NTSB investigations: Lycoming 0-540 series, 2013
15 cases on aircraft whose registry engine model is Lycoming 0-540 series. Aircraft are matched to the registry by N-number and event date, checked against the reported serial number, make and model, so older matches can be wrong.
Cases per year
| 1964 | 146 |
|---|---|
| 1965 | 151 |
| 1966 | 150 |
| 1967 | 192 |
| 1968 | 128 |
| 1969 | 110 |
| 1970 | 110 |
| 1971 | 118 |
| 1972 | 115 |
| 1973 | 83 |
| 1974 | 98 |
| 1975 | 83 |
| 1976 | 77 |
| 1977 | 97 |
| 1978 | 78 |
| 1979 | 92 |
| 1980 | 82 |
| 1981 | 80 |
| 1982 | 58 |
| 1983 | 59 |
| 1984 | 51 |
| 1985 | 59 |
| 1986 | 29 |
| 1987 | 47 |
| 1988 | 41 |
| 1989 | 35 |
| 1990 | 39 |
| 1991 | 31 |
| 1992 | 28 |
| 1993 | 26 |
| 1994 | 41 |
| 1995 | 41 |
| 1996 | 41 |
| 1997 | 26 |
| 1998 | 30 |
| 1999 | 35 |
| 2000 | 35 |
| 2001 | 40 |
| 2002 | 52 |
| 2003 | 39 |
| 2004 | 35 |
| 2005 | 39 |
| 2006 | 43 |
| 2007 | 30 |
| 2008 | 38 |
| 2009 | 37 |
| 2010 | 28 |
| 2011 | 37 |
| 2012 | 24 |
| 2013 | 15 |
| 2014 | 31 |
| 2015 | 24 |
| 2016 | 27 |
| 2017 | 25 |
| 2018 | 25 |
| 2019 | 32 |
| 2020 | 24 |
| 2021 | 28 |
| 2022 | 25 |
| 2023 | 30 |
| 2024 | 23 |
| 2025 | 25 |
| 2026 | 23 |
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\") = 2013
AND c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('41532'))
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") = 2013
AND c."mKey" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('41532'))
ORDER BY c."eventDate" DESC, c."ntsbNumber" DESCRun 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 ANC13FAMS2Accident · 1 fatalMissing aircraftFinal reportPiper PA-32-260 · Yakutat, AKUndetermined because the pilot and airplane were not found.NTSB ERA13LA408Accident · Minor injuriesLimited investigationFinal reportPiper PA-24-250 · Woodstock, CTThe pilot’s improper preflight inspection, which resulted in fuel exhaustion and a total loss of engine power.NTSB WPR13CA367Accident · No injuriesData collectionFinal reportPiper PA-24-250 · Hesperia, CAThe pilot’s failure to maintain sufficient airspeed on final approach to landing which resulted in an inadvertent stall.NTSB WPR13LA322Accident · No injuriesLimited investigationFinal reportPiper PA-28-235 · Albany, ORThe loss of hydraulic fluid, which rendered the brakes ineffective. The reason for the loss of hydraulic fluid could not be determined based on the available evidence.NTSB CEN13LA520Accident · No injuriesLimited investigationFinal reportPiper PA-25-235 · Boonville, MOThe pilot’s failure to maintain directional control of the airplane during landing on a gravel road.NTSB WPR13LA295Accident · No injuriesLimited investigationFinal reportRobinson Helicopter R44 · Fielding, UTThe pilot's failure to maintain rotor rpm while traversing a canyon in high-density altitude and gusting wind conditions.NTSB CEN13LA379Accident · No injuriesLimited investigationFinal reportPiper PA-25-235 · Salisbury, MOThe airplane's reduced braking efficiency and the pilot's subsequent delayed decision to go around, which resulted in a loss of directional control.NTSB ERA13CA280Accident · No injuriesData collectionFinal reportPiper PA-25-260 · Hollywood, FLThe pilot's failure to maintain directional control during the landing roll.NTSB CEN13CA319Accident · No injuriesData collectionFinal reportCessna TR182 · Emporia, KSThe pilot's failure to lower the landing gear prior to landing.NTSB CEN13FA259Accident · 1 fatalField investigationFinal reportPiper PA-25-235 · Lamar, MOThe pilot's in-flight loss of control, which was likely due to a sudden cardiac event.NTSB ERA13CA164Accident · Minor injuriesData collectionFinal reportPiper PA-25-235 · Groveland, FLThe pilot's failure to maintain the proper airspeed during a tailwind approach, his improper decision to continue a fast approach with a tailwind rather than go around, and his improper use of the wheel brakes during the landing roll.NTSB WPR13LA109Accident · No injuriesLimited investigationFinal reportPiper PA-28-235 · Bountiful, UTA total loss of engine power during initial climb for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.NTSB WPR13LA094Accident · No injuriesLimited investigationFinal reportPiper PA-28-235 · Rock Springs, WYThe pilot's inadvertent movement of the fuel selector valve beyond its tank detent, which resulted in a total loss of engine power due to fuel starvation. Contributing to the accident was the failure of the fuel selector interlock mechanism.NTSB CEN13CA139Accident · No injuriesData collectionFinal reportPiper PA-24-250 · Phillipsburg, OHThe pilot's improper operation of the airplane controls during engine start, which resulted in a collision with a hangar.NTSB ERA13LA112Accident · No injuriesLimited investigationFinal reportCessna T182 · Brandon, FLFailure of the No. 2 cylinder’s rod bearing, which resulted in a total loss of engine power.