NTSB investigations
410 cases where the sequence of events included Flight control sys malf/fail.
Cases, newest first
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.\"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.
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."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
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 ERA20LA051Accident · Serious injuriesClass 3 · LimitedFinal reportParsons Two Place #1 · Naguabo, PRA failure of the rudder attachment bolt, which resulted in the rudder’s subsequent inflight separation from the fuselage.NTSB DCA20IA014Incident · No injuriesClass 3 · IncidentFinal reportEmbraer ERJ170 · Atlanta, GAThe captain’s use of his pitch trim switch, which had been placarded inoperative but not deactivated, resulting in the airplane pitching up when the captain was trying to trim down. The trim commands were reversed due to maintenance personnel’s incorrect…NTSB WPR20LA004Accident · Minor injuriesClass 3 · LimitedFinal reportGlaser Dirks DG500 · Marana, AZThe pilots’ exceedance of the glider’s never-exceed speed (VNE) during recovery from an intentional aerobatic maneuver, which resulted in a failure of the right-wing air brake control drive, asymmetrical air brake deployment, and a subsequent hard landing.NTSB WPR20LA001Accident · 1 fatalClass 3 · LimitedFinal reportBuckeye Breeze · Moore, UTThe pilot’s improper preflight inspection and detection of a pinch point in the steering line, which resulted in a loss of control in flight and impact with terrain.NTSB DCA19WA212Incident · No injuriesForeign investigationBoeing 737 · South AfricaThe government of South Africa has notified the NTSB of an incident involving a BOEING 737 airplane that occurred on September 02, 2019. The NTSB has appointed a U.S. Accredited Representative to assist the government of South Africa's investigation under the…NTSB CEN19LA224Accident · No injuriesClass 3 · LimitedFinal reportPiper PA18 · Osceola, WIThe failure of the right horizontal stabilizer during takeoff, resulting in a loss of control and forced landing. Contributing to the accident was the installation of an unapproved stabilizer frame and failure of maintenance personnel to identify…NTSB ERA19FA225Accident · 1 fatalClass 3 · FieldFinal reportQuicksilver Mxii · Oliver Springs, TNThe noncertificated pilot’s decision to continue to takeoff and climb after encountering an undetermined airplane control issue that he was unable to counteract, which resulted in collision with trees and subsequent impact with terrain.NTSB CEN19LA219Accident · No injuriesClass 3 · LimitedFinal reportFisher Flying Products Super Koala · Hazen, NDThe airplane owner's and mechanic's improper rigging and cable tension of the aileron control system, which resulted in a loss of control during takeoff.NTSB CEN19LA174Accident · No injuriesClass 3 · LimitedFinal reportRobinson R44 · Key West, FLThe failure of maintenance personnel to properly secure the right-side tail boom mounting bolts which resulted in the failure of the bolts and an inflight separation of the tail rotor.NTSB DCA19LA154Accident · No injuriesLimited investigationFinal reportAurora PAV · Manassas, VAa loss of hover lift thrust provided by the eight lift motors due to a false on-ground rotor speed reduction command, resulting from excessive vibration.NTSB WPR19LA112Accident · Serious injuriesClass 3 · LimitedFinal reportAir Tractor AT502 · Morganza, LAA loss of aircraft control due to the separation of the elevator pushrod attachment bolt.NTSB WPR19LA114Accident · No injuriesClass 3 · LimitedFinal reportGreat Lakes 2T-1A-2 · San Diego, CAThe fracture of the aileron hinge strap due to fatigue crack propagation, which resulted in substantial damage to a wing rib aft of the spar at the outboard aileron cutout. Contributing to the accident was inadequate maintenance inspection.NTSB 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.NTSB DCA19WA023Incident · No injuriesForeign investigationEmbraer 190 · Bara, PortugalThe GPIA of Portugal has notified the NTSB of an incident involving a Embraer 190 airplane that occurred on November 11, 2018. The NTSB has appointed a U.S. Accredited Representative to assist the GPIA of Portugal's investigation under the provisions of ICAO…NTSB CEN19WA042Accident · No injuriesForeign investigationPiper PA34 · Uk, United KingdomThe government of United Kingdom has notified the NTSB of an accident involving a PIPER PA34 airplane that occurred on November 02, 2018. The NTSB has appointed a U.S. Accredited Representative to assist the government of United Kingdom's investigation under…NTSB ERA19FA034Accident · 2 fatalField investigationFinal reportAutogyro Cavalon · Sebring, FLThe pilot's improper decision to operate the gyroplane in an unairworthy condition, which resulted in the cyclic pitch control disconnecting in flight. Contributing was the pilot's inability to maintain control of the helicopter utilizing the published…NTSB ERA18LA258Accident · Minor injuriesClass 3 · LimitedFinal reportBeech 35 · Georgetown, SCA loss of directional control during landing due to overstress failure of the left seat’s left rudder pedal arm clevis, which occurred as a result of manufacturing defects.NTSB WPR18LA242Accident · Serious injuriesClass 3 · LimitedFinal reportBell 212 · Dardanelle, CAAn in-flight failure of the trunnion bearing and subsequent failure of the drive link and swashplate support, which resulted in the loss of helicopter control.NTSB WPR18LA221Accident · No injuriesClass 2 · LimitedFinal reportHughes 369 · Honolulu, HIThe operator's improper installation of the tail rotor (TR) teeter bearings, which resulted in cascading in-flight failures of the TR components and attach hardware.NTSB 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.NTSB CEN18LA246Accident · No injuriesLimited investigationFinal reportCessna 337 · Baldwin City, KSThe loss of hydraulic accumulator pressure for reasons that could not be determined, which prevented the propeller from unfeathering, and the pilot's improper decision to attempt a go-around, which resulted in an off-airport landing and the airplane impacting…NTSB ERA18FA180Accident · 1 fatalField investigationFinal reportCessna 150J · Manteo, NCA loss of control due to the banner tow rope becoming entangled with the left horizontal stabilizer in crosswind conditions.NTSB 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.NTSB ERA18LA140Accident · Minor injuriesLimited investigationFinal reportRobinson R22 · Panama City, FLThe pilot's failure to properly remove and secure the tie-down ropes during the preflight inspection, which resulted in the ropes becoming entangled in the rotor head swashplate and pitch control rods during flight and the subsequent loss of pitch control.NTSB 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.NTSB CEN18WA399Accident · Minor injuriesForeign investigationCessna 172 · Hamilton, BermudaOn April 30, 2018, about 2045 universal coordinated time (UTC), a Cessna 172 M airplane, N9085H, was substantially damaged during a landing at the L. F. Wade International Airport, near Hamilton, Bermuda. The pilot sustained minor injuries.The accident…NTSB DCA18WA315Accident · No injuriesForeign investigationAirbus A320 · Tallinn, EstoniaThe Estonian Safety Investigation Bureau (AIB) has notified the NTSB of an accident involving a Airbus 320, which occurred on February 28, 2018. The NTSB has appointed a U.S. Accredited Representative to assist the AAIB investigation under the provisions of…NTSB CEN18LA099Accident · No injuriesLimited investigationFinal reportBeech 35 · Batesville, ARAn in-flight control system flutter encounter during a turbulence encounter; the reason for the flutter could not be determined.NTSB ANC18LA020Accident · No injuriesLimited investigationFinal reportEurocopter France SA330J Puma · Pacific Ocean, JapanThe worn rear bearing of the freewheel unit. Contributing to the accident was the delay in analyzing an oil sample, which would have detected the increase in metal contaminants from the worn bearing.NTSB WPR18LA047Accident · No injuriesClass 3 · LimitedFinal reportCessna 172D · Auburn, WAThe pilot's loss of airplane control for reasons that could not be determined based on the available information.NTSB CEN18LA044Accident · No injuriesLimited investigationFinal reportCessna 170B · Harvard, ILThe failure of the universal joint in the pilot-side flight control yoke due to the fatigue fracture of a rivet within the universal joint. Contributing to the universal joint failure was the universal joint design, which was prone to galling wear and seizure.NTSB ENG18IA003Incident · No injuriesClass 3 · IncidentFinal reportAirbus A330-243 · Seattle, WAThe loss of control of the left-hand engine and the subsequent thermal damage to the left wing on landing during engine reverse operation was due to a blockage of the variable stator vane torque motor filter that resulted in the engine’s electronic engine…NTSB GAA18CA020Accident · No injuriesData collectionFinal reportCessna 150 · Pottsville, PAThe failure of the right rudder cable and subsequent loss of directional control during landing.NTSB WPR18LA004Accident · No injuriesClass 3 · LimitedFinal reportWestern International Avia UH 1H · Arbuckle, CAA collective control malfunction for reasons that could not be determined.NTSB ERA17LA329Accident · Minor injuriesLimited investigationFinal reportCessna 402 · Nantucket, MAThe separation of the pushrod from the elevator trim tab actuator, which rendered controlled flight impossible. Contributing to the separation of the pushrod was the failure of maintenance personnel to properly secure it to the elevator trim tab actuator.NTSB DCA17WA199Incident · No injuriesForeign investigationBoeing 737 · Caracas, VenezuelaThe DGAC of Venezuela has notified the NTSB of an incident involving a Boeing 737 airplane that occurred on September 13, 2017. The NTSB has appointed a U.S. Accredited Representative to assist the DGAC's investigation under the provisions of ICAO Annex 13 as…NTSB CEN17LA375Accident · No injuriesLimited investigationFinal reportHiller UH 12A · Griffith, INThe loss of tail rotor thrust due to a failed tail rotor driveshaft, which resulted in a loss of tail rotor control and a hard landing.NTSB CEN17LA344Accident · No injuriesLimited investigationFinal reportAviat A 1B · Prairie du Chien, WIThe fatigue failure of the aileron hinge bracket tubing for reasons that could not be determined based on the available evidence.NTSB WPR17LA201Accident · No injuriesLimited investigationFinal reportCobalt Aircraft Industries Co50 Valkyrie · Atwater, CAA loss of aileron effectiveness due to the airplane's design configuration, which resulted in the pilot's inability to control the roll axis and led to a hard landing.NTSB ERA17LA292Accident · Minor injuriesClass 3 · LimitedFinal reportHostein K/Hostein S Pietenpol · Albion, NYLoss of directional control due to a restriction of rudder movement.NTSB WPR17LA186Accident · Minor injuriesLimited investigationFinal reportHawker Siddeley Hunter MK.58 · Pacific Ocean (Pacific Ocean)The pilot’s loss of airplane control after flying through another airplane's jet wash during an air defense exercise.NTSB WPR17LA180Accident · No injuriesLimited investigationFinal reportLockheed P2V 5F · Pocatello, IDMaintenance personnel's failure to secure hardware, which resulted in an uncommanded upward deflection of the left elevator and aft movement of the control yoke and inhibited the flight crew from adjusting the airplane's pitch attitude in flight. Contributing…NTSB ERA17LA263Accident · Minor injuriesLimited investigationFinal reportSikorsky S-97A · Jupiter, FLA design change in the helicopter's fly-by-wire control system that resulted in an increase in the sensitivity of the cyclic stick while transitioning from ground to flight mode, magnifying the pilot's control inputs, which resulted in unintentional over…NTSB WPR17FA161Accident · 1 fatalField investigationFinal reportApplegate Panzl S331E · Apple Valley, CAA fatigue failure of the left aileron control rod end during aerobatic flight, which resulted in the pilot's inability to maintain control of the airplane.NTSB ERA17WA230Accident · 9 fatalForeign investigationGulfstream G1159A · Nueva Esparta, VenezuelaOn July 4, 2017, about 1745 coordinated universal time (UTC), a Gulfstream 1159A, Venezuela registration YV2895, descended into the Caribbean Sea northwest of Nueva Esparta, Venezuela, and was presumed to be destroyed. Visual meteorological conditions…NTSB CEN17LA224Accident · No injuriesLimited investigationFinal reportMckenna SD-1A · Juneau, WIThe pilot’s difficulty controlling the airplane due to his incorrect reinstallation of the wings, which led to a bounced precautionary landing. Contributing to the accident was the failure of the pilot and the mechanic to verify the wings’ angle of incidence.NTSB CEN17LA216Accident · No injuriesLimited investigationFinal reportWilliam D Telfair/Zia Z Telfai Excalibur · Albuquerque, NMThe loss of pitch control due to the overload failure of the control rod.NTSB WPR17LA102Accident · Minor injuriesLimited investigationFinal reportPiper PA 18A · Coeur D'Alene, IDThe loss of yaw control due to an inadequately compressed rudder swage, which resulted from inadequate maintenance and led to the separation of the forward right rudder cable.NTSB WPR17LA087Accident · Serious injuriesLimited investigationFinal reportTitan Tornado I · Spanaway, WAMaintenance personnel’s improper attachment of the aileron system components, which resulted in the pilot's inability to maintain flight control.NTSB ERA17FA148Accident · 1 fatalField investigationFinal reportPiper PA 12 · Sanford, FLThe incorrect rigging of the elevator control cables, which resulted in a reversal of elevator control inputs applied by the pilot during the takeoff, an excessive nose-high pitch, and subsequent aerodynamic stall after takeoff. Also causal was the inadequate…