NTSB investigations, 2013
128 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\") = 2013
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") = 2013 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 ERA14LA076Accident · Serious injuriesLimited investigationFinal reportCessna 210N · Tampa, FLA total loss of engine power due to the fatigue failure of the No. 4 connecting rod. Contributing to the accident was a likely loss of lubrication for reasons that could not be determined during a postaccident engine examination.NTSB CEN14WA093Accident · 4 fatalForeign investigationRobinson Helicopter R 44 · Bordeaux, FranceOn December 20, 2013, about 1715 central European time, a Robinson R44 helicopter, French registered F-GPJG, owned and piloted by the accident pilot, was destroyed when it impacted the Dordogne River under unknown circumstances near Bordeaux, France. Visual…NTSB ERA14LA072Accident · No injuriesLimited investigationFinal reportCessna 182T · Burlington, NCA loss of airplane control during takeoff for reasons that could not be determined due to the postaccident condition of the elevator control system.NTSB CEN14LA089Accident · Minor injuriesLimited investigationFinal reportCessna 305C (0 1E) · Hondo, TXThe pilot's loss of directional control during an attempted go-around for reasons that could not be determined based on the available evidence. Contributing to the accident was the flight instructor’s and pilot’s decision to continue flight after experiencing…NTSB WPR14LA061Accident · Minor injuriesLimited investigationFinal reportPiper PA 24-250 · Fair Oaks, CAThe loss of engine power during cruise flight for reasons that could not be determined because postaccident examinations of the airplane and engine did not reveal any anomalies that would have precluded normal operation.NTSB CEN14LA079Accident · Serious injuriesLimited investigationFinal reportThompson William A Sparrow II · Jeromesville, OHThe student pilot's in-flight loss of control while attempting to return to the runway following a loss of engine power. The cause of the loss of engine power could not be determined because the postaccident examination did not reveal any anomalies.NTSB CEN14LA075Accident · No injuriesLimited investigationFinal reportCessna 560 · Walton, INThe inflight separation of the upper and lower right engine cowlings for reasons that could not be determined based on available evidence.NTSB CEN14WA067Accident · 2 fatalForeign investigationRobinson R44 - II · Neuhausen ob Eck, GermanyOn November 19, 2013, at 1134 coordinated universal time, a Robinson R44 II, Germany-registered D-HOMI, was substantially damaged when it impacted forested terrain near Neuhausen ob Eck, Germany. Instrument meteorological conditions prevailed at the time of…NTSB CEN14FA057Accident · 2 fatalField investigationFinal reportCessna 152 · Spring, TXThe flight instructor's failure to maintain airspeed following a partial loss of engine power for reasons that could not be determined during postaccident examination, which resulted in an aerodynamic stall and subsequent loss of airplane control.NTSB ERA14LA043Accident · Serious injuriesLimited investigationFinal reportMaule M-5-180C · Marshfield, MAA partial loss of engine power for reasons that could not be determined in postaccident examinations because fire damage precluded testing of the fuel and several engine accessories.NTSB CEN14FA046Accident · 1 fatalField investigationFinal reportMitsubishi MU 2B-25 · Owasso, OKThe pilot's loss of airplane control during a known one-engine-inoperative condition. The reasons for the loss of control and engine shutdown could not be determined because the airplane was not equipped with a crash-resistant recorder and postaccident…NTSB WPR14LA045Accident · Minor injuriesLimited investigationFinal reportCessna Ector 305A · Mokuleia, HIA landing gear brake malfunction during the landing for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.NTSB ERA14LA034Accident · Minor injuriesLimited investigationFinal reportTeal Harry H Sonerai II Stretch · De Leon Springs, FLA total loss of engine power for reasons that could not be determined because postaccident examination of the airframe and engine revealed no evidence of preexisting mechanical anomalies or failures that would have precluded normal operation.NTSB CEN14FA034Accident · 3 fatalField investigationFinal reportPiper PA 23-250 · Caledonia, MNThe pilot's loss of control for reasons that could not be determined because the postaccident airplane examination did not reveal any anomalies that would have precluded normal operation.NTSB WPR14LA036Accident · No injuriesLimited investigationFinal reportCessna T210M · Scipio, UTA total loss of engine power during cruise flight for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.NTSB CEN14TA020Accident · Minor injuriesFinal reportBell OH-58A · Jefferson City, MOThe loss of engine power for reasons that could not be determined because postaccident examinations of the engine did not reveal any anomalies that would have precluded normal operation.NTSB CEN14LA021Accident · No injuriesLimited investigationFinal reportPohoski RV 4 · New Waverly, TXAn in-flight fire for reasons that could not be determined because the wreckage was consumed by fire.NTSB WPR14CA018Accident · No injuriesData collectionFinal reportPiper PA 28R-201 · Las Vegas, NVThe collapse of a main landing gear for reasons that could not be determined due to no postaccident examination of the airframe.NTSB ERA14LA018Accident · No injuriesLimited investigationFinal reportFuller Van L Sonex · Palatine, NYA total loss of engine power for reasons that could not be determined because a test run and partial teardown of the engine did not reveal any anomalies.NTSB WPR14CA013Accident · Serious injuriesData collectionFinal reportPiper PA 28-180 · Cody, WYA loss of engine power during climb to cruise for reasons that could not be determined due to no postaccident examination.NTSB ERA14LA050Accident · No injuriesLimited investigationFinal reportCessna 170 · Ridgely, MDA total loss of engine power for reasons that could not be determined based on the available evidence.NTSB CEN14LA003Accident · Serious injuriesLimited investigationFinal reportKenneth M Franz Ultra PUP · Belleville, TXThe pilot’s failure to maintain adequate airspeed and his exceedance of the airplane's critical angle-of-attack while turning back to the airport instead of landing straight ahead following a partial loss of engine power, which resulted in an aerodynamic…NTSB ERA14LA007Accident · 1 fatalLimited investigationFinal reportBritten-Norman BN-2A-8 · Culebra, PRThe pilot's failure to maintain airplane control for reasons that could not be determined because the wreckage was not recovered.NTSB WPR14CA006Accident · Minor injuriesData collectionFinal reportSiemens Rotorway Exec 162F · Nampa, IDA flight control malfunction during cruise flight for reasons that could not be determined. No follow-up examination was conducted due to a lapse in agency funding and subsequent government shutdown.NTSB ERA14LA008Accident · Minor injuriesLimited investigationFinal reportCessna 172 - F · Gainesville, FLA total loss of engine power for reasons that could not be determined because a postaccident engine examination and test run revealed no anomalies.NTSB WPR14CA004Accident · Minor injuriesData collectionFinal reportVenables Zenith CH701 · Snohomish, WAA jammed rudder control while maneuvering in the pattern for reasons that could not be determined. No follow-up examination was conducted due to a lapse in agency funding and subsequent government shutdown.NTSB ERA14LA035Accident · Serious injuriesLimited investigationFinal reportAirborne Edge Executive · Eustis, FLThe pilot's inadvertent stalling of the wing following a total loss of engine power for reasons that could not be determined during postaccident examinations, which resulted in a hard landing.NTSB ERA13LA437Accident · Serious injuriesLimited investigationFinal reportInnovator Technologies Mosquito XEL · Felda, FLThe pilot’s loss of helicopter control while hovering for reasons that could not be determined during postaccident examination of the helicopter, which was limited due to postcrash fire damage.NTSB CEN13LA571Accident · No injuriesLimited investigationFinal reportCessna 182J · Santa Teresa, NMA loss of engine power for reasons that could not be determined because no anomalies were found during the postaccident engine examination.NTSB ERA13FA432Accident · 1 fatalField investigationFinal reportLowerre Bruce T S 12-E · Pahokee, FLUndetermined because the wreckage was not recovered.NTSB CEN13LA561Accident · No injuriesLimited investigationFinal reportWeatherly 620 · Ulysses, KSAn in-flight fire and subsequent loss of engine power for reasons that could not be determined due to extensive fire damage to the airplane and its fuel and electrical systems.NTSB ERA13LA429Accident · No injuriesLimited investigationFinal reportDe Havilland DH 82A · Rhinebeck, NYThe total loss of engine power for reasons that could not be determined because postaccident examinations revealed no anomalies that would have precluded normal operation, which resulted in a forced landing into trees.NTSB CEN13LA552Accident · No injuriesLimited investigationFinal reportPiper PA 28-180 · Frankenmuth, MIAn intermittent loss of engine power for reasons that could not be determined because postaccident examinations revealed no anomalies that would have precluded normal operation.NTSB WPR13LA407Accident · No injuriesLimited investigationFinal reportMooney M20J · Lund, NVThe pilot’s failure to monitor the environment, which led to a collision with power lines during climbout. Contributing to the accident was the loss of engine power during low-altitude flight for reasons that could not be determined because postaccident…NTSB WPR13LA408Accident · No injuriesLimited investigationFinal reportCessna 182A · Casa Grande, AZA loss of engine power during final approach for reasons that could not be determined because postaccident examinations did not reveal any anomalies that would have precluded normal operation.NTSB WPR13FA405Accident · 2 fatalField investigationFinal reportKamtz RV-7A · Jackson Hole, WYA loss of engine power for reasons that could not be determined because postaccident examination revealed no mechanical malfunctions or failures that would have precluded normal operation. Also causal was the pilot’s failure to adequately compensate for the…NTSB ANC13FAMS2Accident · 1 fatalMissing aircraftFinal reportPiper PA-32-260 · Yakutat, AKUndetermined because the pilot and airplane were not found.NTSB WPR13FA399Accident · 1 fatalField investigationFinal reportTyler Ives SD-1 TG · Spanish Fork, UTThe pilot’s failure to maintain airplane control while performing prohibited aerobatic maneuvers and the deployment and separation of the ballistic parachute system from the airframe for reasons that could not be determined due to the severity of impact…NTSB DCA13FA148Accident · No injuriesField investigationFinal reportBeech 1900D · Telluride, COFailure of the left main landing gear actuator internal lock to engage in the locked position for undetermined reasons.NTSB WPR13LA392Accident · Minor injuriesLimited investigationFinal reportPiper PA-18-105 Special · Rancho Palos Verdes, CAA loss of engine power during cruise flight for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation.NTSB WPR13LA389Accident · Serious injuriesLimited investigationFinal reportChampion 8KCAB · Wahiawa, HIA total loss of engine power during cruise flight 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 CEN13LA514Accident · Minor injuriesLimited investigationFinal reportChallenger II · Emporia, KSThe right wing’s folding up in flight for reasons that could not be determined because an examination did not reveal any abnormalities with the airframe that would have precluded normal operation.NTSB CEN13FA509Accident · 1 fatalField investigationFinal reportCessna 421C · Paris, ILThe pilot's failure to abort the takeoff during the ground roll after detecting the airplane's degraded performance. Contributing to the accident was the pilot's decision to attempt a flight with a known problem with the left engine and the likely partial…NTSB WPR13LA384Accident · Serious injuriesLimited investigationFinal reportPiper PA 28 · Sacramento, CAA partial loss of engine power during initial climb for reasons that could not be determined because postaccident examination revealed no evidence of preimpact mechanical malfunction or failure that would have precluded normal operation.NTSB CEN13LA502Accident · Minor injuriesLimited investigationFinal reportAnderas Tiger Moth R80 · New Franken, WIThe 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 WPR13LA378Accident · No injuriesLimited investigationFinal reportCessna 172B · Sisters, ORA loss of engine power during cruise flight for reasons that could not be determined because the engine was not properly preserved to prevent corrosion after the wreckage was recovered from the lake.NTSB CEN13LA490Accident · No injuriesLimited investigationFinal reportTaylorcraft BC12-D1 · Eastport, MIA fuel leak in the engine compartment and subsequent fire, the source of which could not be determined because of extensive postaccident fire damage.NTSB CEN13LA484Accident · No injuriesLimited investigationFinal reportRockwell International S-2R · Larchwood, IAA complete loss of engine power during an agricultural application flight for reasons that could not be determined because postaccident examinations did not reveal any anomalies that would have precluded normal operation.NTSB ERA13LA360Accident · Minor injuriesLimited investigationFinal reportQuest Kodiak 100 · Westport, MAA failure to achieve a positive climb rate after takeoff for reasons that could not be determined because postaccident examination of the airframe and engine did not reveal any mechanical malfunctions or anomalies that would have precluded normal operation.NTSB CEN13FA476Accident · 2 fatalField investigationFinal reportBeechcraft F33A · Ennis, TXThe loss of engine power for reasons that could not be determined during postaccident examinations due to postcrash fire damage.