NTSB investigations, 2013
62 cases where the defining event was Loss of engine power (partial).
Cases per year
| 2008 | 75 |
|---|---|
| 2009 | 75 |
| 2010 | 78 |
| 2011 | 88 |
| 2012 | 95 |
| 2013 | 62 |
| 2014 | 88 |
| 2015 | 89 |
| 2016 | 82 |
| 2017 | 66 |
| 2018 | 77 |
| 2019 | 81 |
| 2020 | 58 |
| 2021 | 78 |
| 2022 | 53 |
| 2023 | 64 |
| 2024 | 69 |
| 2025 | 80 |
| 2026 | 61 |
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 e.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e.\"isDefiningEvent\" AND e.\"tier2Number\" = '342')
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 e.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e."isDefiningEvent" AND e."tier2Number" = '342') 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 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 CEN14LA058Accident · Serious injuriesLimited investigationFinal reportPiper PA 28-140 · San Antonio, TXA partial loss of engine power after departure due to the collapse of the carburetor air inlet duct, which restricted the airflow to the engine. Contributing to the accident was the overdue annual inspection and the installation of the improper air inlet duct.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 WPR14LA046Accident · No injuriesLimited investigationFinal reportRovey Jason H RV-8 · Wickenburg, AZThe fatigue failure of a propeller pitch change pin due to excessive shot peening of the pin’s surface during the manufacturing process.NTSB WPR14CA035Accident · No injuriesData collectionFinal reportPiper PA 18-150 · Twin Falls, IDThe pilot's loss of aircraft control during the rejected takeoff.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 WPR14LA023Accident · Minor injuriesLimited investigationFinal reportCessna 172 - M · Hardin, MTA rough-running engine and partial loss of power, which resulted from the pilot’s failure to use carburetor heat appropriately while operating in an area conducive to carburetor icing.NTSB CEN13CA543Accident · Serious injuriesData collectionFinal reportTaylorcraft BL 65 · Chippewa Falls, WIThe loss of engine power after takeoff due to carburetor icing.NTSB WPR13LA390Accident · Serious injuriesLimited investigationFinal reportBell Helicopter Textron 206L-1 · Payson, AZA partial loss of engine power due to an overtemperature event that thermally damaged the turbine blades and vanes, which resulted in a hard landing.NTSB ERA13CA375Accident · Minor injuriesData collectionFinal reportMark C Pauls RV-7A · Cortland, NYA partial loss of engine power during go-around due to incorrect maintenance of the fuel system by the pilot/builder.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 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.NTSB WPR13LA366Accident · No injuriesLimited investigationFinal reportPiper PA-28-180 · Overgaard, AZThe partial loss of engine power during takeoff due to the separation of the exhaust baffling, which resulted in a partial blockage of airflow. Contributing to the accident was inadequate maintenance of the exhaust system.NTSB CEN13WA576Accident · No injuriesForeign investigationSocata TB10 - NO Series · Zamora, SpainOn August 9, 2013, about 0930 UTC, a Socata TB-10 airplane, EC-FPN, (s/n 1485) was involved in a forced landing following an engine failure. The airplane was substantially damaged and there were no injuries. This investigation is under the jurisdiction and…NTSB ERA13LA342Accident · Minor injuriesLimited investigationFinal reportMooney M20J · Leonardtown, MDThe improper installation and inspection of the throttle linkage by maintenance personnel, which resulted in the throttle linkage coming loose and a subsequent partial loss of engine power.NTSB CEN13LA443Accident · No injuriesLimited investigationFinal reportGrumman G-164A · Monte Vista, COThe partial loss of engine power due to a fatigue failure of the engine cylinder exhaust rocker housing as a result of an excessively torqued rocker assembly.NTSB WPR13LA346Accident · Minor injuriesLimited investigationFinal reportBeech 35-B33 · Lone Pine, CAA partial loss of engine power after takeoff for reasons that could not be determined because postaccident examination did not reveal any anomalies that would have precluded normal operation. Contributing to the accident was the pilot's decision to not…NTSB ANC13LA068Accident · Serious injuriesLimited investigationFinal reportDehavilland Beaver DHC 2 · Thorne Bay, AKThe failure of the No. 1 linkrod bushing or the bottom portion of the linkrod, which resulted in a total loss of engine power.NTSB WPR13LA320Accident · No injuriesLimited investigationFinal reportStinson 108-3 · Blackfoot, IDA partial loss of engine power during cruise flight for reasons that could not be determined because postaccident examination revealed no mechanical malfunctions or failures that would have precluded normal operation.NTSB ANC13CA062Accident · No injuriesData collectionFinal reportAeronca 11AC · Kodiak, AKThe loss of engine power due to carburetor icing and the pilot's failure to continue the use of carburetor heat after experiencing carburetor ice.NTSB CEN13LA383Accident · Serious injuriesLimited investigationFinal reportVink Robert D Youngster · Grand Haven, MIThe loss of engine power due to carburetor icing.NTSB WPR13LA318Accident · Serious injuriesLimited investigationFinal reportChicco Quicksilver Sport II · Newbury Park, CAThe partial loss of engine power while maneuvering due to the blockage of the exhaust system by broken internal engine baffles that had shifted during the flight, which resulted in a forced landing and subsequent impact with terrain.NTSB ANC13LA059Accident · No injuriesLimited investigationFinal reportCessna 175 · Skwentna, AKThe partial loss of engine power for reasons that could not be determined because the postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation. .NTSB WPR13FA289Accident · 1 fatalField investigationFinal reportCessna P337H · San Luis Obispo, CALoss of engine power from the rear engine for reasons that could not be determined because of the postimpact thermal damage to the engine. Contributing to the accident were the pilot's decision to continue flight with a known deficiency, his failure to abort…NTSB ERA13LA300Accident · Minor injuriesLimited investigationFinal reportSikorsky 269C · Lumberton, NJThe pilot's movement of the throttle to the idle detent at the beginning of a practice autorotation, which was contrary to procedures and resulted in the engine hesitating during the power recovery and a subsequent hard landing.NTSB CEN13LA359Accident · No injuriesLimited investigationFinal reportBell 206 - L4 · Lake City, ARA partial loss of engine power 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 CEN13LA390Accident · No injuriesLimited investigationFinal reportRockwell S-2R · Boise City, OKThe total loss of engine power for reasons that could not be determined because postaccident examination of the engine and fuel system revealed no anomalies.NTSB CEN13LA341Accident · No injuriesLimited investigationFinal reportAir Tractor AT-301 · Farnsworth, TXThe partial loss of engine power for reasons that could not be determined because the postaccident engine examination revealed no anomalies.NTSB CEN13LA325Accident · Minor injuriesLimited investigationFinal reportRobinson Helicopter R22 Beta · New Braunfels, TXThe pilot's improper flare during an autorotation, which resulted in a hard landing, and a partial 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…NTSB ERA13LA269Accident · Minor injuriesLimited investigationFinal reportStinson 108 · Elkton, KYThe pilot's failure to use carburetor heat during the approach to landing, which resulted in carburetor icing and a partial loss of engine power during a subsequent initial climb.NTSB ERA13LA263Accident · 1 fatalLimited investigationFinal reportWilson William M Cricket MC12 · Doylestown, PAThe pilot's failure to abort the takeoff after detecting the airplane’s degraded performance. Contributing to the accident were the likely loss of power from the left engine for reasons that could not be determined during the postaccident examination of the…NTSB WPR13CA252Accident · Minor injuriesData collectionFinal reportCessna 172A · Eatonville, WAA partial loss of engine power due to carburetor icing and the pilot's failure to maintain adequate airspeed during a go-around, which resulted in a stall.NTSB ERA13LA257Accident · No injuriesLimited investigationFinal reportCessna 180J · Greenwood, MSA partial loss of engine power due to carburetor icing.NTSB CEN13LA305Accident · Minor injuriesLimited investigationFinal reportStinson 108-3 · Beaumont, TXThe lack of a forward clamp on the carburetor heat box rubber boot, which allowed the boot to be ingested into the inlet of the carburetor heat box, restricting the airflow and leading to a subsequent partial loss of engine power.NTSB CEN13LA287Accident · Minor injuriesLimited investigationFinal reportPiper PA-28-161 · Oskaloosa, IAThe loss of engine power for reasons that could not be determined because the engine examination did not reveal any malfunctions or failures that would have precluded normal operation.NTSB WPR13LA230Accident · No injuriesLimited investigationFinal reportCessna T188C · Pine Bluffs, WYThe 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 ERA13LA241Accident · No injuriesLimited investigationFinal reportCessna 182E · Southwick, MAThe partial loss of engine power for reasons that could not be determined because postaccident examination of the engine did not reveal any malfunctions or failures that would have precluded normal operation.NTSB CEN13LA304Accident · Minor injuriesLimited investigationFinal reportAnkestar, Bradley D. RAND-ROBINSON KR2 · Hamilton, OHThe loss of engine power due to vapor lock in the fuel system. Contributing to the accident was the operation of the airplane with automotive gasoline and the installation of noninsulated fuel components near heat sources in the engine compartment.NTSB ANC13CA044Accident · No injuriesData collectionFinal reportPiper PA-18-150 · Palmer, AKThe pilot's failure to use continuous carburetor heat while operating in conditions conducive to carburetor icing, which resulted in the development of carburetor ice and a subsequent partial loss of engine power.NTSB WPR13LA216Accident · Minor injuriesLimited investigationFinal reportRans S-17 · Fontana, CAA loss of engine power due to improper construction and inadequate maintenance of the fuel system and engine. Contributing to the accident was the airplane’s inadvertent contact with an unseen guy wire during the landing flare.NTSB WPR13LA224Accident · No injuriesLimited investigationFinal reportCessna 172M · Lakeport, CALoss of engine power during climb due to a failure of the No. 2 piston assembly; the reason for the failure could not be determined because of the extent of damage to the piston assembly.NTSB ERA13FA217Accident · Minor injuriesField investigationFinal reportCessna 172N · Dade City, FLThe in-flight loosening of the No. 3 cylinder exhaust valve rocker arm stud, which resulted in a complete loss of engine power.NTSB CEN13LA245Accident · No injuriesLimited investigationFinal reportRaytheon G36 · Hoxie, KSThe loss of engine power due to fuel starvation 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 ERA13LA214Accident · Serious injuriesLimited investigationFinal reportBeech 35-C33A · Knoxville, TNThe loss of engine power during takeoff for a reasons that could not be determined because postaccident examinations and testing revealed no anomalies that would have precluded normal operation.NTSB ERA13LA211Accident · Serious injuriesLimited investigationFinal reportPiper PA-18-135 · Inlet, NYA loss of engine power for reasons that could not be determined during postaccident examination.NTSB CEN13LA232Accident · No injuriesLimited investigationFinal reportCessna 172G · Reading, MIThe partial loss of engine power due to the improper securing of the throttle linkage by maintenance personnel.NTSB ERA13WA203Accident · 2 fatalClass 5 · ForeignPiper PA-23-250 · Georgetown, GuyanaOn April 13, 2013, about 1854 coordinated universal time, a Piper PA-23-250, N27FT, was destroyed when it impacted a residence shortly after departing from Ogle International Airport (SYGO), Georgetown, Guyana. The certificated airline transport pilot and one…NTSB ERA13LA187Accident · No injuriesLimited investigationFinal reportCessna 152 · Miami, FLA partial loss of engine power due to the failure of the No. 3 exhaust valve. Contributing to the accident was the airplane operator’s failure to follow the engine manufacturer’s recommended engine overhaul intervals.NTSB ERA13WA304Accident · Minor injuriesForeign investigationEurocopter BO-105 · Granville, Cedros, Trinidad & TobagoOn March 26, 2013, about 1300 universal coordinated time, a Eurocopter BO-105 helicopter, Trinidad and Tobago registry 9Y-TIC, was substantially damaged during a forced landing to a forested area in Granville, Cedros, Trinidad and Tobago. The pilot sustained…NTSB ERA13LA171Accident · Serious injuriesLimited investigationFinal reportMcnulty John S Aerolite 103 · Immokalee, FLThe loss of engine power due to the seizure of the magneto piston.