NTSB investigations
83 cases where NTSB found Empennage structure.
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 f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f.\"findingCode\", '010355')) 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 f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f."findingCode", '010355')) 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 CEN12LA531Accident · No injuriesLimited investigationFinal reportRistine Avid Mark IV · Poplar Grove, ILThe failure of the lower right side longeron tail-spring support area during landing due to excessive corrosion.NTSB WPR12MA034Accident · 5 fatalMajor investigationFinal reportEurocopter EC 130 B4 · Pukoo, HIThe pilot's failure to maintain clearance from mountainous terrain while operating in marginal weather conditions, which resulted in the impact of the horizontal stabilizer and lower forward portion of the fenestron with ground and/or vegetation and led to…NTSB ERA12FA018Accident · 1 fatalField investigationFinal reportBerger Michael A Waiex · Washington, GAThe in-flight failure of the aircraft’s Y-tail attachment structure during maneuvering flight due to overload. Contributing to the accident was, the kit manufacturer’s use of 14 CFR Part 23, Appendix A design guidelines intended for a conventional tail…NTSB CEN11CA679Accident · No injuriesData collectionFinal reportWaltman Theodore J Moose · Hays, KSRudder flutter due to the design changes to the airplane's horizontal stabilizer.NTSB WPR11MA454Accident · 11 fatalClass 1 · MajorFinal reportNorth American/Aero Classics P-51D · Reno, NVThe reduced stiffness of the elevator trim tab system that allowed aerodynamic flutter to occur at racing speeds. The reduced stiffness was a result of deteriorated locknut inserts that allowed the trim tab attachment screws to become loose and to initiate…NTSB WPR11LA265Accident · No injuriesLimited investigationFinal reportAerovodochody L-29 Delfin · Reno, NVThe failure of a modified engine mount to keep the engine properly aligned, which resulted in partial failure of the rudder support structure due to the deflection of the jet engine exhaust.NTSB ANC11LA027Accident · No injuriesLimited investigationFinal reportPiper PA-32-301 · Cold Bay, AKAn in-flight encounter with unforecast turbulence, which resulted in structural damage to the stabilator.NTSB WPR11FA155Accident · 1 fatalField investigationFinal reportMuse KR2 · Newberry Springs, CAThe airplane’s encounter with severe turbulence, which resulted in the in-flight breakup of the airplane. Contributing to the accident was the pilot’s inadequate preflight planning.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 ERA11LA141Accident · No injuriesLimited investigationFinal reportPiper PA-31-350 · Baltimore, MDAn in-flight overload failure of the left elevator inboard balance weight rib for undetermined reasons.NTSB CEN11IA111Incident · No injuriesIncident investigationFinal reportCessna 560XL · Birmingham, ALThe manufacturer's inadequate initial design and inadequate subsequent modifications of the tailcone, which allowed moisture to collect and freeze around rudder cables during operations in subfreezing temperatures, resulting in a loss of rudder authority…NTSB CEN11IA087Incident · No injuriesIncident investigationFinal reportCessna 560XL · Toledo, OHThe manufacturer's inadequate initial design and subsequent modifications of the tailcone, which allowed moisture to collect and freeze around rudder cables during flight levels above the freezing level and resulted in a loss of rudder authority. Contributing…NTSB ANC11LA004Accident · No injuriesLimited investigationFinal reportBeech 1900C · Sitka, AKA lightning strike which resulted in substantial damage to the elevator.NTSB CEN10CA569Accident · Minor injuriesData collectionFinal reportCentral Ohio Dragonfly Clubllc DRAGONFLY-C · Orient, OHThe pilot's failure to disconnect the tow bridal line prior to takeoff.NTSB ERA10CA477Accident · Minor injuriesData collectionFinal reportBeam-Walter RS-15 · Windsor, VAThe pilot's inadequate installation and preflight inspection of the right rudervator assembly, which resulted in a loss control during takeoff.NTSB ERA10LA328Accident · No injuriesLimited investigationFinal reportParks J L/Dreffin D Seawind 3000 · Sanibel Island, FLAn overstress failure of the elevator. Contributing to the accident was the owner/builder's modification of the experimental airplane beyond the recommendations of the kit manufacturer.NTSB WPR10LA306Accident · No injuriesLimited investigationFinal reportLuscombe 11A · Merced, CAThe pilot’s inability to maintain airplane control during cruise flight due to the failure of the elevator trim tab as a result of missing hardware for the elevator control cable bellcrank to elevator torque tube attachment bracket.NTSB WPR10CA226Accident · No injuriesData collectionFinal reportBeech B35 · Burbank, CAThe airplane's encounter with turbulence while at an airspeed above maneuvering airspeed, which exceeded the limit load of the stabilizers and ruddervators.NTSB ERA10LA166Accident · Minor injuriesLimited investigationFinal reportBelcher William B II Firestar · Wetumpka, ALThe student pilot’s in-flight loss of control as a result of previous damage to the airplane from an undetermined event.NTSB 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,…NTSB ERA09LA502Accident · 2 fatalLimited investigationFinal reportM-Squared Sprint 1000 · Madeira Beach, FLA loss of torque to the gearbox engine-side coupling flange bolts, which resulted in separation of the gearbox and propeller from the engine and the subsequent severing of the airplane's tail structure.NTSB ERA09LA492Accident · 1 fatalLimited investigationFinal reportBond Neal O S-9 · Saylorsburg, PAThe pilot’s excessive flight control inputs that resulted in an overload failure of the right elevator and horizontal stabilizer.NTSB ERA09LA392Accident · 1 fatalLimited investigationFinal reportNoles Vance L Vans RV7A · Sanderson, FLThe pilot's continued visual flight into instrument meteorological conditions with convective activity and thunderstorms. Contributing to the accident was his failure to get an adequate weather briefing.NTSB WPR09IA070Incident · No injuriesIncident investigationFinal reportMD Helicopter MD 900 · Kamuela, HIThe separation of the endplate bolts for undetermined reasons, resulting in an in-flight separation of the right endplate. Contributing to the accident was the manufacturer's failure to provide sufficient guidance for endplate bolt installation.NTSB ERA09FA029Accident · 2 fatalField investigationFinal reportPiper PA-24 · Red Hill, VAThe pilot's failure to maintain aircraft control due to an improper repair to the stabilator, which resulted in an in-flight failure of the stabilator. Contributing to the accident was the descent in turbulence, at airspeeds above the maximum structural…NTSB CEN09LA023Accident · Serious injuriesLimited investigationFinal reportPiper PA-36-285 · Silverton, TXThe pilot's failure to maintain clearance from a transmission wire.NTSB SEA08FA196Accident · 1 fatalField investigationFinal reportDebus J / Mountain S / Bowes E DEBUS-CASST-SNOSHOO · Reno, NVThe movement of the airplane’s modified horizontal stabilizer trim system during an intentional high speed aerobatic maneuver that resulted in exceedence of the design stress limits of the airplane and an in-flight structural failure. Contrubuting to the…NTSB CHI08MA270Accident · 3 fatalMajor investigationFinal reportConvair CV-580 · Columbus, OHThe improper (reverse) rigging of the elevator trim cables by company maintenance personnel, and their subsequent failure to discover the misrigging during required post-maintenance checks. Contributing to the accident was the captain’s inadequate…NTSB CHI08FA172Accident · No injuriesField investigationFinal reportEnstrom Helicopter 480B · Marinette, WIThe pilot inadvertently operating the helicopter at a gross weight greater than its maximum allowable operating weight, and flying the helicopter at an airspeed greater than the never-to-exceed speed for the helicopter’s gross weight condition, resulting in…NTSB CHI08CA168Accident · No injuriesData collectionFinal reportWolseley Motors SE5-A · Seymour, INThe pilot/builder's failure to manufacture the airplane with an appropriate engine thrust angle. Contributing to the accident was the pilot/builder's adjustment of the horizontal stabilizer which rendered the airplane uncontrollable.NTSB LAX08LA160Accident · 1 fatalLimited investigationFinal reportQuad City Ultralight Challenger LSS · Moses Lake, WAThe pilot's inability to maintain control due to an in-flight separation of the vertical fin as a result of the failure of the airplane's builder to properly secure the vertical fin to the fuselage.NTSB CHI08IA109Incident · No injuriesIncident investigationFinal reportEclipse EA500 · Pontiac, MIThe inadvertent stalling of the rudder trim actuator motor during flight due to the pilot's unintentional exceedence of the motor's design limit for stalling while accelerating after completing a simulated engine-out maneuver.NTSB MIA08CA088Accident · Serious injuriesData collectionFinal reportWilliam E. Furr SeaRey · Winter Springs, FLThe pilot's inadequate preflight inspection of the airplane.