NTSB investigations: Hughes 269A
13 cases on aircraft the registry lists as Hughes 269A, where the first occurrence was “Loss of engine power”. 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
| 1982 | 1 |
|---|---|
| 1985 | 1 |
| 1986 | 1 |
| 1991 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 1 |
| 2001 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 1 |
Where
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 x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('4470402')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_occurrences.parquet' o WHERE o.case_mkey = x.case_mkey AND o.aircrafts_position = x.position AND o.\"occurrenceNumber\" = 1 AND o.\"occurrenceCode\" = 350))
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."mKey" IN (SELECT x.case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_aircrafts.parquet' x WHERE x.aircraft_model_code IN ('4470402')
AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_occurrences.parquet' o WHERE o.case_mkey = x.case_mkey AND o.aircrafts_position = x.position AND o."occurrenceNumber" = 1 AND o."occurrenceCode" = 350))
ORDER BY c."eventDate" DESC, c."ntsbNumber" DESCRun 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 DFW07LA061Accident · Minor injuriesLimited investigationFinal reportHughes 269A · Fulshear, TXThe loss of engine power for undetermined reasons. A contributing factor was the lack of suitable terrain for the forced landing.NTSB ATL06LA085Accident · No injuriesLimited investigationFinal reportHughes 269A · Concord, NCThe loss of engine power for undetermined reasons while maneuvering, resulting in a forced landing to uneven terrain and a roll over.NTSB CHI06CA029Accident · No injuriesData collectionFinal reportHughes 269A · Omaha, NEThe loss of engine power for an undetermined reason and the pilot's improper execution of the emergency procedure which resulted in an excessive descent rate and subsequent hard landing.NTSB FTW03TA190Accident · Minor injuriesFinal reportHughes 269A · Freer, TXLoss of engine power for undetermined reasons.NTSB CHI01LA223Accident · Minor injuriesLimited investigationFinal reportHughes 269A · Jacksonville, ILThe helicopter's loss of engine power for undetermined reasons while maneuvering close to the ground, and the low altitude and low airspeed. A factor relating to this accident was the pilot not being able to get into autorotation.NTSB CHI98LA293Accident · Serious injuriesLimited investigationFinal reportHughes 269A · Salina, KSinadequate maintenance which failed to detect corrosion in the fuel injector system and the fuel pump. Factors related to the accident were the low altitude and airspeed at which the loss of engine power occurred.NTSB CHI97GA166Accident · Serious injuriesFinal reportHughes 269A-1 · Cedar Rapids, IAloss of engine power due to undetermined reason(s). Related factors included the obstructions (building, utility pole, and transmission wires); and the lack of a functional windsock, due to inadequate facility maintenance by the operator.NTSB ATL97LA067Accident · No injuriesLimited investigationFinal reportHughes 269A · Lake Wales, FLloss of engine power for undetermined reason(s); and the flight instructor's improper flare and improper use of the flight controls, while flaring for an autorotative landing.NTSB CHI96TA306Accident · Minor injuriesFinal reportHughes 269A · Cedar Rapids, IApartial blocking of the fuel injection control, and a fracture of the induction air ducting for reasons undetermined. A factor was trees.NTSB CHI91DCJ05Accident · No injuriesFinal reportMcdonnell Douglas 269A · Harvard, NEThe pilot's failure to maintain adequate rotor RPM during aerial application maneuvers. A related factor was the pilot's inattention.NTSB ATL86LA141Accident · Serious injuriesLimited investigationFinal reportHughes 269A · Daniels, WVThe plt stated that he noted a 'large vibration' after he had taken off. He suspected a psbl bird strike or bearing failure, & subsequently, the helicopter crashed into trees. According to the plt, the eng did not fail; however, witnesses saw the helicopter…NTSB MIA86LA016Accident · No injuriesLimited investigationFinal reportHughes 269A · Marco Island, FLThe plt stated that while on a photographic flt the eng lost pwr & he autorotated the acft into the water. After the acft was recovered & returned to it's home base, the fuel system was drained & purged of all fluids, the magnetos were cleaned, reinstalled &…NTSB FTW82FPJ15Accident · Serious injuriesFinal reportHughes 269 · Boise City, OKThe plt had completed conducting tests with dyed water to determine spray pattern & coverage after recently installing special purpose aerial application equipment. While approaching for a landing at a forward speed of 15-20 mph & descending rapidly he…