NTSB investigations, 2008
62 cases where the sequence of events included Powerplant sys/comp malf/fail.
Cases per year
| 2008 | 62 |
|---|---|
| 2009 | 57 |
| 2010 | 28 |
| 2011 | 37 |
| 2012 | 36 |
| 2013 | 40 |
| 2014 | 36 |
| 2015 | 36 |
| 2016 | 50 |
| 2017 | 40 |
| 2018 | 38 |
| 2019 | 46 |
| 2020 | 30 |
| 2021 | 35 |
| 2022 | 55 |
| 2023 | 57 |
| 2024 | 60 |
| 2025 | 41 |
| 2026 | 37 |
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\" = '340' 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" = '340' 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 ERA09LA108Accident · Serious injuriesLimited investigationFinal reportBeech E18S · Fort Myers, FLThe failure of the right propeller to go to the feathered position for undetermined reasons following a total loss of right engine power during initial climb due to fuel starvation as a result of the pilot's improper fuel planning.NTSB ERA09FA093Accident · 1 fatalField investigationFinal reportBeech 36 · Louisville, KYThe pilot’s continued operation of the aircraft with known deficiencies. Contributing to this accident was the improper sealing of the engine case during overhaul.NTSB ERA09LA072Accident · Serious injuriesLimited investigationFinal reportLeroy Lakey Corben ACE · Cherryville, NCA throttle control malfunction during initial climb, as reported by the pilot.NTSB CEN09CA080Accident · No injuriesData collectionFinal reportBeech E35 · Bloomington, INA partial loss of engine power due to a failure of the number one cylinder exhaust valve, and the associated secondary damage to the intake valve and piston.NTSB ERA09LA062Accident · Minor injuriesLimited investigationFinal reportCirrus Design SR20 · Green Cove Springs, FLThe fusing of an electrical cable from the No. 2 (standby) alternator with the throttle cable resulting in the flight crew’s inability to move the throttle control. Contributing to the accident was the failure of maintenance personnel to detect inadequate…NTSB ERA09CA054Accident · No injuriesData collectionFinal reportSnow 600 · Nashville, TNThe failure of the propeller shaft seal in flight. Contributing to the accident was the lack of suitable terrain for a forced landing.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 CEN09LA055Accident · No injuriesLimited investigationFinal reportPiper PA-28-140 · Nacogdoches, TXThe loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.NTSB ERA09CA040Accident · Minor injuriesData collectionFinal reportFox Jack G Mong Biwin · Thomasville, NCThe builder’s failure to set adequate propeller pitch during propeller installation.NTSB ANC09LA009Accident · Minor injuriesLimited investigationFinal reportConstrucciones Aeronauticas CASA-212 · Toksook Bay, AKThe flight crew’s inability to adjust/increase power to the right engine during the landing approach due to an in-flight disconnect of the engine power control linkage, resulting in a loss of control of the airplane. Contributing to the accident was the…NTSB WPR09LA013Accident · No injuriesLimited investigationFinal reportPiper PA-31-350 · Portland, ORAn in-flight engine fire due to the fatigue fracture of an exhaust pipe that resulted from a failure of the pipe's slip joint.NTSB CEN09LA014Accident · No injuriesLimited investigationFinal reportBeech A36 · Houston, TXThe total loss of engine power due to a fracture in the oil filter adapter housing. Contributing to the accident was the lack of suitable terrain for the forced landing.NTSB NYC08CA325Accident · No injuriesData collectionFinal reportAeronca 7AC · Mt. Pleasant, SCThe pilot's failure to maintain aircraft control during an emergency maneuver. Contributing to the accident was the failure of the left magneto.NTSB DEN08LA163Accident · Minor injuriesLimited investigationFinal reportBeech C23 · Duncan, OKA total loss of engine power due to the fatigue failure of the engine crankshaft. Contributing to the accident were the improper maintenance to the engine crankshaft, improper reassembly of the engine, and failure to follow the engine manufacturer's overhaul…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 DFW08CA236Accident · No injuriesData collectionFinal reportPiper PA-32R-300 · Augusta, KSA loose oil line that resulted in a total loss of engine oil, causing the engine to cease.NTSB CHI08CA284Accident · No injuriesData collectionFinal reportFleet 2 · Leroy, OHThe loss of engine power due to the propeller hub failure during a low-level maneuver. Contributing to the accident were the trees encountered during the forced landing.NTSB LAX08LA292Accident · No injuriesLimited investigationFinal reportCessna T210N · Oakland, CAA loss of engine power while maneuvering due to the disintegration of the number two main bearing, which resulted in a fracture of the crankshaft. Contributing to the accident was inadequate maintenance.NTSB DFW08LA226Accident · Serious injuriesLimited investigationFinal reportCessna 182D · Orange Grove, TXA total loss of engine power due to an improperly installed intake manifold tube.NTSB CHI08LA274Accident · Minor injuriesLimited investigationFinal reportSadler Vampire · Findlay, OHA total loss of engine power due to the failure of the reduction drive assembly as a result of excessive wear and high temperatures. Contributing to the accident were the pilot's lack of total experience in the airplane and the unsuitable terrain for a forced…NTSB SEA08GA194Accident · 3 fatalFinal reportLockheed P2V-7 · Reno, NVThe failure of the flight crew to maintain airspeed above in-flight minimum control speed (Vmca) after losing power in the left jet engine during initial climb after takeoff. Contributing to the accident was the crew's inadequate cockpit resource management…NTSB SEA08LA193Accident · Serious injuriesLimited investigationFinal reportWasson Loehle Loehle P-40 · Oregon City, ORThe loss of total engine power due to a cold seizure.NTSB MIA08CA178Accident · No injuriesData collectionFinal reportDehavilland DH82A · Sevierville, TNThe failure of the wooden propeller.NTSB DFW08CA211Accident · No injuriesData collectionFinal reportMurray Frank H DA5B · Odessa, TXFailure of the intake manifold when the flexible connectors disconnected from the carburetor after a turbulence encounter. Contributing to the accident was insuitable terrain for a forced landing.NTSB NYC08LA291Accident · No injuriesLimited investigationFinal reportCessna 441 · Baltimore, MDThe pilot's delayed decision to abort the takeoff. Contributing to the accident was the pilot's attempted takeoff with a propeller start lock inadvertently engaged.NTSB LAX08LA268Accident · No injuriesLimited investigationFinal reportRouse Glasair III · Reno, NVThe excessively worn throttle/mixture linkage arms and pins and a missing mixture control linkage spring washer, which resulted in a loss of power due to an excessively rich mixture.NTSB ENG08IA038Incident · No injuriesIncident investigationFinal reportBoeing 757 · Las Vegas, NVThe engine experienced an uncontained release of high pressure turbine material due to fatigue cracks that occurred on four consecutive blade retainig lugs on the 2nd stage turbine hub. The cracked lugs resulted in the release of four 2nd stage turbine blades…NTSB DEN08CA135Accident · No injuriesData collectionFinal reportGrumman G-164A · Walsh, COThe total failure of a cylinder head assembly. Contributing to the accident was the lack of suitable terrain for a forced landing.NTSB ANC08LA097Accident · Serious injuriesLimited investigationFinal reportPiper PA-31-350 · Aniak, AKA partial loss of engine power during takeoff due to a failure of the left engine's turbocharger as a result of the failure of a turbine shaft bearing. Contributing to the accident was unsuitable terrain for a forced landing.NTSB ANC08WA098Accident · Serious injuriesForeign investigationBeech 65-A90 · Pitt Meadows, CanadaNTSB CHI08LA230Accident · Minor injuriesLimited investigationFinal reportCessna 172RG · Tomahawk, WIA total loss of engine power due to a loss of all of the engine's oil as a result of the safety wire on the governor idler gear shaft's oil plug breaking, leading to the oil plug coming unscrewed. Contributing to the accident was the lack of a suitable area…NTSB ANC08IA092Incident · No injuriesIncident investigationFinal reportSaab-Scania Saab 340B · Anchorage, AKThe failure of one of the stage 1 gas generator rotor blades due to high-cycle fatigue, resulting in a contained engine failure during the takeoff roll.NTSB ANC08LA089Accident · No injuriesLimited investigationFinal reportDehavilland DHC-3 · Iliamna, AKA total loss of engine power due to the separation of the number 8 cylinder from the engine, which separated an oil line, resulting in a loss of oil and oil pressure. Contributing to the accident was the float-equipped airplane's forced landing on a road.NTSB NYC08LA251Accident · No injuriesLimited investigationFinal reportHolmes Arthur Orman Kitfox IV · Burkesville, KYThe total loss of engine power due to the installation of an engine oil filter that did not meet the engine manufacture's specifications.NTSB MIA08LA142Accident · Serious injuriesLimited investigationFinal reportJ. E. Douglas Starduster 2 · Tappahannock, VALoss of engine power for undetermined reasons.NTSB LAX08LA230Accident · Minor injuriesLimited investigationFinal reportBell UH-1H · Rock Springs, WYA total loss of engine power due to the failure of the No. 1 bearing for undetermined reasons.NTSB SEA08LA156Accident · Serious injuriesLimited investigationFinal reportCessna TR182 · Bend, ORThe failure of the crankshaft during cruise flight due to fatigue.NTSB LAX08LA195Accident · No injuriesLimited investigationFinal reportArrow Falcon Exporters OH-58C · Fresno, CAThe loss of engine power due to fatigue failure of a second stage compressor blade.NTSB DEN08LA108Accident · No injuriesLimited investigationFinal reportMercer Avid Flyer Mk IV · Augusta, KSFailure of the engine cooling system's thermostat, causing the engine to overheat and seize. Contributing to the accident was the fence.NTSB ANC08LA060Accident · No injuriesLimited investigationFinal reportPiper PA-34 · Ocala, FLThe pilot's continued operation of the airplane with a known mechanical deficiency--a propeller that would feather at low power. Contributing to the accident was the uncommanded feathering of the propeller.NTSB LAX08LA168Accident · No injuriesLimited investigationFinal reportMkii Lancair Legacy 2000 · Bend, ORA total loss of engine power due to the fatigue failure of the Number 3 cylinder connecting rod.NTSB CHI08LA154Accident · No injuriesLimited investigationFinal reportBeech A36 · Grand Rapids, MNA loss of engine thrust due to the propeller separating from the aircraft as a result of fatigue failure of the propeller attachment bolts caused by the insufficient torque of the bolts during installation.NTSB NYC08CA208Accident · Minor injuriesData collectionFinal reportCessna 177RG · Bessemer, ALFailure of the left magneto for undetermined reasons resulting in a partial loss of engine power during takeoff.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 CHI08IA152Incident · No injuriesIncident investigationFinal reportEclipse EA500 · Chicago, ILThe airplane manufacturer's inadequate software design requirements of the engine's full authority digital electronic controls (FADEC) fault logic that resulted in a simultaneous unrecoverable loss of thrust control on both engines when the FADEC's input data…NTSB NYC08LA196Accident · Minor injuriesLimited investigationFinal reportBoeing A75N1 · Romney, WVA partial loss of engine power during takeoff due to failure of the left magneto. Contributing to the accident was unsuitable terrain to conduct a forced landing.NTSB CHI08CA139Accident · No injuriesData collectionFinal reportCessna 172N · Blue Ash, OHThe separation of the throttle cable from the linkage during the approach to land and the altitude/clearance not being available to the pilot during the forced landing. Contributing to the accident was the electrical wires the airplane impacted.NTSB LAX08LA153Accident · No injuriesLimited investigationFinal reportCessna P210N · Peach Springs, AZA loss of engine power due to induced catastrophic internal failure of the engine as a result of the displacement and rotation of the number 2 main bearing that resulted in a fatigue fracture of the crankshaft.NTSB ENG08IA027Incident · No injuriesIncident investigationFinal reportBoeing MD-11F · Miami, FLThe insufficient predicted fatigue life of the P/N KBE6-59 adjustable-length 3/8-inch rod end, and the inadequate fatigue margin at the transcowl CDU clevis assembly bracket attachment rivets for the one actuator out condition, which resulted in the failure…NTSB CHI08LA125Accident · Serious injuriesLimited investigationFinal reportRans S-12 XL · Pelion, SCA loss of engine power due to the improper actions of the instructor pilot and the low experience level of the instructor pilot in this make and model of aircraft.