NTSB investigations, IL
31 cases where NTSB found Engine (reciprocating).
Cases per year
| 2008 | 2 |
|---|---|
| 2009 | 3 |
| 2010 | 3 |
| 2011 | 3 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 1 |
| 2016 | 3 |
| 2018 | 1 |
| 2019 | 1 |
| 2020 | 3 |
| 2021 | 2 |
| 2022 | 2 |
| 2023 | 2 |
| 2025 | 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\" = 'IL' 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" = 'IL' 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 CEN25LA322Accident · No injuriesClass 3 · LimitedFinal reportPiper PA-18-150 · Joliet, ILThe failure of the No. 2 cylinder exhaust valve, which resulted in a total loss of engine power.NTSB CEN23LA372Accident · No injuriesClass 3 · LimitedFinal reportPietenpol Aircamper · Hanover, ILThe pilot’s exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall during an attempted forced landing at low altitude. Contributing to the accident was the loss of engine power for undetermined reasons.NTSB CEN23LA145Accident · Serious injuriesClass 3 · LimitedFinal reportPiper PA32 · Lincoln, ILA total loss of engine power during an approach for landing for undetermined reasons.NTSB CEN22LA377Accident · No injuriesClass 3 · LimitedFinal reportPiper PA-28-140 · Vernon Hills, ILThe pilot’s improper in-flight fuel management, which led to a loss of engine power due to fuel starvation. Contributing to the accident was the collapsed carburetor heat induction tube that restricted airflow to the engine preventing engine restart.NTSB CEN22LA128Accident · No injuriesClass 3 · LimitedFinal reportRyan L17 · Livingston, ILA total loss of engine power due to fuel injection system contamination from an unknown source.NTSB CEN21LA402Accident · No injuriesClass 3 · LimitedFinal reportMurphy Renegade II · Sheridan, ILA total loss of engine power during initial climb due to a piston seizure.NTSB CEN21LA221Accident · No injuriesClass 3 · LimitedFinal reportBeech A36 · Pinckneyville, ILThe total loss of engine power due to oil starvation. The reason for the oil starvation could not be determined based on available evidence.NTSB CEN21LA100Accident · Serious injuriesClass 3 · LimitedFinal reportWalton Daniel J Sonex · Pecatonica, ILA total loss of engine power for reasons that could not be determined based on the available information, and the pilot’s exceedance of the airplane’s critical angle of attack following the loss of engine power, which resulted in an aerodynamic stall/spin and…NTSB CEN21FA024Accident · 1 fatalClass 3 · FieldFinal reportGlasair III · Ford Heights, ILThe loss of engine power for reasons that could not be determined based on the available evidence.NTSB CEN20LA219Accident · 1 fatalClass 3 · LimitedFinal reportFlight Design Ctls · Beecher, ILThe pilot’s decision to continue takeoff after a partial loss of engine power, and the pilot’s subsequent failure to control airplane pitch during a forced landing. Contributing to the accident was the partial loss of engine power for reasons that could not…NTSB CEN19LA098Accident · Serious injuriesClass 3 · LimitedFinal reportPiper PA32R · Waterloo, ILThe loss of engine power due to a connecting rod failure for reasons that could not be determined due to secondary mechanical damage, which resulted in a subsequent forced landing.NTSB CEN18LA299Accident · Serious injuriesLimited investigationFinal reportPiper PA28 · Columbia, ILThe airplane's inability to climb due to reduced engine power as a result of insufficient compression in all cylinders and fouled spark plugs in the No. 2 cylinder while operating near its maximum gross weight.NTSB CEN16LA297Accident · No injuriesLimited investigationFinal reportCessna 172F · Newark, ILThe failure of the No. 4 cylinder exhaust valve, which resulted in a partial loss of engine power and a forced landing. Contributing to the valve failure and loss of engine power was the extended time since the last overhaul.NTSB CEN16LA218Accident · No injuriesLimited investigationFinal reportAeronca 7AC · East St. Louis, ILA total loss of engine power due to fracture of the piston pin, which led to fatigue cracking and eventual fracture of the adjacent connecting rod.NTSB CEN16LA166Accident · Minor injuriesLimited investigationFinal reportCessna 172 · Brimfield, ILA loss of engine power for reasons that could not be determined, as postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation.NTSB CEN15CA274Accident · No injuriesData collectionFinal reportEnstrom F 28C · Romeoville, ILThe certified flight instructor (CFI) did not maintain directional control during a downwind emergency running landing to soft muddy terrain, which resulted in a dynamic rollover. Contributing to the accident was the CFI's delayed or insufficient remedial…NTSB CEN14LA309Accident · No injuriesLimited investigationFinal reportSchumacher Challenger II · St. Joesph, ILThe total loss of engine power due to a lack of lubrication following the in-flight failure of the mechanical oil injection pump. Contributing to the accident was the temporary obscuration of the pilot's forward visibility due to sun glare during the forced…NTSB CEN13LA204Accident · No injuriesLimited investigationFinal reportBeech A36 · Cordova, ILA partial loss of engine power for reasons that could not be determined because a postaccident test run of the engine revealed no mechanical failures or malfunctions that would have precluded normal operation.NTSB CEN13LA103Accident · Serious injuriesLimited investigationFinal reportAuman JL T-51 · Dekalb, ILThe improper engine overhaul by the airplane kit manufacturer, which resulted in a catastrophic engine failure.NTSB CEN12LA309Accident · Minor injuriesLimited investigationFinal reportQuicksilver Sprint II · Lebanon, ILThe total loss of engine power due to a fatigue failure of the crankshaft, attributed to the relative movement between the crankshaft and flywheel assembly.NTSB CEN11LA618Accident · No injuriesLimited investigationFinal reportVicari Waiex · Marion, ILThe partial loss of engine power during initial climb for undetermined reasons.NTSB CEN11LA413Accident · No injuriesLimited investigationFinal reportCessna 172N · Bedford Park, ILA loss of engine power due to a fractured push rod precipitated by a stuck exhaust valve.NTSB CEN11FA227Accident · No injuriesField investigationFinal reportLancair LC41-550FG · Carbondale, ILThe fatigue fracture and subsequent failure of the No. 2 cylinder exhaust valve during cruise flight, which resulted in a total loss of engine power.NTSB CEN11FA125Accident · 1 fatalField investigationFinal reportBeech C24R · Wheeling, ILThe installation of the wrong engine-driven fuel pump, which resulted in a loss of engine power during takeoff, and the pilot's subsequent decision to turn back toward the airport at an insufficient altitude to complete the maneuver. Contributing to the…NTSB CEN11LA049Accident · 1 fatalLimited investigationFinal reportLuscombe 8A · Schaumburg, ILThe pilot did not maintain airspeed following a loss of engine power during takeoff climb, which resulted in an aerodynamic stall. Contributing to the accident was the loss of engine power due to the unlocked engine primer.NTSB CEN10LA420Accident · No injuriesLimited investigationFinal reportAir Tractor AT-401 · Toulin, ILA partial loss of engine power as a result of a cracked cylinder and the reduced visibility due to the oil-covered windshield.NTSB CEN10LA023Accident · No injuriesLimited investigationFinal reportPiper PA-32-260 · Peoria, ILA loss of engine power for undetermined reasons during climb out after takeoff, which resulted in a forced landing to a roadway.NTSB CEN09LA494Accident · No injuriesLimited investigationFinal reportCrisman Flightstar Iisc · Malta, ILThe loss of engine power due to the separation of the flywheel, resulting in a high-cycle fatigue fracture of the crankshaft following takeoff, which resulted in a forced landing on an agricultural field.NTSB CEN09IA172Incident · No injuriesIncident investigationFinal reportCessna 150 · Grayslake, ILThe failure of the number 1 cylinder intake valve which resulted in a partial loss of engine power. Contributing to the incident was the failure of the operator to maintain the engine per manufacturer's recommendations.NTSB CHI08LA171Accident · Minor injuriesLimited investigationFinal reportPiper PA-28R-200 · Watseka, ILThe loss of engine power for undetermined reasons.NTSB CHI08CA112Accident · No injuriesData collectionFinal reportPierson RV-6 · Newark, ILThe partial loss of engine power due to the fracture of the number 4 exhaust valve, and the pilot's decision to shut-down the engine without sufficient altitude to ensure a safe glide path to the runway. Contributing to the accident was the barbed wire fence…