NTSB investigations, TX
29 cases where the sequence of events included Aircraft structural failure.
Cases per year
| 2008 | 1 |
|---|---|
| 2009 | 5 |
| 2010 | 1 |
| 2011 | 3 |
| 2012 | 4 |
| 2013 | 3 |
| 2014 | 2 |
| 2015 | 2 |
| 2016 | 1 |
| 2018 | 1 |
| 2019 | 2 |
| 2023 | 2 |
| 2024 | 2 |
Where
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\" = '337' 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.
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" = '337' 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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
NTSB DCA25LA025Accident · No injuriesClass 4 · LimitedFinal reportBoeing 737-9 · Houston, TXBrake application before all three landing gears were on the ground, which caused the failure of the right main landing gear tires and resulted in tire fragments impacting the fuselage.NTSB CEN24LA162Accident · No injuriesClass 3 · LimitedFinal reportAmerican Champion 7ECA · Longview, TXThe rudder post’s failure due to corrosion fatigue. Contributing to the accident were the misalignment of the rudder hinge components, which produced mechanical binding and elevated localized stress, and a compromised the protective coating, which allowed…NTSB CEN23LA405Accident · No injuriesClass 3 · LimitedFinal reportAlisport Silent 2 Electro · Giddings, TXThe glider’s encounter with flutter during cruise flight that resulted in structural damage to the fuselage.NTSB CEN23LA319Accident · No injuriesClass 3 · LimitedFinal reportAlisport Silent 2 Electro · Wallis, TXThe failure of the tail boom structure due to cyclic torsion overloading as of a result of flutter in the empennage. The reason for the flutter could not be determined.NTSB CEN20CA033Accident · No injuriesData collectionFinal reportPiper PA18 · Kerrville, TXThe pilot’s loss of airplane control during the landing flare, which resulted in a loss of directional control and ground-loop.NTSB CEN19FA094Accident · 4 fatalField investigationFinal reportCessna T337 · Longview, TXThe noninstrument-rated pilot's improper decision to continue flight into convective weather conditions, which resulted in the airplane exceeding its maximum maneuvering speed and the subsequent in-flight breakup. Contributing to the accident was the pilot's…NTSB CEN19FA004Accident · 2 fatalField investigationFinal reportPiper PA32RT · Poolville, TXThe pilot's loss of airplane control as a result of spatial disorientation and the exceedance of the structural capabilities of the airplane. Contributing to the accident was the pilot's limited experience in instrument conditions.NTSB DCA16FA199Accident · 2 fatalClass 2 · FieldFinal reportBell 525 · Italy, TXA severe vibration of the helicopter that led to the crew's inability to maintain sufficient rotor rotation speed (Nr), leading to excessive main rotor blade flapping, subsequent main rotor blade contact with the tail boom, and the resultant in-flight…NTSB CEN16LA027Accident · No injuriesLimited investigationFinal reportBell 407 · San Antonio, TXThe failure of the No. 3 tail rotor adapter and shaft due to a loss of torque on the retaining nut. Contributing to the accident was the lack of a requirement to inspect the tail rotor assembly for security in the helicopter manufacturer's maintenance manual…NTSB CEN15LA104Accident · 1 fatalLimited investigationFinal reportBaker Bobby J Safari · The Woodlands, TXAn in-flight separation of the helicopter’s horizontal stabilizer due to undetected fatigue cracking of the stabilizer spar, which resulted in a loss of control.NTSB CEN14LA351Accident · No injuriesLimited investigationFinal reportCessna 152 · Denton, TXThe in-flight failure of the right wing’s rear spar.NTSB CEN14FA140Accident · 1 fatalField investigationFinal reportHillam Scott L Rans S 10 · Shepherd, TXThe noncertificated pilot’s improper decision to attempt aerobatic maneuvers that exceeded the airplane’s design limitations, which resulted in the subsequent in-flight breakup of the airplane. Contributing to the accident was the pilot’s lack of aerobatic…NTSB CEN14LA056Accident · 1 fatalLimited investigationFinal reportPearson Jon M Dragonfly · Anahuac, TXThe incorrect installation by the pilot, who was not a certificated mechanic or repairman, of the main rotor head bearing block, which resulted in the in-flight separation of the rotor head.NTSB CEN13FA213Accident · 2 fatalField investigationFinal reportSchleicher Alexander · Littlefield, TXThe pilot’s improper decision to conduct aerobatic maneuvers in a glider not approved for such maneuvers. Contributing to the accident was the degradation of the adhesive holding the wing together, which should have been detected either during the last annual…NTSB CEN13LA186Accident · 1 fatalLimited investigationFinal reportFisher Michael E Celebrity · Terrell, TXThe pilot’s exceedance of the airplane’s design stress limits while performing aerobatic maneuvers.NTSB CEN13FA105Accident · 2 fatalField investigationFinal reportBeech E-90 · Amarillo, TXThe pilot’s loss of control of the airplane after encountering icing conditions and heavy to extreme turbulence and the subsequent exceedance of the airplane’s design limit, which led to an in-flight breakup.NTSB CEN12FA628Accident · 1 fatalField investigationFinal reportPiper PA-23-250 · Bullard, TXThe pilot's maneuver, which exceeded the airplane's structural limit and resulted in an in-flight breakup.NTSB DCA12IA113Incident · No injuriesIncident investigationFinal reportBoeing 737-3H4 · El Paso, TXthe rupture of the nose landing gear hydraulic line that resulted from abrasions due to contact with the nose landing gear tire. Contributing to the incident was the incorrect installation of union and restrictor on the actuator.NTSB CEN12FA164Accident · 2 fatalField investigationFinal reportPiper PA-24-250 · Albany, TXThe loss of flight instrumentation due to a failed vacuum pump while flying a night without a discernable horizon, which resulted in the pilot's spatial disorientation and an in-flight loss of control and impact with terrain. Contributing was the continued…NTSB CEN12FA108Accident · 5 fatalField investigationFinal reportPiper PA-32-260 · Bryan, TXThe pilot’s inadvertent encounter with severe weather, which resulted in the airplane’s left wing failing in positive overload. Contributing to the accident was the pilot’s reliance on outdated weather information that he received on his in-cockpit…NTSB CEN11FA422Accident · 1 fatalField investigationFinal reportRobinson R22 Beta · Del Valle, TXThe divergence of the main rotor from its normal plane of rotation for reasons that cannot be determined because the pilot’s control inputs leading up to the event are unknown, resulting in mast bumping and main rotor blade separation.NTSB CEN11LA209Accident · No injuriesLimited investigationFinal reportGreat Lakes 2T-1A-2 · Kingsville, TXA pre-existing crack in the front spar of the right horizontal stabilizer near a riveted fitting, causing it to fail and separate from the airplane in flight. Contributing to the accident was the failure of maintenance personnel comply with existing service…NTSB CEN10FA291Accident · 2 fatalField investigationFinal reportBell 222 · Midlothian, TXThe fracture of a swashplate drive pin as a result of hydrogen embrittlement due to an unknown source, which resulted in an in-flight breakup of the main rotor system during cruise flight.NTSB CEN10FA044Accident · 3 fatalField investigationFinal reportBeech A36 · Spring Branch, TXThe pilot's failure to maintain control of the airplane during cruise flight in instrument meteorological conditions. Contributing to this accident was the pilot’s lack of recent experience in flying in instrument meteorological conditions.NTSB CEN09LA611Accident · 1 fatalLimited investigationFinal reportMckenna James E AVID-CATAL · Inks Lake, TXThe pilot’s decision to take off with a known airframe deficiency.NTSB CEN09CA521Accident · No injuriesData collectionFinal reportMaule M-4-220C · Abernathy, TXThe failure of the fuselage's tube structure due to corrosion during a hard landing.NTSB CEN09LA379Accident · No injuriesLimited investigationFinal reportUrban Air Sro UFM-13 · Bourne Stage, TXThe pilot’s exceedance of the aircraft’s placarded never-exceed speed (Vne), resulting in aerodynamic flutter in the empennage and the subsequent in-flight structural failure of the aft portion of the fuselage.NTSB CEN09CA268Accident · No injuriesData collectionFinal reportLuscombe 8 · Terrell, TXThe failure of the landing gear due to undetected corrosion.NTSB CEN09FA087Accident · 1 fatalField investigationFinal reportBeech C90 · Rocksprings, TXThe pilot's failure to properly configure the pressurization controls, resulting in his impairment and subsequent incapacitation due to hypoxia.