachment point in accordance with the manufacturer’s service bulletin.May 2, 2018 · N73BH · Substantial damageNTSB CEN16CA359Accident · No injuriesData collectionFinal reportBeech 58 · Wichita Falls, TXThe incorrect maintenance of the airplane's ventilation system which resulted in an obstruction of the elevator control system.Aug 26, 2016 · N15MD · Substantial damageNTSB CEN16LA244Accident · No injuriesLimited investigationFinal reportPollack Quicksilver SPRINT2S · Bullard, TXA loss of airplane control during landing for reasons that could not be determined, because the airplane sank and was not recovered.Jul 3, 2016 · N250AB · Substantial damageNTSB GAA16LA182Accident · Serious injuriesLimited investigationFinal reportHughes 369 · Weatherford, TXThe pilot/mechanic's inadequate postmaintenance and preflight inspections, which resulted in his failure to remove the antitorque pedal lock and a subsequent loss of control during hover operations.Apr 8, 2016 · N298SD · Substantial damageNTSB CEN16IA103Incident · No injuriesIncident investigationFinal reportCessna 560 · Dallas, TXThe loss of aileron trim due to the lack of separation between the cannon head on the back of autopilot cannon plug and the aileron trim tab control gear. Contributing to the incident was the lack of guidance in the airplane maintenance manual to verify…Feb 9, 2016 · N774SB · No damageNTSB CEN15LA395Accident · No injuriesLimited investigationFinal reportBell Helicopter Textron Canada 429 · Port O'Connor, TXThe fatigue failure of the tail rotor pitch change link spherical bearing housing as a result of corrosion pitting.Aug 21, 2015 · N429AR · Substantial damageNTSB CEN15LA182Accident · Serious injuriesLimited investigationFinal reportAir Tractor AT 400 · Levelland, TXThe in-flight separation of the left aileron's attachment hardware at the connection between the long aileron pushrod and the left aileron bellcrank. Contributing to the accident was maintenance personnel’s improper installation of, or failure to install, the…Mar 26, 2015 · N136DB · Substantial damageNTSB CEN13LA518Accident · Minor injuriesLimited investigationFinal reportAmerican Champion 7GCB · Pearsall, TXThe failure of the rudder cable due to electrical arcing damage from contact with an unguarded battery and the pilot's subsequent loss of control during the go-around.Sep 2, 2013 · N9967Y · Substantial damageNTSB CEN13LA437Accident · Serious injuriesLimited investigationFinal reportEnstrom F-28A · Danbury, TXThe loss of collective control for reasons that could not be determined due to extensive fire damage.Jul 26, 2013 · N287Q · Substantial damageNTSB CEN12LA525Accident · No injuriesLimited investigationFinal reportBell 214ST · Avalon, TXMaintenance personnel’s failure to properly torque the retaining nut and install the cotter pin that secured the helicopter’s tail rotor counterweight bellcrank. Contributing to the accident was the lack of detailed maintenance records that documented…Aug 7, 2012 · N409SB · Substantial damageNTSB CEN12LA120Accident · Serious injuriesLimited investigationFinal reportContinental Copters 47G2 · Lohn, TXThe improper installation of the tail rotor gearbox by maintenance personnel, which led to accelerated wear of the ring and pinion gears, resulting in the loss of tail rotor effectiveness and subsequent forced landing.Jan 1, 2012 · N9021R · Substantial damageNTSB CEN11LA558Accident · No injuriesLimited investigationFinal reportPiper Aerostar 601P · Alpine, TXThe pilot’s improper flare which resulted in a hard landing. Contributing to the accident was the pilot’s improper decision to fly the airplane with a known mechanical deficiency.Aug 22, 2011 · N8076J · Substantial damageNTSB CEN11CA438Accident · No injuriesData collectionFinal reportCessna A188 · Castroville, TXThe pilot's failure to maintain obstacle clearance during the agricultural spraying flight.Jun 24, 2011 · N731ST · Substantial damageNTSB CEN11LA226Accident · No injuriesLimited investigationFinal reportRobinson Helicopter R22 Beta · Bulverde, TXThe in-flight separation of the fuel cap, which impacted the helicopter’s tail rotor and resulted in the loss of tail rotor thrust. Contributing to the accident was the inadequate preflight inspection by both pilots, who did not ensure that the fuel cap was…Mar 9, 2011 · N112HE · Substantial damageNTSB CEN10CA200Accident · No injuriesData collectionFinal reportQuicksilver Sport 2S · Canton, TXThe airplane builder’s improper installation of the left rear wing strut eyebolt.Apr 9, 2010 · N439MM · Substantial damageNTSB CEN10IA084Incident · No injuriesIncident investigationFinal reportATR ATR72 · Dallas, TXA fatigue failure of an elevator stop bracket, which resulted in a partial jam of the elevator control. Contributing to the failure was the improper installation of shim stacks, poor alignment of the brackets, and cyclic stresses acting on the lower stop,…Dec 26, 2009 · N494AE · Minor damageNTSB CEN09IA578Incident · No injuriesIncident investigationFinal reportCessna 421 · Sugar Land, TXThe improper installation of the pitch trim cable which resulted in it making improper contact with a guard pin that led to the fatigue failure of the cable.Sep 4, 2009 · N2349S · Minor damageNTSB CEN09IA032Incident · No injuriesIncident investigationFinal reportMD Helicopter MD 900 · Amherst, TXThe failure of the vertical stabilizer control adapter due to reverse bending fatigue.Oct 19, 2008 · N902NM · Minor damageNTSB CEN09IA003Incident · No injuriesIncident investigationFinal reportMD Helicopter MD 900 · Weatherford, TXThe failure of the vertical stabilizer control adapter due to reverse bending fatigue.Oct 8, 2008 · N902RN · Minor damage