NTSB investigations: GE CF6-6 series, TN

4 cases on aircraft whose registry engine model is GE CF6-6 series. Aircraft are matched to the registry by N-number and event date, checked against the reported serial number, make and model, so older matches can be wrong.

Cases per year

19992026
NTSB investigations: GE CF6-6 series, TN per year, 1999–2026: 4 cases
19991
20031
20062

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.\"eventStateOrRegion\" = 'TN' AND c.\"eventCountry\" = 'USA'
    AND c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('30020'))
  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 DCA06FA058Accident · No injuriesField investigationFinal reportBoeing MD-10-10F · Memphis, TNthe failure of the left main landing gear due to fatigue cracking in the air filler valve hole on the aft side of the landing gear. The fatigue cracking occurred due to the presence of stray nickel plating in the air filler valve hole. Contributing to this…Jul 28, 2006 · N391FE · Substantial damageNTSB DCA06FA033Accident · No injuriesField investigationFinal reportMcdonnell Douglas DC10 · Memphis, TNThe rupture of a fatigue crack in the forward air seal tooth serration of the No. 3 engine low pressure turbine stage 1 disk that initiated due to an improper weld repair performed during original manufacture. The improper weld repair changed the material…Apr 4, 2006 · N386FE · Substantial damageNTSB DCA04MA011Accident · Minor injuriesClass 1 · MajorFinal reportMcDonnell Douglas MD-10-10F · Memphis, TN1) the first officer's failure to properly apply crosswind landing techniques to align the airplane with the runway centerline and to properly arrest the airplane's descent rate (flare) before the airplane touched down; and 2) the captain's failure to…Dec 18, 2003 · N364FE · DestroyedNTSB MIA99LA220Accident · No injuriesLimited investigationFinal reportMcDonnell Douglas DC-10-10F · Memphis, TNThe inadequate design by the airplane manufacturer for using bolts to secure the inboard trailing edge flap that are susceptible to stress corrosion cracking. Also, the stress corrosion cracking failure of the four H-11 bolts that secure the left inboard…Aug 7, 1999 · N68058 · Substantial damage