NTSB investigations
358 cases where the defining event was 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 e.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e.\"isDefiningEvent\" AND e.\"tier2Number\" = '333') 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 e.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e."isDefiningEvent" AND e."tier2Number" = '333') 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 ERA13LA229Accident · Serious injuriesLimited investigationFinal reportSchweizer SGS 2-33A · Erwinna, PAThe pilot’s loss of glider control due to improper rigging of the rudder control cables, the mechanic’s inadequate flight control checks following the glider’s most recent annual inspection, and the pilot’s failure to perform a thorough preflight inspection.NTSB WPR13LA189Accident · No injuriesLimited investigationFinal reportBeech 95-C55 · Santa Monica, CAThe left main wheel locking up during the landing roll, which resulted in the deflation of the tire, the left main landing gear collapse, and the subsequent loss of control during the runway exit.NTSB CEN13LA225Accident · Minor injuriesLimited investigationFinal reportAtkins ACRO-SPORT I · Midland, LAThe failure of the left elevator torque tube due to poor quality welds by the manufacturer, which resulted in the loss of pitch control.NTSB CEN13LA168Accident · Minor injuriesLimited investigationFinal reportAir Tractor AT-502 · Forrest City, ARThe in-flight separation of the left aileron's push-pull rod and hardware. Contributing to the accident was the failure of maintenance personnel to apply proper torque to the self-locking nuts.NTSB ERA13LA116Accident · Minor injuriesLimited investigationFinal reportRobinson Helicopter R22 Beta · Ellington, CTThe separation of the collective push-pull tube and jackshaft assembly, which resulted in the total loss of helicopter control and collision with terrain. Contributing to the accident was the inadequate supervision of maintenance personnel by the operator…NTSB ERA13IA114Incident · No injuriesIncident investigationFinal reportCessna 560XL · Debary, FLAn accumulation of debris in the airplane’s bilge drain holes that prevented accumulated moisture from properly draining; the accumulated moisture subsequently froze around the elevator control components, which resulted in the flight control stiffness.…NTSB WPR13LA087Accident · Serious injuriesLimited investigationFinal reportBell OH-58C · Riverdale, CAA flight control malfunction while maneuvering for reasons that could not be determined because it was not possible to establish whether observed damage to the flight control assembly was the result of wreckage recovery efforts or a preexisting condition.NTSB WPR13LA093Accident · No injuriesLimited investigationFinal reportKaufmann Vans RV-10 · Las Vegas, NVA missing elevator control assembly attachment bolt, which rendered the elevator control system ineffective and resulted in a loss of pitch control, and the pilot’s incorrect installation of the elevator control assembly.NTSB WPR13LA063Accident · No injuriesLimited investigationFinal reportAerotek Pitts S-1T · Billings, MTThe pilot’s inability to maintain directional control during the landing roll because of the failure of the tailwheel support bracket.NTSB ERA13LA052Accident · No injuriesLimited investigationFinal reportWaller Charles R Rans S12-XL · Gordon, ALA fatigue failure of the elevator pitch trim cable, which resulted in aerodynamic flutter of the elevator in flight and the airplane’s subsequent nose-over during the resultant precautionary landing.NTSB CEN13FA038Accident · No injuriesField investigationFinal reportPiaggio P180 · Boyne City, MIThe select/bypass valve's failure to seal correctly because of improper shimming, which resulted in an uncommanded and uncontrollable left turn during landing. Contributing to the accident was the overhaul facility's improper overhaul of the steering manifold.NTSB ENG13WA001Incident · No injuriesForeign investigationBeech 1900 · Lyon, FranceOn October 09, 2012, at 9:40 am local time, a Beechcraft 1900, F-GOPE, operated by Hex'Air, experienced a elevator trim system failure after take-off at Lyon-Saint Exupery airport(LFLL), France. A post flight inspection revealed that the elevator trim forward…NTSB WPR12FA421Accident · No injuriesField investigationFinal reportFrederick F 1 · Reno, NVThe pilot’s operation of the airplane above the established never-exceed speed and the incorrect installation of the trim tab control horn, which resulted in the flutter of the left elevator trim tab.NTSB WPR12LA407Accident · 1 fatalLimited investigationFinal reportMoore Edward R MXS · Borrego Springs, CAThe pilot’s inability to maintain control of the airplane following the loss of aileron and elevator control due to the forward flight control torque tube assembly’s detachment from the forward bearing. Contributing to the accident was the inadequate…NTSB WPR12TA364Accident · No injuriesFinal reportAmerican Eurocopter AS350B3 · Sunburst, MTThe improper installation of the engine-to-main gearbox flex coupling, which resulted in the failure of the flex coupling and a loss of power to the rotor system during takeoff.NTSB CEN12IA554Incident · No injuriesIncident investigationFinal reportCessna 560XL · Des Moines, IAA temporary loss of control during cruise flight for reasons that could not be determined because postincident examination of the autopilot, pitch trim systems, and horizontal stabilizer revealed no anomalies consistent with a loss of control.NTSB ERA12LA505Accident · No injuriesLimited investigationFinal reportPiper PA-22-160 · Bay Minette, ALThe separation of the tailwheel linkage for reasons that could not be determined because the linkage was not located, which resulted in a loss of directional control during landing.NTSB 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…NTSB WPR12LA341Accident · No injuriesLimited investigationFinal reportFairchild Hiller FH-1100 · Cody, WYThe failure of a tail rotor driveshaft coupling due to fatigue.NTSB WPR12FA332Accident · No injuriesField investigationFinal reportPiaggio P180 · Henderson, NVThe failure of maintenance personnel to properly torque the elevator attachment hardware in accordance with the maintenance manual, which led to the detachment of the elevator. Contributing to the accident were maintenance personnel's failure to identify the…NTSB WPR12CA293Accident · No injuriesData collectionFinal reportPiper PA-12 · Stevensville, MTThe separation of the left rudder control cable from the rudder bellcrank, which resulted in a loss of directional control during landing roll.NTSB ERA12FA395Accident · 1 fatalField investigationFinal reportRemos Acft Gmbh Flugzeugbau Remos GX · Westminster, MDThe pilot's inadequate preflight inspection, which failed to ensure that the elevator quick-fastener was properly secured, resulting in an inflight elevator control disconnect and subsequent loss of control during the ensuing emergency landing. Contributing…NTSB ERA12LA368Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Piney Flats, TNThe mechanic’s improper maintenance of the main transmission aft pinion nut and belt drive system, which resulted in the uncoupling of the tail rotor driveshaft and the subsequent loss of helicopter control.NTSB WPR12IA248Incident · No injuriesIncident investigationFinal reportEurocopter AS 350 B2 · Seattle, WAFailure of maintenance personnel to ensure that the tail rotor pitch change link bolt was properly secured, which resulted in an in-flight separation of the bolt and subsequent vibration.NTSB ERA12LA307Accident · No injuriesLimited investigationFinal reportRice Leo B Kitfox Series 5 · Port Canaveral, FLImpingement of the elevator control by foreign objects (clamp, glove) left in the flight control path by the pilot/owner or maintenance personnel.NTSB WPR12FA155Accident · 2 fatalField investigationFinal reportExtra Flugzeugbau EA-300 · Salinas, CAA loose portable XM-GPS antenna that migrated to the tail section of the airplane and jammed the elevator bell crank. Contributing to the accident was the pilot’s failure to account for the cockpit portable GPS antenna during preflight or postflight…NTSB WPR12WA167Incident · No injuriesForeign investigationSaab 2000 · Copenhagen, DenmarkOn March 20, 2012, about 0610 UTC, a Saab 2000, registered in Sweden as SE-LOM, experienced an elevator flight control malfunction during landing at Copenhagen Airport (EKCH), Denmark. None of the three flight crew or 47 passengers were injured. The airplane…NTSB ERA12IA237Incident · No injuriesIncident investigationFinal reportPiper PA-32R-300 · Warrenton, VAMaintenance personnel's failure to identify stress corrosion cracking in the stabilator control cable during the most recent inspection, and the subsequent failure of the cable on the flight after the inspection.NTSB ERA12CA215Accident · No injuriesData collectionFinal reportCessna 140A · Mooresville, NCThe separation of the left rudder cable turnbuckle and the pilot’s subsequent loss of directional control during landing.NTSB WPR12LA107Accident · Minor injuriesLimited investigationFinal reportBell AH-1F · Coolidge, AZA flight control malfunction while maneuvering for reasons that could not be determined because postaccident examination revealed no evidence of a mechanical malfunction or failure that would have precluded normal operation.NTSB DCA12CA042Accident · No injuriesData collectionFinal reportEmbraer EMB120 · Iliamna, AKthe maintenance personnel's failure to install the cotter pins that secured castellated nuts on the left elevator vertical hinge bolts, which resulted in the left elevator partially detaching in flight. Contributing to the accident was the failure of…NTSB ERA12LA150Accident · No injuriesLimited investigationFinal reportM-Squared Breese 2 · Bayou La Batre, ALThe pilot's inability to maintain control of the airplane for reasons that could not be determined because postaccident examination of the rudder control system did not reveal any anomalies that would have precluded control of the airplane.NTSB 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.NTSB ERA12FA127Accident · No injuriesField investigationFinal reportCessna 650 · Ft. Lauderdale, FLThe crew's failure to use proper emergency procedures during an uncommanded right roll after takeoff, which led to a forced landing with a quartering tailwind. Contributing to the accident was a faulty right roll spoiler actuator, which allowed the right roll…NTSB CEN12LA114Accident · Serious injuriesLimited investigationFinal reportSouthern Powered Parachute Condor · Rogersville, MOThe pilot's inadequate preflight inspection of the takeoff area, which resulted in a loss of control due to the binding of the parachute's lines.NTSB DCA13WA052Incident · No injuriesForeign investigationBeech 1900 · Goose Bay, CanadaOn 10 December 2011, at 1028 Newfoundland Standard Time, an Exploits Valley Air Services Hawker Beechcraft 1900D aircraft (registration C-GLHO, serial number UE-266), operating as Air Canada Express flight EV7645, was conducting a scheduled passenger flight…NTSB ERA12IA097Incident · No injuriesIncident investigationFinal reportCessna 560XL · Ocoee, FLWater contamination in the pitch trim actuators.NTSB DCA12WA007Accident · No injuriesForeign investigationBoeing 737 - 800 · Faro, PortugalTheAir AccidentInvestigation Unit (AAIU) ofIrelandhas notified the NTSB of an accidentinvolving a B737-8AS that occurred on October 20, 2011. The NTSBhas appointed a U.S. Accredited Representative to assist the AAIU investigationunder the provisions of ICAO…NTSB CEN11CA679Accident · No injuriesData collectionFinal reportWaltman Theodore J Moose · Hays, KSRudder flutter due to the design changes to the airplane's horizontal stabilizer.NTSB 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.NTSB CEN11LA588Accident · Minor injuriesLimited investigationFinal reportHendryx Steve/Wiley Ross Super Rebel · La Porte City, IAThe improper assembly of the aileron cable by the airplane builder.NTSB ERA11CA375Accident · No injuriesData collectionFinal reportTemco GC-1B · Sparta, TNThe improper installation of the right rudder control cable by maintenance personnel, which resulted in the pilot's inability to maintain directional control during takeoff.NTSB CEN11LA414Accident · No injuriesLimited investigationFinal reportEnstrom F-28C-2 · Blair, NEThe failure of a tail rotor pitch change link due to the retaining bolt becoming separated in flight. Contributing to the accident was the pilot’s inadequate preflight inspection.NTSB WPR11LA275Accident · Serious injuriesLimited investigationFinal reportBuckeye Breeze LX · Montague, CAThe unintended capture of the parachute bridle on a portion of the airframe during the takeoff roll, which resulted in a misinflated or misaligned parachute and an in-flight loss of control.NTSB CEN11CA326Accident · No injuriesData collectionFinal reportGetten Marvin T Quickie Q2 · Albuquerque, NMThe pilot's loss of elevator control, due to control stick's counter-weight binding with the airplane's header tank.NTSB WPR11IA213Incident · No injuriesIncident investigationFinal reportCessna 421B · Truckee, CAFatigue failure of the right flap extend cable during the landing approach.NTSB CEN11CA282Accident · No injuriesData collectionFinal reportDelf Tim Zenith CH-701 · Davenport, IAThe improper installation of the rudder cable to rudder pedal attachment hardware.NTSB CEN11IA286Incident · No injuriesIncident investigationFinal reportCessna 560XL · Abbeville, LAThe pitch trim control cable failed due to fatigue, rendering the elevator trim inoperative.NTSB CEN11LA275Accident · No injuriesLimited investigationFinal reportPiper PA-32-300 · Oklahoma City, OKThe loss of aircraft control due to the failure of the stabilator control cable turnbuckle.NTSB ERA11IA184Incident · No injuriesIncident investigationFinal reportCessna 560XL · Haynesville, VAThe manufacturer's inadequate design fix for previously known tailcone stinger water ingestion and retention.