NTSB investigations, IL
66 cases where NTSB found Aircraft power plant.
Cases per year
| 2008 | 5 |
|---|---|
| 2009 | 7 |
| 2010 | 6 |
| 2011 | 4 |
| 2012 | 6 |
| 2013 | 2 |
| 2014 | 5 |
| 2015 | 3 |
| 2016 | 7 |
| 2017 | 2 |
| 2018 | 3 |
| 2019 | 1 |
| 2020 | 3 |
| 2021 | 2 |
| 2022 | 3 |
| 2023 | 4 |
| 2024 | 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\", '0105'))
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", '0105')) 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 CEN25FA056Accident · Serious injuriesClass 3 · FieldFinal reportZenith Zodiac CH601 · Columbia, ILThe pilot’s failure to secure the engine oil filter following maintenance, which resulted in oil starvation, a total loss of engine power, and impact with terrain.NTSB CEN24LA203Accident · No injuriesClass 3 · LimitedFinal reportPulsar Super Pulsar · Rochelle, ILA partial loss of engine power for undetermined reasons.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 CEN23LA317Accident · No injuriesClass 3 · LimitedFinal reportGrumman G-164A · Patoka, ILA partial loss of engine power due to the failure of two compressor turbine blades as a result of the engine operating near or above the engine’s operating limits for an undetermined amount of time beyond the recommended engine’s TBO limit, which led to…NTSB CEN23LA145Accident · Serious injuriesClass 3 · LimitedFinal reportPiper PA32 · Lincoln, ILA total loss of engine power during an approach for landing for undetermined reasons.NTSB CEN23LA106Accident · No injuriesClass 3 · LimitedFinal reportJabiru USA Sport J250-SP · Cortland, ILA total loss of engine power for reasons that could not be determined.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 CEN22LA312Accident · No injuriesClass 3 · LimitedFinal reportAir Tractor AT-502B · Decatur, ILFracture of the compressor turbine (CT) blades due to creep.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 CEN18FA259Accident · Serious injuriesField investigationFinal reportEurocopter Deutschland EC135 P1 · Chicago, ILThe pilot's inadvertent disabling of the No. 1 and No. 2 engines' electronic engine control systems, which resulted in engine and rotor overspeed conditions, a subsequent autorotation, and a hard landing. Contributing to the accident were the pilot's…NTSB GAA18CA401Accident · No injuriesData collectionFinal reportGrumman G164 · Rochelle, ILThe pilot’s failure to move the power lever to the proper position before takeoff, which resulted in insufficient airspeed and a subsequent aerodynamic stall.NTSB CEN17LA309Accident · No injuriesClass 3 · LimitedFinal reportAir Tractor AT-802A · Galesburg, ILA total loss of engine power due to the fracture of a single 1st stage compressor rotor airfoil in high-cycle fatigue as a result of the erosion and thinning of the airfoil's leading edge. Contributing to the fractured airfoil and loss of engine power was the…NTSB ENG17IA028Incident · No injuriesIncident investigationFinal reportBombardier CL 600 2C10 · Chicago, ILA Bombardier CRJ700 No. 1 engine failure caused by buckling of the combustion outer liner due to fatigue cracks. The liner buckling resulted in airflow disruption and reduced engine performance. The engine fuel control unit attempted to compensate for the…NTSB ENG17IA006Incident · No injuriesIncident investigationFinal reportBombardier CL 600 2C10 · Kansas, ILThe probable cause of the uncontained No. 1 (left) engine failure was a separated high pressure turbine 2nd stage blade that failed due to a fatigue crack that originated below the blade platform from an area of corrosion.NTSB DCA17FA021Accident · Serious injuriesClass 1 · FieldFinal reportBoeing 767 · Chicago, ILThe failure of the high-pressure turbine (HPT) stage 2 disk, which severed the main engine fuel feed line and breached the right main wing fuel tank, releasing fuel that resulted in a fire on the right side of the airplane during the takeoff roll. The HPT…NTSB CEN16LA387Accident · Minor injuriesLimited investigationFinal reportPahnke Vernon A Vans RV 9A · Newark, ILThe pilot's failure to properly assemble the fuel pump, which resulted in the loss of fuel pressure and the subsequent partial loss of engine power.NTSB CEN16LA335Accident · Serious injuriesLimited investigationFinal reportCessna U206G · Cave-In-Rock, ILA total loss of engine power due to air entering the fuel system for reasons that could not be determined based on available information. Contributing to the accident was the pilot’s inability to restart the engine due to the check valve assembly design.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 CEN15LA414Accident · Minor injuriesLimited investigationFinal reportCessna 172P · Nutwood, ILA partial loss of engine power due to the undetected loosening of the four carburetor bolts that connect the throttle body to the bowl assembly.NTSB CEN15LA402Accident · Serious injuriesLimited investigationFinal reportViking Dragonfly · Freeport, ILThe airplane’s degraded climb performance due to its being over its maximum gross weight and a hole in the engine exhaust.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 CEN15LA028Accident · 1 fatalLimited investigationFinal reportHuebbe Sonex HB · Plainview, ILThe loss of engine power during cruise flight due to a fatigue fracture of the crankshaft, which resulted in a forced landing on unsuitable terrain.NTSB CEN15CA033Accident · No injuriesData collectionFinal reportPiper PA-23-250 · Quincy, ILThe pilot's improper fuel management, which resulted in the total loss of power to both engines due to fuel exhaustion and the subsequent forced landing in a field. Also causal to the accident was the pilot's decision to use the slower emergency hand-pump to…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 CEN14LA196Accident · No injuriesLimited investigationFinal reportPiper PA 46-350P · West Chicago, ILThe failure of the nose gear actuator attachment to the engine mount due to overstress, which resulted in the loss of directional control during landing.NTSB CEN14LA134Accident · No injuriesLimited investigationFinal reportCessna 172K · Milan, ILThe pilot’s delayed use of carburetor heat while operating the airplane in atmospheric conditions conducive to carburetor icing, which resulted in a total loss of engine power due to carburetor icing during a short final approach.NTSB CEN13LA473Accident · No injuriesLimited investigationFinal reportAir Tractor AT-502B · Nauvoo, ILA fatigue failure of an engine compressor turbine blade, which resulted in extensive secondary engine damage and a complete loss of engine power.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 CEN13IA008Incident · No injuriesIncident investigationFinal reportMueller Michael Walter Challenger II CW SPC · Sandwich, ILA total loss of engine power due to significant engine corrosion. Contributing to the accident was inadequate engine maintenance.NTSB CEN12LA577Accident · No injuriesLimited investigationFinal reportJones Kitfox III · Rockford, ILThe pilot's improper installation of a spark plug, which led to a partial loss of engine power after takeoff and the resultant forced landing.NTSB CEN12LA470Accident · Minor injuriesLimited investigationFinal reportYamokoski William Glastar · Chicago, ILFailure of the automotive engine's reduction gearbox while in cruise flight.NTSB CEN12LA455Accident · No injuriesLimited investigationFinal reportCessna 175A · Shelby, ILThe loss of engine power due to oil starvation for reasons that could not be determined because engine examinations revealed no malfunctions or failures that would have led to oil starvation.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 DCA11IA047Incident · No injuriesIncident investigationFinal reportBoeing 737-7Q8 · Chicago, ILThe flight crew's delayed deployment of the speedbrakes and thrust reversers, resulting in insufficient runway remaining to bring the airplane to a stop. Contributing to the delay in deployment of these stopping devices was the flight crew's inadequate…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.