NTSB investigations, Outside the U.S.
23 cases where NTSB found Aircraft power plant.
Cases per year
| 2008 | 2 |
|---|---|
| 2009 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 3 |
| 2014 | 1 |
| 2015 | 1 |
| 2017 | 1 |
| 2018 | 1 |
| 2019 | 3 |
| 2020 | 1 |
| 2022 | 1 |
| 2024 | 1 |
| 2025 | 3 |
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 c.\"eventCountry\" <> 'USA'
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 c."eventCountry" <> 'USA' 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 ENG25WA049IncidentClass 3 · ForeignEmbraer EMB145 · Sokoto, NigeriaNTSB ENG25WA034OccurrenceClass 5 · ForeignAirbus A321 · Ciudad de México, MexicoNTSB ENG25WA015IncidentClass 5 · ForeignBombardier BD100 1A10 · Nassau, BahamasNTSB ENG24LA014Incident · No injuriesClass 3 · LimitedFinal reportBoeing 787 · Singapore, SingaporeThe uncontained left engine failure was caused by the failure and liberation of the HPT stage 1 aft blade retainer as a result of a fatigue crack in the upper collet radius that originated from a surface connected cluster of Oxide/Carbonitride/Nitride/Carbide…NTSB ENG22LA049IncidentClass 3 · LimitedFinal reportBombardier Global 7500 · Riyadh, Saudi ArabiaAn in-flight engine fire resulted from a fuel leak from fuel nozzle No. 18 pigtail-to-fuel manifold b-nut connection that contacted hot engine parts and ignited. Contributing to the manifold fuel leak was the misalignment between fuel manifold female ferrule…NTSB ENG20LA015Incident · No injuriesClass 4 · LimitedFinal reportAirbus A220 · Bordeaux, FranceA No. 1 (left) engine low pressure compressor (LPC) stage 1 integrally bladed rotor (IBR) separation due to a high cycle fatigue crack (HCF) that originated at the runout of an airfoil leading edge root radius. The HCF crack developed because of a…NTSB ENG20LA001IncidentClass 3 · LimitedFinal reportAirbus BD-500-1A11 (CS300) · West Flanders Province, BelgiumA No. 1 (left) engine low pressure compressor (LPC) stage 1 integrally bladed rotor (IBR) separation due to a high cycle fatigue crack (HCF) that originated at the runout of an airfoil leading edge root radius. The HCF crack developed because of a…NTSB ENG19IA034Incident · No injuriesClass 3 · IncidentFinal reportAirbus A220 · Côte-d'Or Region, FranceA No. 1 (left) engine low pressure compressor (LPC) stage 1 integrally bladed rotor (IBR) separation due to a high cycle fatigue crack (HCF) that originated at the runout of an airfoil leading edge root radius. The HCF crack developed because of a…NTSB ENG19IA029Incident · No injuriesClass 3 · IncidentFinal reportAirbus A220 · Perrigny-sur-Armançon, FranceA No. 1 (left) engine low pressure compressor (LPC) stage 1 integrally bladed rotor (IBR) separation due to a high cycle fatigue crack (HCF) that originated at the runout of an airfoil leading edge root radius. The HCF crack developed as a result of a…NTSB ENG19IA008IncidentClass 3 · IncidentFinal reportAirbus A220 · Busan, South KoreaThe manufacturer’s inadequate cleaning of the crucible before melting the nickel alloy used in casting the low pressure turbine stage 3 blades that resulted in a casting anomaly from where an intergranular crack occurred became the origin of a fatigue crack…NTSB ENG17IA026Incident · No injuriesIncident investigationFinal reportBoeing 747 451 · Tokyo, JapanThe PW4056 engine lost power due to the fatigue fracture of a 5th stage compressor blade. The cause of the fatigue fracture could not be determined.NTSB ENG16IA001Incident · No injuriesIncident investigationFinal reportBoeing 747 · Russian airspace, JapanThe PW4056 engine experienced an in-flight loss of power because of damage to the low-pressure turbine (LPT) because of the inadequate overhaul inspection and repair instructions that existed at the time of the LPT module's last overhaul. A vane hook in the…NTSB ENG14IA029Incident · No injuriesIncident investigationFinal reportBombardier CRJ700 · Hodeida, YemenThe probable cause of the undercowl engine fire was the burn-through of the combustion chamber inner liner from the accumulation of dust that became molten during operating and infiltrated the combustion chamber thermal barrier coating causing it to spall off…NTSB CEN14WA180Accident · No injuriesForeign investigationChristen Industries Pitts S-2B · Meaux-Esbly, FranceOn December 8, 2013, at 1607 coordinated universal time, a Pitts S-2B airplane, F-GEAL, experienced a loss of engine power and conducted a force landing near Meaux-Esbly, France. The pilot and passenger were not injured. The airplane was substantially…NTSB ENG13WA040Incident · No injuriesForeign investigationSikorsky S76 - A · Macae, BrazilWhile the helicopter was running on the runway, the pilots noticed that the number two engine parameters were below prescribed values and decided to abort the take-off. After leaving the runway and entering the company apron, the pilots saw company mechanics…NTSB ENG13IA033Incident · No injuriesIncident investigationFinal reportBoeing 777 · Ugolny Airport, RussiaThe failure of the transfer gearbox resulting from the fracture and separation of the radial gearshaft from fatigue cracking as a result of a combination of high residual tensile stresses produced by local decarburization during the manufacturing process…NTSB CEN13WA102Incident · No injuriesForeign investigationRobinson Helicopter R44 · Oosterschelde, NetherlandsOn January 21, 2012, at 1430 universal coordinated time, a Robinson Helicopter Company model R44, Dutch registration PH-WMW, made an uneventful forced landing after experiencing a partial loss of engine power near Oosterschelde, The Netherlands. The pilot and…NTSB ERA11WA209Accident · Serious injuriesForeign investigationCessna 182 · Palora, EcuadorOn Feburary 14, 2011, about 1935, universal coordinated time, a Cessna 182E, Ecuadorian registration HC-CDL, registered to and operated by Fundación Amazónica., incurred substantial damage during a force landing in rough terrain due to a total loss of engine…NTSB ERA10WA236Accident · Serious injuriesForeign investigationCessna 150 · Santo Domingo, EcuadorOn April 7, 2010, about 1300 central standard time, a Cessna 150M, of Ecuadorian registration, HC-CHL, registered to and operated by Sky Ecuador Aerolineas S.A., incurred substantial damage during a force landing in rough terrain due to a partial loss of…NTSB ENG09IA017Incident · Minor injuriesIncident investigationFinal reportEmbraer ERJ 190-100 IGW · Nassau, Bahamasfailure of the engine high pressure turbine active clearance control valve fuel rod supply tube coupling seal due to a cross-threaded B-nut as installed during original manufacture.NTSB ENG09IA004Incident · No injuriesIncident investigationFinal reportMcdonnell-Douglas DC-10-30 · Bogota, ColombiaFailure of the low pressure turbine stage 3 disk due to a design that is vulnerable to high pressure turbine unbalance-induced synchronous vibration that cannot be detected in flight, and the subsequent uncontained engine failure.NTSB NYC08IA290Incident · No injuriesIncident investigationFinal reportBoeing 747-209B · Bogota, ColombiaThe combination of fan blade edge contour, variable blade trim, and the high altitude, which resulted in an engine surge.NTSB ENG08IA030IncidentIncident investigationFinal reportBoeing B747 · Jeddah, Saudi ArabiaFailure of the low pressure turbine stage 3 disk due to a design that is vulnerable to high pressure turbine unbalance-induced synchronous vibration that cannot be detected in flight, and the subsequent uncontained engine failure.