NTSB investigations, 2012
229 cases where the sequence of events included Loss of engine power (total).
Cases per year
| 2008 | 255 |
|---|---|
| 2009 | 264 |
| 2010 | 259 |
| 2011 | 243 |
| 2012 | 229 |
| 2013 | 219 |
| 2014 | 206 |
| 2015 | 210 |
| 2016 | 196 |
| 2017 | 208 |
| 2018 | 204 |
| 2019 | 170 |
| 2020 | 142 |
| 2021 | 241 |
| 2022 | 152 |
| 2023 | 135 |
| 2024 | 145 |
| 2025 | 201 |
| 2026 | 146 |
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\") = 2012
AND c.\"mKey\" IN (SELECT s.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' s WHERE s.\"tier2Number\" = '341' AND s.case_mkey IN (SELECT case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' WHERE \"isDefiningEvent\"))
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") = 2012 AND c."mKey" IN (SELECT s.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' s WHERE s."tier2Number" = '341' AND s.case_mkey IN (SELECT case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' WHERE "isDefiningEvent")) 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 WPR13LA078Accident · No injuriesLimited investigationFinal reportCessna 210A · Chandler, AZA loss of engine power during takeoff climb for reasons that could not be determined because postaccident examination and testing of the engine revealed no mechanical malfunctions or failures that would have precluded normal operation.NTSB CEN13LA118Accident · No injuriesLimited investigationFinal reportPiper PA-24-250 · Mc Allen, TXA loss of engine power due to carburetor icing.NTSB CEN13LA119Accident · No injuriesLimited investigationFinal reportBell 407 · Big Lake, TXThe loss of engine power due to the fatigue failure of the outer combustion case at the fuel nozzle port. Contributing to the accident was the operator’s failure to conduct the recommended routine inspections of the outer combustion case.NTSB ERA13FA096Accident · 1 fatalField investigationFinal reportPiper PA-31-350 · Leesburg, FLThe pilot's inadequate preflight planning, which resulted in fuel exhaustion and a subsequent total loss of power in both engines during cruise flight. Contributing to the accident was the pilot’s use of prescription and illicit drugs, which likely impaired…NTSB ERA13LA099Accident · No injuriesLimited investigationFinal reportPiper PA-28RT-201T · Boca Raton, FLThe pilot's improper landing flare after a loss of engine power shortly after takeoff, which resulted in a hard landing. The reason for the loss of engine power could not be determined based on the available information.NTSB ERA13LA097Accident · Serious injuriesLimited investigationFinal reportPiper PA-28R-200 · Lock Haven, PAThe reinstallation of improper connecting rods at engine overhaul, which resulted in abnormal wear of the connecting rod bearings; while the bearings did not meet the manufacturer’s specifications, the use of the unapproved connecting rods more likely caused…NTSB CEN13LA110Accident · Minor injuriesLimited investigationFinal reportBeech 95-B55 (T42A) · Las Cruces, NMThe pilot's failure to properly manage the airplane's fuel, which resulted in engine failure due to fuel starvation.NTSB ERA13LA094Accident · No injuriesLimited investigationFinal reportWragg George Skybolt · Sarasota, FLThe pilot's inadequate preflight planning and failure to monitor the fuel quantity during flight, which resulted in a total loss of engine power due to fuel exhaustion.NTSB CEN13LA111Accident · No injuriesLimited investigationFinal reportPiper L-18C · Graham, TXThe failure of an engine connecting rod and the subsequent loss of oil pressure, which resulted in a total loss of engine power.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 ERA13LA084Accident · Minor injuriesLimited investigationFinal reportMerritt Leslie R Kelly D · Brandon, MSA total loss of engine power during takeoff for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.NTSB CEN13LA097Accident · Minor injuriesLimited investigationFinal reportNorth American T-28C · Moody, TXThe total loss of engine power for reasons that could not be determined because the examination of the engine did not reveal any anomalies that would have precluded normal operation.NTSB CEN13LA104Accident · No injuriesLimited investigationFinal reportCessna 172M · Arcola, TXThe loss of engine power during initial climb for reasons that could not be determined because postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation.NTSB CEN13LA099Accident · No injuriesLimited investigationFinal reportEnstrom F-28C · Abilene, TXThe flight instructor's failure to conduct an autorotation following the loss of engine power due to fuel exhaustion. Contributing to the accident was the failure of the flight instructor and the student pilot to visually check fuel levels to ensure adequate…NTSB CEN13LA091Accident · Minor injuriesLimited investigationFinal reportStinson 108-2 · Halfway, MOThe pilot's failure to properly maintain the airplane and engine, which resulted in a total loss of engine power due to improperly installed magnetos and a broken camshaft.NTSB ANC13LA012Accident · Minor injuriesLimited investigationFinal reportCessna 208B · Mekoryuk, AKThe total loss of engine power as a result of a fractured first-stage compressor blade due to fatigue cracking. The source of the fatigue crack could not be determined due to secondary damage sustained to the fracture surface.NTSB ERA13CA073Accident · No injuriesData collectionFinal reportBeech B19 · Fort Lauderdale, FLThe pilot's inadequate preflight planning, which resulted in fuel exhaustion and a total loss of engine power.NTSB CEN13FA080Accident · Minor injuriesField investigationFinal reportCessna 208B · Bryans Corner, OKThe total loss of engine power as a result of a fractured compressor turbine blade due to fatigue cracking.NTSB CEN13LA076Accident · No injuriesLimited investigationFinal reportCessna 177RG · Lansing, MIA loss of engine power due to the loss of fuel flow through the airplane's fuel tank selector valve.NTSB CEN13FA075Accident · 1 fatalField investigationFinal reportHughes 369 · Childress, TXThe improper maintenance of the helicopter fuel system that resulted in erroneous fuel gauge indications and the pilot’s inadequate fuel management, both of which resulted in fuel exhaustion during a long-line hover. Also causal was the lack of company…NTSB WPR13LA052Accident · Minor injuriesLimited investigationFinal reportCessna U206 · Van Nuys, CAA partial loss of engine power during cruise flight due to fatigue fractures of two crankshaft gear teeth from corrosion pitting, which resulted in an off-airport forced landing and collision with obstacles on the ground.NTSB CEN13LA072Accident · Serious injuriesLimited investigationFinal reportBeech S35 · DeRidder, LAA total loss of engine power due to oil starvation after the oil filler cap separated from the oil filler tube during flight due to corrosion. Contributing to the accident was the pilot's failure to maintain airspeed during low altitude operations, which…NTSB WPR13LA047Accident · No injuriesLimited investigationFinal reportCessna 210 · San Rafael, CAThe loss of engine power during initial climb for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.NTSB CEN13LA063Accident · 1 fatalLimited investigationFinal reportRedd Tom Quicksilver GT 400 · Oak Grove, LAThe total loss of engine power, the specific cause of which could not be identified during the postaccident examination, and the airplane’s subsequent impact with trees.NTSB ERA13LA060Accident · Minor injuriesLimited investigationFinal reportBeech 35B33 · White Plains, NYThe pilot's improper fuel management and his excessive slip maneuver, which led to fuel starvation and a total loss of engine power, and his failure to activate the electric boost pump during the attempted engine restart.NTSB WPR13LA043Accident · Minor injuriesLimited investigationFinal reportCirrus SR22 · Show Low, AZThe fatigue failure of an improperly installed nipple in the oil system of a supplemental type certificate-installed supercharger, which resulted in a complete loss of engine oil during cruise climb.NTSB ERA13LA053Accident · No injuriesLimited investigationFinal reportCessna 210 · Jasper, GAA loss of engine power due to fuel starvation as a result of the pilot’s prolonged sideslip maneuvers during the descent to landing. Contributing to the accident was the airplane’s lack of a required placard advising pilots to avoid lengthy sideslip maneuvers…NTSB CEN13LA056Accident · Minor injuriesLimited investigationFinal reportCessna 210L · La Grange, TXThe total loss of engine power due to the loss of oil to the engine. Contributing to the accident was maintenance personnel’s improper installation of the engine oil filter adaptor, which resulted in the loss of oil to the engine.NTSB CEN13LA054Accident · 1 fatalLimited investigationFinal reportCessna P210N · Conway, ARThe pilot's inadequate preflight inspection, which failed to detect the lack of fuel and resulted in fuel exhaustion during climb, and the pilot's subsequent failure to maintain airplane control, which resulted in an aerodynamic stall at low altitude from…NTSB CEN13FA049Accident · 1 fatalField investigationFinal reportCessna 208B · Wichita, KSThe total loss of engine power as a result of a fractured compressor turbine blade due to high-cycle fatigue.NTSB CEN13FA044Accident · 2 fatalField investigationFinal reportCessna 310 · Stotts City, MOThe pilot's failure to maintain airplane control after he shut down the right engine in flight due a loss of oil pressure. Contributing to the accident was the pilot's decision to reposition the unairworthy airplane during twilight after extensive maintenance…NTSB CEN13LA055Accident · Serious injuriesLimited investigationFinal reportCentral Ohio Dragonfly Club DRAGONFLY-C · Darbyville, OHThe total loss of engine power due to a cold-seizure event that occurred at a low altitude, which precluded the pilot's recovery from an inadvertent aerodynamic stall/spin.NTSB ANC13LA008Accident · No injuriesLimited investigationFinal reportBellanca 7ECA · Kenai, AKThe loss of engine power due to carburetor icing and the pilot's failure to apply carburetor heat when he reduced engine power.NTSB ERA13WA050Accident · Serious injuriesForeign investigationCessna 206 · Kiim, EcuadorOn October 31, 2012, about 1545 coordinated universal time (1045 local time), a Cessna 206, Ecuadorian registration HC-CBG, was substantially damaged during a forced landing in Kiim, Ecuador. The Ecuadorian commercial pilot was seriously injured. The airplane…NTSB ERA13LA029Accident · Minor injuriesLimited investigationFinal reportGrumman Acft ENG Cor-Schweizer G-164B · Edison, GAThe total loss of engine power due to the fatigue failure of the k-pin associated with the No. 1 cylinder.NTSB WPR13LA015Accident · No injuriesLimited investigationFinal reportBeech N35 · Phoenix, AZA loss of engine power due to oil starvation due to loose oil cooler attachment bolts. Contributing to the accident was inadequate maintenance during the annual inspection.NTSB CEN13LA015Accident · Serious injuriesLimited investigationFinal reportYoung Robert Herman Woody Pusher · Cloverdale, INThe total loss of engine power due to carburetor icing.NTSB WPR13LA011Accident · No injuriesLimited investigationFinal reportCirrus Design SR20 · Parker, AZThe pilot's failure to perform an adequate preflight inspection, which resulted in inadequate fuel for the flight and the subsequent fuel exhaustion and a total loss of engine power. Contributing to the accident was the pilot's failure to land the airplane at…NTSB WPR13LA009Accident · Minor injuriesLimited investigationFinal reportPiper PA-38-112 · Corona, CATotal loss of engine power during the landing approach due to insect debris in the carburetor metering valve, which resulted in fuel starvation.NTSB ERA13TA021Accident · Minor injuriesFinal reportBell OH-58A · Jackson, TNA loss of engine power for undetermined reasons because postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation.NTSB CEN13LA011Accident · No injuriesLimited investigationFinal reportMeyers Little Toot · Roanoke, TXThe total loss of engine power due to partially obstructed fuel lines.NTSB ERA13LA015Accident · Serious injuriesLimited investigationFinal reportVelline'S Breezy RLU-1 · Madison, GAThe pilot’s failure to maintain airspeed following a loss of engine power during takeoff for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation, and the airplane’s…NTSB WPR13LA005Accident · Minor injuriesLimited investigationFinal reportCessna 180H · St Maries, IDThe total loss of engine power for reasons that could not be determined because postaccident examination of the engine and airframe did not reveal any anomalies that would have precluded normal operation.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 ERA13CA011Accident · No injuriesData collectionFinal reportPiper PA-28-140 · Beltzville, PAThe flight instructor’s improper fuel management, which resulted in a loss of engine power due to fuel starvation.NTSB ERA13WA085Accident · No injuriesForeign investigationThrush S2R-T34 · Naranjal, EcuadorOn October 2, 2012, a Thrush S2R-T34, Ecuadorian registration HC-CFU, operated by a private owner, was substantially damaged following an engine failure and collision with terrain near Naranjal Province, Guayas, Ecuador. The flight's last departure point and…NTSB ERA12LA584Accident · 1 fatalLimited investigationFinal reportKeuthan Buccaneer II · Granite Quarry, NCThe pilot’s inadequate preflight fuel planning, which resulted in a total loss of engine power due to fuel exhaustion.NTSB CEN12LA667Accident · No injuriesLimited investigationFinal reportMcdonnell Douglas Heli 369FF · Decorah, IAThe pilot's failure to properly manage the helicopter's available fuel supply, which led to a total loss of engine power due to fuel exhaustion. Contributing to the accident was the improper calibration of the fuel gauge and the fuel-low warning light.NTSB WPR12LA439Accident · Minor injuriesLimited investigationFinal reportCessna 152 · Eugene, ORA total loss of engine power due to fuel exhaustion during cruise flight for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have resulted in the loss of engine power.NTSB CEN12LA675Accident · No injuriesLimited investigationFinal reportBeech E33 · Greeley, COThe loss of engine power for reasons that could not be determined during postaccident examinations and testing.