NTSB investigations, 2015
163 cases where NTSB found Not determined, general.
Cases per year
| 2008 | 150 |
|---|---|
| 2009 | 199 |
| 2010 | 195 |
| 2011 | 156 |
| 2012 | 171 |
| 2013 | 128 |
| 2014 | 150 |
| 2015 | 163 |
| 2016 | 137 |
| 2017 | 135 |
| 2018 | 143 |
| 2019 | 118 |
| 2020 | 86 |
| 2021 | 98 |
| 2022 | 76 |
| 2023 | 68 |
| 2024 | 37 |
| 2025 | 29 |
| 2026 | 9 |
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\") = 2015
AND c.\"mKey\" IN (SELECT f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f.\"findingCode\", '05000000'))
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") = 2015 AND c."mKey" IN (SELECT f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f."findingCode", '05000000')) 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 ANC16LA011Accident · 1 fatalLimited investigationFinal reportCessna 172 · Anchorage, AKThe pilot's intentional flight into a building.NTSB WPR16LA043Accident · Serious injuriesClass 3 · LimitedFinal reportAerostar Acft Corp Of Texas M20F · Nogales, AZThe airplane’s impact with a hillside shortly after takeoff for reasons that could not be determined.NTSB ERA16FA075Accident · 1 fatalField investigationFinal reportBeech C24R · Winder, GAA total loss of engine power for reasons that could not be determined because the examination of the wreckage did not reveal any mechanical anomalies that would have precluded normal operation.NTSB WPR16LA039Accident · No injuriesLimited investigationFinal reportMooney M20E · Corona, CAA partial loss of engine power during initial climb for reasons that could not be determined based on available information. Contributing to the accident was the pilot’s decision to conduct the takeoff with observed engine deficiencies.NTSB CEN16LA058Accident · Minor injuriesLimited investigationFinal reportMcdonnell Douglas Helicopter 600N · Angleton, TXA loss of control while hovering for reasons that could not be determined, because postaccident examination revealed no mechanical anomalies or failures that would have precluded normal operation.NTSB CEN16FA059Accident · 1 fatalField investigationFinal reportCessna 182C · Pattonsburg, MOThe pilot's loss of airplane control while maneuvering during low-level flight for reasons that could not be determined because examination of the airframe and engine did not reveal any preimpact anomalies.NTSB ERA16LA061Accident · Minor injuriesLimited investigationFinal reportPiper PA-24 · Millville, NJThe total loss of engine power during initial climb for reasons that could not be determined because postaccident examination of the engine revealed no anomalies that would have precluded normal operation.NTSB ERA16LA059Accident · No injuriesLimited investigationFinal reportPacific Aerospace 750XL · Raeford, NCThe pilot's failure to obtain the proper touchdown point and speed during a precautionary landing with the engine shut down. Contributing to the accident was an erroneous engine torque indication, which led the pilot to shut the engine down, for reasons that…NTSB ERA16LA054Accident · No injuriesLimited investigationFinal reportRobinson Helicopter R44 II · Destin, FLThe overstress fracture between the tail rotor driveshaft and intermediate flex plate for reasons that could not be determined based on the available evidence.NTSB ERA16LA046Accident · No injuriesLimited investigationFinal reportMooney M20 · Fort Meade, MDA partial loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no mechanical malfunctions or failures that would have precluded normal operation.NTSB ERA16LA045Accident · Serious injuriesLimited investigationFinal reportPhantom Aeronautics Phantom X 1 · Monroe, NCThe partial loss of engine power for reasons that could not be determined because postaccident examination of the engine did not reveal any preimpact anomalies that would have precluded normal operation.NTSB WPR16LA031Accident · No injuriesLimited investigationFinal reportCessna 210 · Coalinga, CAA partial loss of engine power during takeoff for reasons that could not be determined, because postaccident examination revealed no mechanical malfunctions or failures that would have precluded normal operation.NTSB WPR16LA030Accident · Serious injuriesLimited investigationFinal reportCessna T210N · La Verne, CAThe total loss of engine power for reasons that could not be determined based on the available information.NTSB ERA16FA044Accident · 2 fatalField investigationFinal reportBeech F33A · North Salem, NYA loss of airplane control for reasons that could not be determined because examination of the wreckage revealed no mechanical deficiencies.NTSB CEN16LA040Accident · Minor injuriesLimited investigationFinal reportRobinson Helicopter R22 Beta · Sugarland, TXThe overspeed of the main rotor system for reasons that could not be determined based on the available information.NTSB ERA16LA040Accident · No injuriesLimited investigationFinal reportCirrus Design SR22 · Jefferson, NCA total loss of engine power for reasons that could not be determined during a postaccident test run of the engine.NTSB CEN16FA037Accident · 1 fatalField investigationFinal reportCessna 182Q · Richmond, MOThe airplane's impact with trees and terrain during an off-airport forced landing in dark night conditions following a partial loss of engine power. The reason for the partial loss of engine power could not be determined because postaccident examination did…NTSB CEN16LA031Accident · Minor injuriesLimited investigationFinal reportAmerican Autogyro Sparrowhawk · Wakeman, OHA loss of engine power/performance for reasons that could not be determined because a postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.NTSB WPR16LA020Accident · Minor injuriesLimited investigationFinal reportBell 206B · Dallas, ORA loss of engine power for reasons that could not be determined based on the available information.NTSB ERA16LA030Accident · No injuriesLimited investigationFinal reportHughes 369D · Marion, SCA momentary jam in the tail rotor control system from an undetermined source, resulting in a torsional fracture of the tail rotor control torque tube and a loss of helicopter control.NTSB WPR16LA019Accident · No injuriesLimited investigationFinal reportAmerican Eurocopter AS350B3 · Folsom, CAThe flight instructor's failure to perform simulated engine failure training in accordance with manufacturer guidance, including his improper recovery from the maneuver, which resulted in an overshoot of the intended landing zone when the engine did not…NTSB CEN16LA021Accident · No injuriesLimited investigationFinal reportPiper PA 28-235 · Winneconne, WIAn engine compartment fire during landing, which resulted in extensive fire damage, for reasons that could not be determined during examinations of the remaining wreckage.NTSB ERA16LA058Accident · No injuriesLimited investigationFinal reportCessna R182 · Sanford, FLA collapse of the nose landing gear due to a separation of the drag attachment fitting from the airframe. The separation was likely due to preexisting damage from an undetermined event.NTSB WPR16LA011Accident · No injuriesLimited investigationFinal reportChristopher Tom Kitfox 5 · Battle Ground, WAThe total loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no preimpact mechanical malfunctions or failures that would have precluded normal operation.NTSB ERA16FA012Accident · 2 fatalField investigationFinal reportPiper PA 28-180 · Lake Worth, FLA loss of control for reasons that could not be determined based on the available information.NTSB ERA16LA009Accident · No injuriesLimited investigationFinal reportCessna 172N · Miami Beach, FLA total loss of engine power for reasons that could not be determined because the airplane was not recovered from the ocean after the ditching.NTSB CEN16LA019Accident · Serious injuriesLimited investigationFinal reportQuest Kodiak 100 · Sheridan, WYThe loss of airplane control during takeoff for reasons that could not be determined based on the available information.NTSB WPR16LA005Accident · Serious injuriesLimited investigationFinal reportPiper PA28 · Compton, CAA total loss of engine power during initial climb for reasons that could not be determined because postaccident engine examination did not reveal any anomalies that would have precluded normal operation.NTSB CEN16LA003Accident · Minor injuriesLimited investigationFinal reportBell 47G · Huntsville, TXThe pilot's loss of helicopter control during an agricultural application pass for reasons that could not be determined due to the extent of damage to the flight control system.NTSB WPR16LA003Accident · Serious injuriesLimited investigationFinal reportCessna TU206G · Fall City, WAThe airplane’s collision with the ground short of the runway for reasons that could not be determined based on the available evidence.NTSB ERA16FA001Accident · 4 fatalField investigationFinal reportPiper PA32R · Westminster, SCThe pilot's loss of airplane control for reasons that could not be determined based on the available information.NTSB CEN15FA426Accident · 1 fatalField investigationFinal reportJones Ralph D Zodiac CH 601 HD · Ama, LAThe pilot's failure to maintain adequate airspeed and his exceedance of the airplane's critical angle of attack following a loss of engine power for reasons that could not be determined based on available evidence, which resulted in an aerodynamic stall and…NTSB WPR15LA265Accident · Serious injuriesLimited investigationFinal reportAero Commander 680 E · Boise, IDThe pilot's failure to maintain airplane control following an engine problem for reasons that could not be determined because postaccident examination of both engines and the rudder revealed no malfunctions or anomalies that would have precluded normal…NTSB CEN15LA418Accident · Minor injuriesLimited investigationFinal reportCessna 421B · Platteville, WIThe partial loss of right engine power for undetermined reasons with insufficient runway remaining for the aborted takeoff.NTSB ERA15FA362Accident · 2 fatalField investigationFinal reportCessna 150H · Morrisville, NYThe pilot's failure to maintain airspeed and her exceedance of the airplane's critical angle-of-attack, which led to an aerodynamic stall, following a total loss of engine power for reasons that could not be determined because postaccident examination of the…NTSB CEN15LA444Accident · No injuriesLimited investigationFinal reportPiper PA 24-250 · New Orleans, LAThe collapse of the landing gear for reasons that could not be determined based on the available information.NTSB ANC15LA073Accident · No injuriesLimited investigationFinal reportRobinson Helicopter R44 · Fort Glenn, AKThe separation of the tail rotor gearbox from the tailboom attachment point due to overstress loads imposed by a tail rotor blade imbalance as the result of impact with an undetermined object during low-level flight operations.NTSB WPR15LA261Accident · Minor injuriesLimited investigationFinal reportSchweizer 269C · Forest Grove, ORA partial loss of engine power during cruise flight for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.NTSB GAA15LA281Accident · No injuriesLimited investigationFinal reportDehavilland DHC 2 MK.I · Nikolai, AKA loss of directional control during a water takeoff for reasons that could not be determined because the airplane was not examined due to the remote accident location.NTSB CEN15LA439Accident · No injuriesLimited investigationFinal reportRobinson Helicopter R44 II · Alice, TXA loss of engine power during a practice power recovery autorotation for reasons that could not be determined based on the available information.NTSB ANC15LA070Accident · No injuriesLimited investigationFinal reportHelio H 295 · Delta Junction, AKA partial loss of engine power during takeoff for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.NTSB ERA15FA353Accident · 1 fatalField investigationFinal reportAero Vodochody L39 · Oneida, TNThe pilot's failure to maintain airplane control following a partial loss of engine power during initial climb. The reason for the partial loss of engine power could not be determined due to extensive postimpact damage.NTSB CEN15LA412Accident · Minor injuriesLimited investigationFinal reportGuisinger Gary G Baby Belle · Stuart, IAThe failure of the tail rotor driveshaft for reasons that could not be determined due to the mechanically and thermally deformed fracture surface.NTSB ERA15FA351Accident · 1 fatalField investigationFinal reportCessna 172 · Riegelwood, NCThe noncertificated pilot’s failure to maintain adequate clearance from terrain for reasons that could not be determined based on the available evidence.NTSB ERA15LA343Accident · Serious injuriesLimited investigationFinal reportDehavilland DHC-6 · Louisburg, NCThe propeller’s movement to the beta position during landing for reasons that could not be determined during postaccident examination and testing, which resulted in an attempted go-around and subsequent loss of airplane control.NTSB CEN15LA404Accident · 1 fatalLimited investigationFinal reportCessna TR182 · Midland, TXThe partial loss of engine power for reasons that could not be determined based on the available evidence.NTSB WPR15LA257Accident · 1 fatalLimited investigationFinal reportHughes 369HS · Manra Island, KiribatiA The loss of helicopter control for reasons that could not be determined asbecause the helicopter sank in the oceanwater and was not recovered.NTSB WPR15LA254Accident · Minor injuriesLimited investigationFinal reportRaudenbush Ernie Lancair Super ES · Winkelman, AZA partial loss of engine power for reasons that could not be determined because postaccident examination of the engine revealed no anomalies.NTSB CEN15LA391Accident · Minor injuriesLimited investigationFinal reportFerence John W Thatcher CX4A · Hebron, OHThe loss of engine power for reasons that could not be determined because a postaccident examination of the airframe and engine did not reveal any anomalies that would have precluded normal operation.NTSB ERA15LA334Accident · Serious injuriesLimited investigationFinal reportBeech B19 · Dexter, METhe flight instructor’s inadequate preflight planning, which resulted in collision with trees and terrain during takeoff.