NTSB investigations, 2016
128 cases where NTSB found Aircraft power plant.
Cases per year
| 2008 | 197 |
|---|---|
| 2009 | 205 |
| 2010 | 190 |
| 2011 | 201 |
| 2012 | 165 |
| 2013 | 145 |
| 2014 | 130 |
| 2015 | 136 |
| 2016 | 128 |
| 2017 | 136 |
| 2018 | 134 |
| 2019 | 146 |
| 2020 | 119 |
| 2021 | 143 |
| 2022 | 164 |
| 2023 | 175 |
| 2024 | 161 |
| 2025 | 39 |
| 2026 | 8 |
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\") = 2016
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 year(c."eventDate") = 2016 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 ERA17LA077Accident · No injuriesLimited investigationFinal reportBeech 76 · Dunnellon, FLAn inadequate 100-hour maintenance inspection that failed to detect and correct loose nuts on a single-drive dual magneto, which led to the subsequent separation of the magneto from the engine during initial climb and the total loss of engine power.NTSB WPR17LA050Accident · No injuriesClass 3 · LimitedFinal reportDiamond Aircraft Ind DA 40 NG · Kingman, AZThe loss of engine oil pressure during cruise flight, which resulted in partial loss of engine power and necessitated a forced landing. The loss of oil pressure was the result of a failed engine piston, likely initiated by foreign object damage, which…NTSB WPR17LA042Accident · No injuriesLimited investigationFinal reportAir Tractor AT 602 · Willows, CAThe decision of the maintenance facility mechanic to conduct maintenance without reference to the applicable manufacturer’s guidance, which resulted in the improper reassembly and subsequent failure of the engine compressor bleed valve, which in turn…NTSB CEN17LA058Accident · No injuriesLimited investigationFinal reportBellanca 17 30A · Blaine, MNA total loss of engine power due to a lack of crankshaft lubrication to the No. 4 connecting rod journal.NTSB ERA17LA069Accident · No injuriesLimited investigationFinal reportBeech A36 · Shoreham, NYA fatigue crack of the crankshaft at the No. 4 main bearing journal.NTSB ERA17LA067Accident · Serious injuriesLimited investigationFinal reportMathias Linda B Lightning · Franklin, VAA partial loss of engine power due to pre-ignition damage to the No. 2 cylinder piston and the pilot's exceedance of the airplane's critical angle of attack while maneuvering in the airport traffic pattern, which resulted in an aerodynamic stall.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 ANC17LA008Accident · No injuriesLimited investigationFinal reportAirborne Extreme SQ-12 · Palmer, AKThe fuel injector manufacturer's inappropriate guidance to use a 5-ampere circuit breaker in place of the required 10-ampere circuit breaker on the fuel injector circuit, which resulted in the circuit breaker opening, a loss of electrical power to the…NTSB WPR17LA038Accident · No injuriesLimited investigationFinal reportCessna 182A · Safford, AZThe total loss of engine power due to the failure of the No. 5 piston, piston pin, or connecting rod assembly for reasons that could not be determined due to the severity of the post fracture damage.NTSB ANC17LA007Accident · No injuriesLimited investigationFinal reportPiper PA-18 · Bethel, AKThe mechanic's failure to install a whistle slot in the engine breather tube, which resulted in a frozen tube, displacement of the crankshaft oil seal, a loss of oil, and smoke in the cockpit, which led to a forced landing.NTSB WPR17FA024Accident · 4 fatalField investigationFinal reportPiper PA 31T · Elko, NVA loss of engine power to the left engine for reasons that could not be determined due to the extensive fire and impact damage to the airplane.NTSB ERA17LA044Accident · No injuriesLimited investigationFinal reportCessna 152 · Miami, FLThe loss of torque on the No. 3 connecting rod’s nuts, which resulted in the failure of the No. 3 connecting rod’s bolts and a subsequent total loss of engine power due to the operator's maintenance personnel’s improper installation of the connecting rod nuts.NTSB CEN17LA039Accident · Serious injuriesLimited investigationFinal reportCessna P210N · Pleasanton, TXMaintenance personnel's improper installation of the throttle linkage attachment hardware, which resulted in a partial loss of engine power when the hardware separated in flight.NTSB ANC17LA006Accident · Minor injuriesLimited investigationFinal reportPiper PA32R · Bethel, AKA total loss of engine power due to oil starvation, which resulted from an oil cooler leak at a fractured brazed seam.NTSB GAA17LA090Accident · No injuriesLimited investigationFinal reportPiper PA28R · Watertown, WIThe pilot’s failure to attain a proper glidepath on approach for landing, which resulted in impact with trees. Contributing to the accident was a partial, temporary loss of engine power for reasons that could not be determined because postaccident examination…NTSB ERA17LA037Accident · No injuriesLimited investigationFinal reportAviat A 1B · Geneva, FLA partial loss of engine power due to debris in the No. 1 cylinder that damaged the spark plugs.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 CEN17LA099Accident · No injuriesLimited investigationFinal reportRobinson R22 Beta · Asherton, TXThe partial loss of engine power due to the failure of the magneto's internal timing during low-altitude maneuvering.NTSB ENG17IA003Incident · No injuriesIncident investigationFinal reportAirbus A330 223 · Seattle, WAA No. 1 engine fire caused by a fuel manifold supply line high cycle fatigue crack which led to a fuel leak that subsequently ignited on hot engine case surfaces. The fatigue crack originated and progressed due to elevated fuel manifold assembly vibration…NTSB WPR17LA012Accident · Minor injuriesLimited investigationFinal reportNorthland IVP · Lovelock, NVA total loss of engine power due to the failure of the intake valve in the No. 3 cylinder for reasons that could not be determined based on the available information.NTSB GAA17CA039Accident · No injuriesData collectionFinal reportEvolution Revo · Carson City, NVThe pilot receiving instruction's inadvertent application of throttle during the engine start, which led to an inadvertent acceleration and a roll-over.NTSB CEN17LA021Accident · Serious injuriesLimited investigationFinal reportZenith CH-750 · Morristown, MNA total loss of engine power due to fuel vapor lock. Contributing to the loss of engine power were the corrosion of the spark plugs and the spacing of the electrode gaps.NTSB WPR17LA009Accident · No injuriesLimited investigationFinal reportGray Jim Robert Exec 90 · Caldwell, IDThe pilot's failure to properly tighten the tension bolts during the installation of the alternator belt, which resulted in inadequate voltage to sustain ignition and the subsequent partial loss of engine power.NTSB ERA17LA024Accident · Minor injuriesLimited investigationFinal reportCessna 172 · Cedar Key, FLA partial loss of engine power due to a stuck exhaust valve and the noncertificated pilot's inadequate preflight planning, which resulted in the airplane being overloaded, both of which led to the airplane's inability to attain a positive climb rate.…NTSB ERA17LA015Accident · Serious injuriesLimited investigationFinal reportCessna 150 · Stockbridge, GAA partial loss of engine power due to a stuck exhaust valve and the pilot's exceedance of the airplane’s critical angle of attack, which resulted in an aerodynamic stall.NTSB WPR17LA004Accident · Serious injuriesClass 3 · LimitedFinal reportRockwell International 112A · Phoenix, AZA catastrophic engine failure due to lack of lubrication due to the absence of 2 piston cooling nozzles that backed out of their respective threaded bores, which resulted in a forced landing on unsuitable terrain.NTSB ERA17LA019Accident · No injuriesLimited investigationFinal reportCessna 182 · Toone, TNA stuck No. 3 cylinder exhaust valve, which resulted in failure of the cylinder's valvetrain components, breach of the cylinder's rocker box cover, and partial loss of engine power due to oil starvation.NTSB CEN17LA014Accident · No injuriesLimited investigationFinal reportCessna 150M · Beasley, TXThe No. 2 cylinder exhaust valve being stuck in the “full open” position due to carbon deposits, which resulted in a total loss of engine power.NTSB CEN17LA015Accident · No injuriesLimited investigationFinal reportMilholland Kelly D · Livingston, TXA total loss of engine power for reasons that could not be determined based on the available information.NTSB CEN17LA006Accident · No injuriesLimited investigationFinal reportCessna 172K · Wilmot, WIA failure of the No. 1 piston pin plug due to corrosion in the cylinder barrel, which resulted in oil contamination, oil starvation to the crankshaft connecting rod bearings, and a subsequent partial loss of engine power.NTSB CEN17LA010Accident · Minor injuriesLimited investigationFinal reportPiper PA 28-180 · Clarendon, TXThe failure of a cylinder piston pin, which resulted in an obstructed oil inlet screen, reduced the amount of oil available to the engine, and led to the subsequent loss of engine power. Contributing to the accident was the failure of the nonmechanic, who had…NTSB ERA17LA026Accident · No injuriesClass 3 · LimitedFinal reportCessna 172 · Fort Lauderdale, FLThe pilot’s improper landing flare in gusting crosswind conditions, which resulted in a nose landing gear collapse.NTSB ERA17LA005Accident · No injuriesLimited investigationFinal reportPiper PA28 · Laurel, MSA total loss of engine power due to a stuck carburetor float. The reason the carburetor float became stuck could not be determined because postaccident examination of the float and needle/seat revealed no anomalies.NTSB CEN17LA009Accident · Minor injuriesLimited investigationFinal reportAero Smart Solutions Lancair Evolution · Iola, KSWater contamination of the fuel due to the pilot’s inadequate preflight inspection, which led to a total loss of engine power. Contributing to the accident was the pilot’s failure to complete the engine-out checklist, which resulted in an excessive loss of…NTSB ERA16LA331Accident · Minor injuriesLimited investigationFinal reportPiper PA32RT · Camden, SCA total loss of engine power due to the improper torqueing of the magneto, which led it to its malfunctioning in flight.NTSB CEN16LA391Accident · No injuriesLimited investigationFinal reportCessna 177RG · Cloquet, MNA lack of lubrication in the engine for reasons that could not be determined based on the available information, which resulted in a failure of the No. 4 connecting rod and a subsequent total loss of engine power.NTSB ERA16LA333Accident · No injuriesLimited investigationFinal reportRyan Navion · Hurt, VAIncorrect installation of the oil temperature probe and an inadequate annual inspection that failed to detect leaking oil around the loose probe, which resulted in a catastrophic engine failure due to oil starvation.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 ERA16LA319Accident · Minor injuriesClass 3 · LimitedFinal reportGrumman G164 · Chestertown, MDLoss of engine power due to a failure of the No. 3 cylinder head, which resulted in a forced landing and collision with ground equipment.NTSB WPR16LA184Accident · No injuriesLimited investigationFinal reportOGG Richard A OGG Glasair I · Reno, NVThe failure of an induction elbow following an engine backfire, which resulted in an in-flight fire and loss of engine power.NTSB ANC16FA065Accident · 1 fatalField investigationFinal reportHefty Polar Cub · Anchorage, AKThe pilot's severe impairment from carbon monoxide poisoning in flight, which resulted in a loss of control and a subsequent collision with trees and terrain.NTSB WPR16LA179Accident · No injuriesClass 3 · LimitedFinal reportMccluskey Challenger II · Bisbee, AZA total loss of engine power for reasons that could not be determined based on the available information.NTSB WPR16FA176Accident · Serious injuriesField investigationFinal reportCessna 310N · Wickenburg, AZTotal loss of power to the right engine during takeoff due to a fuel contaminant, which blocked the fuel flow transducer and resulted in fuel starvation to the engine.NTSB ERA16FA311Accident · 3 fatalField investigationFinal reportSikorsky S61 · Palm Bay, FLA dual loss of engine power for undetermined reasons after the pilot's improper decision to attempt another maneuver after recovering from a perceived compressor stall, rather than returning to the airport.NTSB GAA16CA465Accident · No injuriesData collectionFinal reportCessna TR182 · South Lake Tahoe, CAThe pilot's failure to maintain directional control during an attempted go-around, which resulted in a runway excursion and a nose over. Contributing to the accident was the pilot's failure to remove the carburetor heat during the attempted go-around in high…NTSB CEN16LA363Accident · Serious injuriesLimited investigationFinal reportCGS Hawk Aero II · Holland, MIThe improper installation of quick release connectors in the fuel lines, which was not in accordance with the engine manufacturer's maintenance instructions and allowed air to be introduced into the fuel system and resulted in a partial loss of engine power.…NTSB CEN16LA355Accident · Serious injuriesLimited investigationFinal reportRepublic RC3 · Post Oak, MOA partial loss of engine power due to low cylinder compression. Contributing to the loss of engine power was rust formation in the cylinders due to inactivity.NTSB DCA16FA217Accident · No injuriesField investigationFinal reportBoeing 737-700 · Pensacola, FLA low-cycle fatigue crack in the dovetail of fan blade No. 23, which resulted in the fan blade separating in flight and impacting the fan case. This impact caused the fan blade to fracture into fragments that traveled farther than expected into the inlet,…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 GAA16CA497Accident · No injuriesData collectionFinal reportCirrus Design SR20 · Brunswick, GAThe total loss of engine power during takeoff due to a loose B-nut on the fuel flow divider input fuel line fitting, which resulted in a fuel leak and fuel starvation.