NTSB investigations, OR
19 cases where NTSB found Engine (reciprocating).
Cases per year
| 2008 | 3 |
|---|---|
| 2010 | 3 |
| 2011 | 1 |
| 2013 | 2 |
| 2014 | 1 |
| 2018 | 1 |
| 2019 | 2 |
| 2020 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 1 |
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 c.\"eventStateOrRegion\" = 'OR' AND c.\"eventCountry\" = 'USA'
AND c.\"mKey\" IN (SELECT f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f.\"findingCode\", '010585'))
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."eventStateOrRegion" = 'OR' AND c."eventCountry" = 'USA' AND c."mKey" IN (SELECT f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f."findingCode", '010585')) 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 WPR25LA010Accident · No injuriesClass 4 · LimitedFinal reportEnstrom Helicopter 280C · Vale, ORThe pilot’s failure to maintain engine and rotor rpm during takeoff, that resulted in a hard landing.NTSB WPR23LA184Accident · No injuriesClass 3 · LimitedFinal reportRans S-21 · Creswell, ORA total loss of engine power caused by fatigue cracking and fracture of the crankshaft due to severe wear of the bearings.NTSB WPR22LA193Accident · No injuriesClass 3 · LimitedFinal reportVans RV-8 · Galice, ORThe in-flight failure of the crankshaft gear’s alignment dowel as a result of the retaining bolt not being installed, which lead to a total loss of engine power.NTSB WPR22LA177Accident · No injuriesClass 3 · LimitedFinal reportPiper PA-12 · Enterprise, ORThe inadequate maintenance and inspection of the crankshaft expansion plug, which resulted in the separation of the expansion plug from the crankshaft and the subsequent loss of oil and windshield obstruction during departure.NTSB WPR22LA019Accident · No injuriesClass 3 · LimitedFinal reportLancair ES · Fall Creek, ORTotal loss of engine power due to fatigue failure of the camshaft gear.NTSB WPR20LA097Accident · No injuriesClass 3 · LimitedFinal reportCessna 170 · Baker City, ORThe failure of the No. 2 connecting rod bearing as a result of oil starvation due to a contaminated oil filter screen.NTSB WPR19LA217Accident · No injuriesClass 3 · LimitedFinal reportCessna 206 · Prospect, ORThe failure of the counterweight retainer pin plate which resulted in a total loss of engine power.NTSB WPR19LA207Accident · No injuriesClass 3 · LimitedFinal reportStinson 108 · Klamath Falls, ORThe mechanic’s failure to identify an engine performance issue, which led to a partial loss of engine power. Contributing to the accident was the pilot’s decision to operate the airplane with a known mechanical deficiency.NTSB WPR18LA193Accident · Minor injuriesClass 3 · LimitedFinal reportCessna 150 · Ontario, ORA total loss of engine power during final approach for reasons that could not be determined based on the available information.NTSB WPR15LA032Accident · Minor injuriesLimited investigationFinal reportCessna T210M · Jacksonville, ORA loss of engine power during cruise flight due to the failure of the No. 6 connecting rod, which resulted from oil starvation.NTSB WPR14LA055Accident · Serious injuriesLimited investigationFinal reportRichard S Duncan Avid Flyer · Lakeside, ORThe pilot/owner’s failure to comply with the engine manufacturer’s maintenance guidance, which resulted in the total loss of engine power due to the fracture failure of the plastic drive gear for the engine lubricating oil pump.NTSB WPR13LA363Accident · No injuriesLimited investigationFinal reportQuarnoccio Avid Flyer · White City, ORExcessive engine operating temperature, which resulted in engine failure and a forced landing. The reason for the excessive engine operating temperature could not be determined during postaccident engine examination.NTSB WPR11LA290Accident · Minor injuriesLimited investigationFinal reportChristen Industries Pitts S-1T · Alkali Lake, ORThe loss of engine oil during cruise flight due to the failure of the front bearing oil seal.NTSB WPR10LA424Accident · No injuriesLimited investigationFinal reportGrumman American Avn. AA-5A · Lakeview, ORA partial loss of engine power during the initial climb due to a stuck exhaust valve.NTSB WPR10LA419Accident · No injuriesLimited investigationFinal reportHummel / Finberg Ultra Cruiser · Canby, ORThe loss of engine power due to low cylinder compression.NTSB WPR10LA168Accident · No injuriesLimited investigationFinal reportCessna 150F · Tillamook, ORThe partial loss of engine power during climb to cruise due to carburetor icing and the pilot's delay in using carburetor heat.NTSB SEA08LA193Accident · Serious injuriesLimited investigationFinal reportWasson Loehle Loehle P-40 · Oregon City, ORThe loss of total engine power due to a cold seizure.NTSB SEA08LA156Accident · Serious injuriesLimited investigationFinal reportCessna TR182 · Bend, ORThe failure of the crankshaft during cruise flight due to fatigue.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.