NTSB investigations: Lycoming I0360 SER A&C

15 cases on aircraft whose registry engine model is Lycoming I0360 SER A&C, where the defining event was Loss of engine power (total). 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

20092026
NTSB investigations: Lycoming I0360 SER A&C per year, 2009–2026: 15 cases
20091
20101
20113
20123
20133
20152
20171
20181

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 c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('41511')
      AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e.case_mkey = x.case_mkey AND e.aircrafts_position = x.position AND e.\"isDefiningEvent\" AND e.\"tier2Number\" = '341'))
  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.

NTSB WPR18LA181Accident · Minor injuriesClass 3 · LimitedFinal reportCessna 172S · Phoenix, AZA total loss of engine power due to crankshaft failure as the result of a subsurface fatigue crack.Jun 26, 2018 · N154ME · Substantial damageNTSB ANC18LA013Accident · No injuriesLimited investigationFinal reportCessna 172R · Huntingdon, TNA total loss of engine power for reasons that could not be determined because a postaccident engine examination and testing revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation.Dec 2, 2017 · N9730F · Substantial damageNTSB ERA15LA341Accident · Minor injuriesClass 2 · LimitedFinal reportPiper PA 28RT-201 · Russell Springs, KYMaintenance personnel’s inadequate fuel injection servo maintenance due to an out-of-date AD list, which resulted in the fuel injection servo plug backing out of the threaded plug hole on the regulator cover of the fuel injection servo and subsequent total…Sep 4, 2015 · N8162S · Substantial damageNTSB ERA15LA177Accident · No injuriesLimited investigationFinal reportMooney M20J · Allentown, PAA total loss of engine power during takeoff due to an interruption of fuel flow to the engine. The reason for the interruption of the fuel flow could not be determined during postaccident examination and testing.Apr 6, 2015 · N4826H · Substantial damageNTSB WPR13LA407Accident · No injuriesLimited investigationFinal reportMooney M20J · Lund, NVThe pilot’s failure to monitor the environment, which led to a collision with power lines during climbout. Contributing to the accident was the loss of engine power during low-altitude flight for reasons that could not be determined because postaccident…Sep 15, 2013 · N1079K · Substantial damageNTSB CEN13LA370Accident · No injuriesLimited investigationFinal reportMooney M20J · El Reno, OKA loss of engine power, which resulted from the failure of the magneto assembly for reasons that could not be determined during postaccident examinations.Jun 25, 2013 · N205MC · Substantial damageNTSB ERA13LA291Accident · No injuriesLimited investigationFinal reportCessna 172S · Clearwater, FLA total loss of engine power for reasons that could not be determined because neither postaccident visual examinations nor test runs of the engine revealed any anomalies that would have precluded normal operation.Jun 19, 2013 · N426SJ · Substantial damageNTSB ERA12LA422Accident · Serious injuriesLimited investigationFinal reportMooney M20J · Mc Kinnon, TNThe separation of the piston connecting rod from the crankshaft due to inadequate installation from a mechanic, resulting in a total loss of engine power.Jun 28, 2012 · N174JB · Substantial damageNTSB WPR12LA247Accident · No injuriesLimited investigationFinal reportPiper PA28R · Peoria, AZA loss of engine power for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.May 29, 2012 · N963WW · Substantial damageNTSB CEN12LA253Accident · Serious injuriesLimited investigationFinal reportBumford-Royer Christen Eagle II · Pearland, TXA loose B nut on the fuel inlet line due to maintenance personnel’s application of insufficient torque on the nut at an unknown time, which resulted in a fuel leak and a subsequent total loss of engine power during initial climb.Apr 22, 2012 · N80BH · Substantial damageNTSB CEN12LA076Accident · Minor injuriesLimited investigationFinal reportCirrus Design SR20 · New Orleans, LAA loss of engine power due to detonation of the No.2 cylinder from a clogged fuel injector nozzle.Nov 20, 2011 · N211CD · Substantial damageNTSB CEN11FA616Accident · 2 fatalField investigationFinal reportLarson Ken W Christen EAGLE-II · Seward, NEThe pilot’s inadvertent pulling of the mixture control lever on takeoff, which shut down the engine.Sep 4, 2011 · N88CE · Substantial damageNTSB WPR11FA403Accident · No injuriesField investigationFinal reportBeech A23-24 · Palo Alto, CAThe student’s and flight instructor’s mismanagement of the fuel supply, resulting in a total loss of engine power due to fuel starvation.Aug 23, 2011 · N5779V · Substantial damageNTSB ERA10LA486Accident · No injuriesLimited investigationFinal reportPiper PA-28R-200 · Barnwell, SCThe failure of the No. 1 connecting rod end cap for undetermined reasons, which resulted in a total loss of engine power.Sep 19, 2010 · N799SQ · Substantial damageNTSB ERA09LA494Accident · No injuriesLimited investigationFinal reportPiper PA-28R-201 · Luray, VAA total loss of engine power during initial climb for undetermined reasons.Aug 26, 2009 · N186CF · Substantial damage