NTSB investigations, 2008
23 cases where the sequence of events included Flight control sys malf/fail.
Cases per year
| 2008 | 23 |
|---|---|
| 2009 | 15 |
| 2010 | 30 |
| 2011 | 26 |
| 2012 | 29 |
| 2013 | 23 |
| 2014 | 16 |
| 2015 | 24 |
| 2016 | 20 |
| 2017 | 25 |
| 2018 | 16 |
| 2019 | 16 |
| 2020 | 17 |
| 2021 | 26 |
| 2022 | 24 |
| 2023 | 14 |
| 2024 | 25 |
| 2025 | 27 |
| 2026 | 14 |
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 year(c.\"eventDate\") = 2008
AND 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 year(c."eventDate") = 2008 AND 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 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 ERA09LA107Accident · Minor injuriesLimited investigationFinal reportMoore David DM-1 · Salters, SCA hard landing following an autorotation that resulted from the separation of the red main rotor blade cap that led to the uncontrolled movement of the cyclic, autorotation and a hard landing.NTSB WPR09LA028Accident · Minor injuriesLimited investigationFinal reportHiller UH-12E · Powder River, WYA flight control system malfunction while the helicopter was maneuvering at low altitude due to the failure/separation of the rotor blade control tube.NTSB CEN09IA032Incident · No injuriesIncident investigationFinal reportMD Helicopter MD 900 · Amherst, TXThe failure of the vertical stabilizer control adapter due to reverse bending fatigue.NTSB CEN09IA003Incident · No injuriesIncident investigationFinal reportMD Helicopter MD 900 · Weatherford, TXThe failure of the vertical stabilizer control adapter due to reverse bending fatigue.NTSB ERA09IA009Incident · No injuriesIncident investigationFinal reportCirrus Design SR22 · Lakeland, FLA failure of the flap actuator rod end due to low stress, high cycle fatigue, and subsequent overstress failure.NTSB NYC08LA318Accident · No injuriesLimited investigationFinal reportHiller UH-12E · Naruna, VAThe fatigue failure of a main rotor blade drag strut.NTSB MIA08LA187Accident · No injuriesLimited investigationFinal reportPiper J5A · Atlanta, GAThe loss of pitch control due to slippage of the elevator control cable resulting from the maintenance personnel’s improper installation and inspection of the cable.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 LAX08LA251Accident · No injuriesLimited investigationFinal reportCessna TU206E · Murrieta, CAA malfunction of the flight control system and loss of engine power for undetermined reasons.NTSB NYC08LA259Accident · Serious injuriesLimited investigationFinal reportSands Thomas E Rotorway 162 · Graysville, TNA loss of control for undetermined reasons.NTSB LAX08IA241Incident · No injuriesIncident investigationFinal reportMD Helicopters MD 902 · Salinas, CAThe pilot's inability to maintain directional control due to the fatigue failure of the threaded portion of the forward directional control cable as a result of the improper installation a lock washer.NTSB LAX08LA226Accident · No injuriesLimited investigationFinal reportJonsson Sonerai · Hood River, ORThe pilot's failure to maintain directional control during the emergency landing roll with a tailwind. Contributing was the partial separation of the left aileron that prompted the pilot to attempt the emergency landing.NTSB CHI08IA182Incident · No injuriesIncident investigationFinal reportMcdonnell Douglas MD-81 · St. Louis, MOThe inadvertent partial inflation of the evacuation slide within the tailcone during takeoff and subsequent binding of the elevator control cables. The partial inflation resulted from the tailcone evacuation slide cover failing to be secured to the floor…NTSB ANC08LA083Accident · No injuriesLimited investigationFinal reportBell UH-1B · Iliamna, AKThe failure of company maintenance personnel to ensure the helicopter was properly maintained, resulting in a severe in-flight vibration due to collective bounce. Contributing to the accident was loose and worn bearings on the helicopter's stabilizer bar,…NTSB CHI08LA190Accident · No injuriesLimited investigationFinal reportde Havilland DHC-6-200 · Baldwin, WIUndetermined.NTSB CHI08LA169Accident · No injuriesLimited investigationFinal reportMorrison E-Racer · Aurora, ILAn undetermined failure in the high-pressure fuel system, and the subsequent loss of engine power and in-flight fire. Contributing to the accident were the pilot's restricted visibility due to the smoke in the cockpit, failure of the aileron control during…NTSB MIA08LA121Accident · 1 fatalLimited investigationFinal reportMckeehan James F Acroduster II SA750 · Panama City, FLThe pilot's inability to recover from an intentional aerobatic maneuver due to loss of aileron control. Contributing to the accident was the installation of an inadequate aileron secondary stop block against the main spar of both lower wings.NTSB ENG08WA029IncidentForeign investigationBoeing 737-2A5 · Pucallpa, PeruOn June 6, 2008, at approximately 1810 local time, OB-1799-P, a Boeing 737-2A5, operated by Aero Condor S.A.C., returned to the FAP Captain David Abenzur Rengifo International Airport, (SPCL), Pucallpa Peru, after experiencing a very strong vibration after…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 NYC08LA129Accident · Serious injuriesLimited investigationFinal reportSikorsky S-58HT · Belmont, WVThe fatigue failure of a tail rotor blade during an external load lift.NTSB DEN08FA058Accident · 1 fatalField investigationFinal reportPiper PA-23-250 · Sterling, KSThe loss of pitch control during cruise flight resulting from the separation of the stabilator trim actuator due to inadequate maintenenace.