Final NTSB investigations, Outside the U.S.

5 cases where the defining event was Powerplant sys/comp malf/fail.

Cases per year

20182026
Final NTSB investigations, Outside the U.S. per year, 2018–2026: 5 cases
20181
20193
20201

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.\"completionStatus\" = 'Completed'
    AND c.\"mKey\" IN (SELECT e.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' e WHERE e.\"isDefiningEvent\" AND e.\"tier2Number\" = '340')
  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.

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…Feb 12, 2020 · YL-AAU · No damageNTSB 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…Oct 15, 2019 · HB-JCC · Minor damageNTSB 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…Sep 16, 2019 · HB-JCA · No damageNTSB 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…Jul 25, 2019 · HB-JCM · Minor damageNTSB 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…Dec 26, 2018 · HL8314 · No damage