Final NTSB investigations: Pratt & Whitney Canada PW206C

7 cases on aircraft whose registry engine model is Pratt & Whitney Canada PW206C. 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

20022026
Final NTSB investigations: Pratt & Whitney Canada PW206C per year, 2002–2026: 7 cases
20021
20051
20061
20091
20121
20141
20191

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.\"completionStatus\" = 'Completed'
    AND c.\"mKey\" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.engine_model_code IN ('52160'))
  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 ENG20IA005Incident · No injuriesClass 3 · IncidentFinal reportAgusta A109 · Penobscot, MEFatigue fracture of the main rotor blade tip cap leading edge and subsequent partial separation of the tip cap, resulting in increased vibrations in the main rotor.Nov 16, 2019 · N901EM · Minor damageNTSB CEN14FA369Accident · 3 fatalField investigationFinal reportAgusta A109E · Newkirk, NMThe pilot's inadvertent visual flight into instrument meteorological conditions, which resulted in a loss of helicopter control.Jul 17, 2014 · N507CF · DestroyedNTSB CEN12FA670Accident · Serious injuriesField investigationFinal reportAgusta A109E · Eastland, TXThe loss of helicopter control after an in-flight upset, which occurred when the pilot selected the autopilot’s altitude hold mode; the reason for the reported in-flight control anomaly could not be determined during postaccident helicopter examinations.…Sep 30, 2012 · N144CF · Substantial damageNTSB CEN09PA348Accident · 2 fatalClass 1Final reportAgusta A109E · Santa Fe, NMThe pilot's decision to take off from a remote, mountainous landing site in dark (moonless) night, windy, instrument meteorological conditions. Contributing to the accident were an organizational culture that prioritized mission execution over aviation safety…Jun 10, 2009 · N606SP · DestroyedNTSB DFW06LA057Accident · No injuriesLimited investigationFinal reportAgusta A109E · Fort Worth, TXThe pilot's inadvertent encounter with ground resonance which resulted in the destruction of the helicopter.Jan 19, 2006 · N142CF · Substantial damageNTSB SEA06FA015Accident · Minor injuriesField investigationFinal reportAgusta A109E · Olympia, WAThe pilot's improper positioning of the number 2 Power Flight Control switch and his inability to obtain the proper climb rate to clear a concrete wall barrier. Contributing factors included the checklist not being followed and the limit override switch not…Oct 29, 2005 · N950AL · Substantial damageNTSB FTW03LA038Accident · No injuriesLimited investigationFinal reportAgusta A109E · Fort Worth, TXThe pilot's attempted running takeoff with the power controls in the improper position.Nov 8, 2002 · N142CF · Substantial damage