NTSB investigations

5 cases where NTSB found Fuselage attach fittings sys.

Cases per year

20102026
NTSB investigations per year, 2010–2026: 5 cases
20102
20131
20201
20221

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.\"mKey\" IN (SELECT f.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_findings.parquet' f WHERE starts_with(f.\"findingCode\", '01035340'))
  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 ANC22FA041Accident · Serious injuriesClass 3 · FieldFinal reportBell 407 · Kalea, HIThe in-flight separation of the tail boom as a result of abnormal loading and fracture of the upper-left tail boom attachment bolt due to a gap between the upper-left longeron and aft fuselage bulkhead.Jun 9, 2022 · N402SH · Substantial damageNTSB WPR21LA037Accident · No injuriesClass 3 · LimitedFinal reportRemos Aircraft Gmbh Flugzeugbau GX · Glendale, AZThe material overstress failure of the airframe’s aluminum carry-through of the main landing gear.Nov 4, 2020 · N87GX · Substantial damageNTSB WPR13FA411Accident · 1 fatalField investigationFinal reportBell UH 1B · Detroit, ORThe fatigue failure of the upper two tailboom attachment points, which resulted in the tailboom separating from the fuselage during logging operations. Contributing to the accident was poor maintenance throughout the helicopter’s operational life.Sep 16, 2013 · N204UH · Substantial damageNTSB CEN10LA560Accident · No injuriesLimited investigationFinal reportSchweizer 269C · Schaumburg, ILThe in-flight separation of the left aft cluster fitting assembly following the loss of torque on the lock nut due to a manufacturing defect.Sep 20, 2010 · N34LB · Substantial damageNTSB CEN10LA414Accident · No injuriesLimited investigationFinal reportWogenstahl Wallace L Wogenstahl 281 MR · Mount Cory, OHThe improper installation of the rivets at the aft fuselage bulkhead which resulted in the pilot not having full elevator control on landing.Jul 14, 2010 · N5281R · Substantial damage