NTSB investigations, 2008
37 cases where the sequence of events included Aircraft maintenance event.
Cases per year
| 2008 | 37 |
|---|---|
| 2009 | 34 |
| 2010 | 24 |
| 2011 | 32 |
| 2012 | 39 |
| 2013 | 33 |
| 2014 | 25 |
| 2015 | 33 |
| 2016 | 28 |
| 2017 | 27 |
| 2018 | 31 |
| 2019 | 14 |
| 2020 | 17 |
| 2021 | 25 |
| 2022 | 21 |
| 2023 | 32 |
| 2024 | 23 |
| 2025 | 9 |
Where
Open the mapLatest 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\" = '040' 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" = '040' 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 WPR09CA059Accident · No injuriesData collectionFinal reportCessna 210 · Sheridan, WYMaintenance personnel's failure to reinstall the left front pilot's seat correctly, which resulted in the pilot's loss of control and subsequent impact with a taxiway sign.NTSB WPR09CA064Accident · No injuriesData collectionFinal reportAir Tractor AT-502 · Dinuba, CAThe failure of maintenance personnel to properly install the engine's Py line correctly, which resulted in the total loss of engine power and subsequent force landing. Contributing to the accident was the lack of suitable terrain.NTSB WPR09LA052Accident · Serious injuriesLimited investigationFinal reportAdkins Ridge Runner II · Mulino, ORThe pilot's failure to attain an adequate airspeed that resulted in a stall/mush during the initial climb. Contributing to the accident were the pilot's lack of experience in this make and model airplane and the improper adjustment of the propeller pitch.NTSB WPR09LA048Accident · No injuriesLimited investigationFinal reportHughes 369HS · Fillmore, UTThe loss of engine power due to fuel starvation as a result of a loose fuel filter upper drain cap, which was not properly secured by maintenance personnel.NTSB ERA09LA047Accident · Minor injuriesLimited investigationFinal reportBell 206B · Boynton Beach, FLA loss of engine power due to an undertorqued air line fitting to the fuel control.NTSB WPR09LA025Accident · No injuriesLimited investigationFinal reportNaval Aircraft Factory N3N-3 · Rialto, CAA total loss of engine power during initial climb due to an interruption in fuel flow through an improperly assembled carburetor.NTSB ERA09LA057Accident · No injuriesLimited investigationFinal reportCampbell Earl S JR RV-6A · Cambridge, MDThe failure of the RV-6A's right brake assembly o-ring due to excessive heat.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 WPR09LA022Accident · 1 fatalLimited investigationFinal reportStinson 108-1 · Concrete, WAThe loss of engine power during initial climb due to the pilot's improper exhaust system maintenance, which resulted in restriction of the carburetor's air intake.NTSB ERA09LA015Accident · Serious injuriesLimited investigationFinal reportCessna 172 · Kissimmee, FLThe pilot's inadequate preflight inspection, which resulted in a total loss of engine power during initial climb due to fuel contamination. Contributing to the accident was a fuel tank cap that did not seal properly.NTSB MIA08CA201Accident · Serious injuriesData collectionFinal reportCox Clyde H Fshr Aero Vsns Clbty · Tampa, FLThe pilot’s failure to maintain control of the airplane during takeoff due to inadequate maintenance.NTSB SEA08LA206Accident · No injuriesLimited investigationFinal reportStearman C3-B · Stevenson, WAA loss of engine power due to fuel starvation from a piece of disintegrating gasket material that was blocking the fuel jet. Also causal was the failure of maintenance personnel to verify the condition of the gaskets when the carburetor was examined prior to…NTSB DCA08MA098Accident · 4 fatalClass 1 · MajorFinal reportLearjet LR60 · Columbia, SCThe operator’s inadequate maintenance of the airplane’s tires, which resulted in multiple tire failures during takeoff roll due to severe underinflation, and the captain’s execution of a rejected takeoff (RTO) after V1, which was inconsistent with her…NTSB MIA08LA196Accident · No injuriesLimited investigationFinal reportCessna 120 · Jesup, GAAn oil starvation-induced catastrophic engine failure due to the improper installation of the crankshaft expansion plug during engine overhaul.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 MIA08LA185Accident · No injuriesLimited investigationFinal reportBellanca 17-30A · Sparta, TNFailure of the nose landing gear mount during a normal landing due to an improper weld.NTSB DFW08LA223Accident · No injuriesLimited investigationFinal reportRockwell International S-2R · Uvalde, TXA total loss of engine power due to the improper use of unauthorized replacement parts in the engine and repeated operation of the engine in an over-temperature condition.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 ANC08LA113Accident · Minor injuriesLimited investigationFinal reportCessna 206 · Galena, AKThe en route loss of engine power due to a mechanic's failure to tighten a fuel line fitting, which became disconnected in flight.NTSB LAX08LA274Accident · 3 fatalLimited investigationFinal reportKillgore Velocity · North Las Vegas, NVA partial loss of engine power during initial climb due to the detachment of the engine supercharger drive belt. The detachment resulted from the owner/builder's inadequate installation of the supercharger system and belt-tensioning adjustment.NTSB LAX08LA269Accident · No injuriesLimited investigationFinal reportCessna TU206F · Glendale, AZA loose fuel line fitting that resulted in a partial loss of engine power during the initial takeoff climb. Contributing to the accident was inadequate maintenance installation of the fitting.NTSB DEN08LA138Accident · No injuriesLimited investigationFinal reportBell 206L-1 · Heber Springs, ARthe improper installation of the PC line on the engine which resulted in a partial loss of engine power. Contributing to the accident was the trees encountered during the forced landing.NTSB MIA08LA169Accident · No injuriesLimited investigationFinal reportPiper PA-32R-301 · Oxford, MSA loss of engine power due to fuel starvation as a result of maintenance personnel's failure to tighten a fuel line fitting.NTSB DFW08LA196Accident · No injuriesLimited investigationFinal reportPiper PA-36-285 · Petersburg, TXA partial loss of engine power due to the substandard and incomplete maintenance of the engine.NTSB CHI08IA200Incident · No injuriesIncident investigationFinal reportEclipse EA500 · Rockford, ILThe improper installation of the forward edge of the left-hand wing-to-body panel, causing the fairing to separate from the airplane during an in-flight encounter with light turbulence. Contributing to the event was the use of small-head screws and grommets…NTSB LAX08LA221Accident · Minor injuriesLimited investigationFinal reportCessna 172RG · Moorpark, CAA partial loss of engine power due to the disconnection of the throttle control cable from the throttle arm due to the operator's improper maintenance. Contributing to the accident was unsuitable terrain for a forced landing.NTSB MIA08FA122Accident · 1 fatalField investigationFinal reportYates Lancair IV-P · Springfield, KYA total loss of engine power due to a loss of engine oil as a result of the installation of the wrong oil adapter O-ring seal.NTSB NYC08LA213Accident · Minor injuriesLimited investigationFinal reportMarrin Pitts S-1 · St. Petersburg, FLThe pilot's failure to maintain adequate airspeed following a partial loss of engine power, which resulted in an aerodynamic stall. Contributing to the accident was improper maintenance practices during the construction of the airplane, which resulted in…NTSB LAX08LA184Accident · No injuriesLimited investigationFinal reportMooney M20J · Evanston, WYA collapse of the landing gear due to improper maintenance.NTSB CHI08LA160Accident · No injuriesLimited investigationFinal reportPiper PA-44-180 · Battle Creek, MIThe in-flight separation of the tip of a propeller blade due to metal fatigue that resulted from an inadequate inspection and repair.NTSB CHI08FA146Accident · 2 fatalField investigationFinal reportPiper PA28 · Hillsboro, OHThe pilot's failure to maintain control of the airplane due to an in-flight fire as a result of a corrosion hole in the muffler that was not identified by the mechanic. Contributing to the accident was the improper emergency procedure performed for an…NTSB NYC08LA165Accident · 1 fatalLimited investigationFinal reportDragon Fly GT-500 · Paris, TNA fuel system configuration that was not in accordance with the engine manufacturer's published guidance, which resulted in a complete loss of engine power due to fuel starvation.NTSB LAX08LA118Accident · Serious injuriesLimited investigationFinal reportCessna C175A · Groveland, CAA total loss of engine power due to fuel starvation as a result of a blocked fuel line that was improperly fabricated by the pilot. Also causal was the pilot's excessive ground speed during the taxi tests that resulted in an inadvertent takeoff.NTSB DFW08LA095Accident · No injuriesLimited investigationFinal reportHawker Beechcraft G36 · El Dorado, KSThe improper installation of the fuel manifold valve's brass plug. Contributing to the accident was the unsuitable landing area for the forced landing.NTSB LAX08LA063Accident · 1 fatalLimited investigationFinal reportWilson RV-7 · Nevada City, CAThe improper installation of the fuel pump, leading to a fatigue failure of the pump's lever arm and subsequent loss of engine power. Contributing to the accident was the lack of suitable terrain for a forced landing.NTSB LAX08LA055Accident · No injuriesLimited investigationFinal reportCessna 152 · Palo Alto, CALoss of engine power during the takeoff initial climb due to lack of compression to a cylinder.NTSB NYC08LA086Accident · Minor injuriesLimited investigationFinal reportPiper PA-28-R200 · York, SCLoss of engine power due to improper welding of the crankcase, which resulted in fatigue failure of the through-studs and a subsequent separation of the number two cylinder. Contributing to the accident was the unsuitable terrain for a forced landing.