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 ENG17RA040Incident · No injuriesForeign investigationATR ATR72 · Guarulhos, BrazilThe Centro de Investigação e Prevenção de Acidentes Aeronáuticos (CENIPA) of Brazil has notified the NTSB of an incident involving an Aerospatiale and Alenia ATR-72-212A, which occurred on March 21, 2017. The NTSB has appointed a U.S. Accredited…NTSB ERA17CA129Accident · Minor injuriesData collectionFinal reportKerns Kenneth H Kens Wingless Wonder · Mount Airy, NCThe pilot’s improper adjustment of the prerotator motor, which resulted in its failure to disengage and the subsequent loss of aircraft control during takeoff.NTSB DCA17FA076Accident · Minor injuriesClass 1 · FieldFinal reportMcdonnell Douglas MD80 · Ypsilanti, MIthe jammed condition of the airplane's right elevator, which resulted from exposure to localized, dynamic wind while the airplane was parked and rendered the airplane unable to rotate during takeoff. Contributing to the accident were (1) the effect of a large…NTSB GAA17CA178Accident · No injuriesData collectionFinal reportSchweizer 269C · Ormond beach, FLThe separation of the throttle cable’s outer housing from the inner housing at the throttle linkage while at a high-power setting, which prevented the pilot from being able to control the throttle and execute a proper landing flare and resulted in a hard…NTSB DCA17WA056Incident · No injuriesForeign investigationBoeing 737 · Paris, FranceThe Bureau d'Enquêtes et d'Analyses (BEA) of France has notified the NTSB of an incident involving a BOEING 737 airplane that occurred on December 30, 2016. The NTSB has appointed a U.S. Accredited Representative to assist the government of France's…NTSB WPR17WA039Accident · 1 fatalForeign investigationRobinson R44 · Juhu, IndiaNTSB CEN17FA012Accident · 2 fatalField investigationFinal reportFairchild Hiller FH 1100 · Lino Lakes, MNThe separation of the main rotor assembly due to mast bumping.NTSB WPR17LA002Accident · Minor injuriesLimited investigationFinal reportTamarack Helicopters UH-1H · Gila Bend, AZThe separation of the 90° tail rotor gearbox assembly as a result of fatigue to the tail rotor gearbox input quill assembly attachment studs due to the helicopter experiencing highly repetitive agricultural flight profiles for which it was not designed.NTSB WPR17CA001Accident · No injuriesData collectionFinal reportCessna R172K · Rosamond, CAThe pilot's improper use of the control lock, combined with his incomplete execution of two pre-departure procedures, which resulted in a takeoff with the control lock installed.NTSB DCA16WA229Incident · No injuriesForeign investigationPulse Vapor 55 · Ballina, AustraliaThe Australian Transport Safety Bureau (ATSB) has notified the NTSB of an incident involving a Pulse Vapor 55 unmanned helicopter that occurred on September 28, 2016. The NTSB has appointed a U.S. Accredited Representative to assist the ATSB's investigation…NTSB ERA16LA322Accident · No injuriesLimited investigationFinal reportAero Vodochody L 39 · Norfolk, VAAn uncommanded flap retraction for reasons that could not be determined, as a postaccident examination of the flap system did not reveal evidence of any preaccident anomalies.NTSB GAA16CA476Accident · No injuriesData collectionFinal reportLuscombe 8 · Juneau, WIThe pilot's failure to maintain directional control during the landing roll in gusting crosswind conditions, which resulted in a runway excursion. Contributing to the accident was the foot pad cover slipping off the right rudder pedal during the landing roll.NTSB 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.NTSB ERA16LA293Accident · No injuriesClass 3 · LimitedFinal reportCessna 150G · Shirley, NYMaintenance personnel’s inadequate maintenance and inspection of the airplane, which resulted in the left elevator attachment bolt backing out of the nutplate, and partial inflight separation and damage of the elevator.NTSB ERA16FA248Accident · 1 fatalField investigationFinal reportBell Helicopter Textron Canada 407 · Hickory, KYCompany maintenance personnel's inappropriate removal without replacement of the safety wires on the collective lever pin screws during a recent maintenance inspection, which resulted in the screws backing out and led to a loss of collective control in flight.NTSB 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.NTSB ANC16LA034Accident · No injuriesLimited investigationFinal reportDe Havilland DHC3 · Homer, AKAn in-flight collision with a bald eagle, which resulted in substantial damage to the left wing.NTSB CEN16LA230Accident · No injuriesLimited investigationFinal reportGlaeser Nieuport 11 · Gardner, KSThe pilot's diverted attention during the approach for the precautionary landing, which resulted in low airspeed, an exceedance of the airplane’s critical angle of attack, and a subsequent aerodynamic stall. Contributing to the accident was the control system…NTSB WPR16LA099Accident · Minor injuriesClass 3 · LimitedFinal reportBell 47G 5 · San Ardo, CAThe failure of the pin in the outboard end of the lateral flight control torque tube.NTSB 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.NTSB DCA16WA104Incident · No injuriesForeign investigationBoeing 747 · Jeddah, Saudi ArabiaThe government of Saudi Arabia has notified the NTSB of an accident involving a BOEING 747 airplane that occurred on March 09, 2016. The NTSB has appointed a U.S. Accredited Representative to assist the government of Saudi Arabia's investigation under the…NTSB CEN16WA110Accident · No injuriesForeign investigationPiper PA23 · Saint François, GuadeloupeOn February 22, 2016, a Piper PA-23-250 airplane, N539EG, sank after ditching near the Saint François Airport (TFFC), Saint François, Guadeloupe (France). The pilot was not injured.This investigation is under the jurisdiction and control of the French…NTSB ANC16WA070Accident · No injuriesForeign investigationPiper PA-28-140 · St Andrews, CanadaOn February 13, 2016, about 2039 Coordinated Universal Time (UTC), a Piper PA-28-140 airplane, (Canadian Registration C-GQPN) was on approach to St. Andrews, MB (CYAV) with an instructor and a student on board. Prior to touch down at approximately 50 feet…NTSB 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…NTSB ERA16LA030Accident · No injuriesLimited investigationFinal reportHughes 369D · Marion, SCA momentary jam in the tail rotor control system from an undetermined source, resulting in a torsional fracture of the tail rotor control torque tube and a loss of helicopter control.NTSB ERA16LA015Accident · No injuriesLimited investigationFinal reportBell 206L 3 · Dickinson, ALThe improper installation by company maintenance personnel of the securing hardware of a tail rotor driveshaft section, which resulted in that section of tail rotor driveshaft disconnecting and a complete loss of tail rotor thrust.NTSB CEN15WA449Accident · 1 fatalForeign investigationTrendak Tercel · Odorheiul Secuiesc City, RomaniaThis is preliminary information, subject to change, and may contain errors. On September 26, 2015, at an unknown time, a Trendak Tercel gyroplane, A11-DUN, impacted terrain after takeoff from an airfield near Odorheiul Secuiesc city, Harghita County, Romania.…NTSB GAA15CA294Accident · No injuriesData collectionFinal reportHoward DGA 15P · Englewood, COThe separation of the elevator control system linkage at a push/pull tube and cable joint, for an unknown reason, because the bolt and associated hardware securing the joint was not found for examination.NTSB CEN15FA425Accident · 1 fatalField investigationFinal reportCessna T310Q · Wichita, KSThe separation of the attachment hardware connecting the elevator trim tab pushrod to the elevator trim actuator, which resulted in the elevator trim tab jamming in a position outside the limits of normal travel and a subsequent loss of airplane control.NTSB ERA15LA374Accident · No injuriesLimited investigationFinal reportBell 206 · Thomaston, GAThe loss of tail rotor control due to a fractured pin in the tail rotor control system; the reason the pin fractured could not be determined as the fractured pin was lost in shipping.NTSB ERA15LA360Accident · No injuriesLimited investigationFinal reportJ. Schilling S-19 · East Falmouth, MAThe experimental airplane builder's failure to properly secure the stabilator trim tab push-pull tube’s connection, which resulted in the tube’s separation and a subsequent hard landing. Contributing to the accident was the pilot/owner's failure to detect the…NTSB ERA15LA358Accident · Serious injuriesLimited investigationFinal reportBellanca 7KCAB · Manteo, NCThe inadvertent lodging of the banner-tow cable between the right elevator and horizontal stabilizer after the pilot threw the grapple hook out the window, which resulted in the loss of pitch control and the airplane’s subsequent impact with water.NTSB CEN15LA412Accident · Minor injuriesLimited investigationFinal reportGuisinger Gary G Baby Belle · Stuart, IAThe failure of the tail rotor driveshaft for reasons that could not be determined due to the mechanically and thermally deformed fracture surface.NTSB WPR15LA249Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C - Undesignat · Mesa, AZThe disbondment of a main rotor damper, which resulted in the degradation of its damping action and led to excessive main rotor vibrations and oscillations that caused substantial damage to the helicopter in flight and led to a hard landing.NTSB 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.NTSB CEN15LA367Accident · 1 fatalLimited investigationFinal reportAir Tractor AT-802A · Wiville, ARThe pilot's failure to maintain clearance from a utility pole while maneuvering during an agricultural application flight, which resulted in damage to the right aileron and a subsequent uncontrolled right roll at a low altitude.NTSB ERA15LA319Accident · Serious injuriesLimited investigationFinal reportHead AX9 118 · New Holland, PAThe pilot's failure to adequately secure the vent line, which resulted in the premature deflation of the balloon’s envelope and its subsequent contact with power lines. Contributing to the accident were the pilot's choice of an unsuitable landing area, which…NTSB WPR15LA203Accident · No injuriesLimited investigationFinal reportBeech C 99 · Salt Lake City, UTThe airplane’s unmanageable right yaw during takeoff for reasons that could not be determined because postaccident examination of the rudder and rudder assembly did not reveal any anomalies that would have precluded normal operation.NTSB CEN15LA265Accident · No injuriesLimited investigationFinal reportBell 407 · Pecan Island, LAThe fatigue fracture of the tail rotor gearbox attachment studs, which resulted in a loss of tail rotor control and a subsequent hard landing.NTSB ANC15LA037Accident · No injuriesLimited investigationFinal reportDehavilland DHC-3T · Skwentna, AKThe flutter failure of the right elevator servo tab due to the improper fabrication of the servo tab and maintenance personnel’s subsequent failure to detect anomalies with the servo tab.NTSB CEN15IA200Incident · No injuriesIncident investigationFinal reportAir Tractor AT 402A · Brickeys, ARThe in-flight separation of the attachment hardware at the elevator control pushrod due to maintenance personnel's improper reinstallation of the attachment hardware.NTSB 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…NTSB ENG15WA021Incident · No injuriesForeign investigationBoeing 737 - 683 · Oslo, NorwayOn March 25, 2015, at approximately 0730 Coordinated Universal Time (UTC), a Boeing 737-683, Norwegian registration LN-RPA, operated by Scandinavian Airlines System (SAS), experienced a pitch control problem while landing on Runway 01R at Oslo Airport,…NTSB ANC15LA015Accident · No injuriesLimited investigationFinal reportAirbus AS350 B2 · Anchorage, AKThe failure of the ball bearing within the pitch change spider assembly due to its operation with no grease within the bearing, which resulted in the subsequent fracture of the spider assembly and a loss of tail rotor control authority. Also causal to the…NTSB WPR15LA126Accident · No injuriesLimited investigationFinal reportPiper PA 18-150 · Merced, CAThe separation of the flight control stick from the stub due to its improper installation.NTSB CEN15CA166Accident · No injuriesData collectionFinal reportFunk B85C · Leonard, OKThe improper installation of the UP elevator cable turnbuckle which became disconnected during the flight.NTSB CEN15CA159Accident · No injuriesData collectionFinal reportArnold Zodiac CH 650 · Greeley, COThe pilot was unable to maintain directional control during the landing due to the foreign object that lodged behind the rudder.NTSB CEN15LA156Accident · No injuriesLimited investigationFinal reportAgusta Aerospace AW119 Mkii · Gulf of MexicoThe fracture of the tail rotor pitch change link due to excessive bearing rotational friction, which resulted from the bearings being installed in exceedance of the maximum allowable torque during the last overhaul of the pitch change link.NTSB ANC15IA006Incident · No injuriesIncident investigationFinal reportCessna 180J · Nome, AKThe disengagement and subsequent binding of the right tailwheel steering cable, which disabled the rudder system.NTSB CEN15IA085Incident · No injuriesIncident investigationFinal reportDassault/Sud FAN JET Falcon · Shreveport, LAA short in the trim system’s wires and connector, which resulted in the elevator trim being in a full nose-down position.