NTSB investigations: Lycoming HIO-360 series, 2002
13 cases on aircraft whose registry engine model is Lycoming HIO-360 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 | 2 |
|---|---|
| 1965 | 1 |
| 1966 | 1 |
| 1967 | 2 |
| 1968 | 1 |
| 1969 | 2 |
| 1971 | 3 |
| 1972 | 2 |
| 1973 | 4 |
| 1974 | 3 |
| 1975 | 2 |
| 1976 | 5 |
| 1977 | 6 |
| 1978 | 6 |
| 1979 | 10 |
| 1980 | 12 |
| 1981 | 9 |
| 1982 | 6 |
| 1983 | 6 |
| 1984 | 3 |
| 1985 | 8 |
| 1986 | 9 |
| 1987 | 6 |
| 1988 | 10 |
| 1989 | 14 |
| 1990 | 5 |
| 1991 | 3 |
| 1992 | 3 |
| 1993 | 15 |
| 1994 | 10 |
| 1995 | 4 |
| 1996 | 6 |
| 1997 | 12 |
| 1998 | 14 |
| 1999 | 7 |
| 2000 | 12 |
| 2001 | 10 |
| 2002 | 13 |
| 2003 | 15 |
| 2004 | 8 |
| 2005 | 11 |
| 2006 | 9 |
| 2007 | 9 |
| 2008 | 7 |
| 2009 | 3 |
| 2010 | 5 |
| 2011 | 9 |
| 2012 | 9 |
| 2013 | 9 |
| 2014 | 3 |
| 2015 | 11 |
| 2016 | 6 |
| 2017 | 1 |
| 2018 | 5 |
| 2019 | 4 |
| 2020 | 4 |
| 2021 | 4 |
| 2022 | 3 |
| 2023 | 3 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 2 |
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\") = 2002
AND c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('41524'))
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") = 2002
AND c."mKey" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('41524'))
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 LAX03LA052Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Los Banos, CAThe improper engine overhaul by other maintenance personnel, which resulted in an exhaust valve failure and a total loss of engine power while in maneuvering flight.NTSB DEN03LA018Accident · Minor injuriesLimited investigationFinal reportEnstrom F-28C · Morrison, COthe pilot not maintaining clearance from the telephone lines during landing. Factors contributing to the accident were the pilot not being able to see the telephone lines, the low altitude, and the dark night.NTSB CHI02LA293Accident · No injuriesLimited investigationFinal reportHughes 269A · Council Bluffs, IAThe premature fracture of the cyclic/mixture bracket resulting in the inability to conduct a landing flare.NTSB DEN02LA098Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Broomfield, COmaintenance personnel's failure to secure the landing skid oleo strut bolt during the last 50-hour inspection, causing the left rear skid to collapse and the tail rotor to strike the ground.NTSB ATL02LA159Accident · Serious injuriesLimited investigationFinal reportSchweizer 300C · Haleyville, ALThe failure of maintenance personnel to perform an adequate inspection of loose intake components, which resulted in a total loss of engine power and subsequent emergency descent, forced landing, and collision with terrain in dark night conditions.NTSB SEA02LA150Accident · No injuriesLimited investigationFinal reportHughes 269A · Covington, WAAircraft control not maintained while hovering.NTSB ATL02LA141Accident · No injuriesLimited investigationFinal reportHughes HU-269-A · Hamilton, ALThe pilot's improper use of flight controls that resulted in an improper flare and a hard landing during a practice autorotation. A factor was the loss of rotor rpm.NTSB LAX02LA169Accident · Serious injuriesLimited investigationFinal reportEnstrom F-28C · Stockton, CAThe pilot's failure to maintain an adequate clearance from the water tower during takeoff. Also causal was the pilot's selection of a confined area for the landing and subsequent takeoff.NTSB LAX02LA161Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Phoenix, AZthe CFI's failure to maintain an adequate airspeed resulted in a settling with power, and the CFI's failure to take remedial action. A factor in the accident was the high density altitude.NTSB SEA02LA075Accident · No injuriesLimited investigationFinal reportEnstrom F-28C · Hot Springs, MTThe pilot's failure to adequately compensate for unfavorable wind conditions. Factors include unfavorable/shifting winds, and a tailwind gust.NTSB LAX02LA137Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Scottsdale, AZThe flight instructor's inadequate remedial action following the onset of ground resonance.NTSB FTW02LA104Accident · No injuriesLimited investigationFinal reportHughes 269A-1 · Fort Collins, COthe flight instructor's failure to maintain control of the helicopter while hovering. Contributing factors were the tailwind and gusty wind conditions.NTSB MIA02LA070Accident · No injuriesLimited investigationFinal reportHughes 269C · Bessemer, ALThe failure of the flight instructor to adequately monitor the student's rotorcraft control, resulting in an abrupt cyclic input causing a tail rotor strike of the terrain while entering a hover, and the resulting rollover during an uncontrolled descent.