NTSB investigations: Cessna TR182
12 cases on aircraft the registry lists as Cessna TR182, where the first occurrence was “Airframe/component/system failure/malfunction”. 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
| 1984 | 1 |
|---|---|
| 1985 | 1 |
| 1986 | 1 |
| 1992 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1999 | 1 |
| 2000 | 1 |
| 2002 | 2 |
| 2004 | 1 |
Where
Open the mapLatest 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 ('2072735')
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\" = 130))
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 ('2072735')
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" = 130))
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 LAX04LA287Accident · No injuriesLimited investigationFinal reportCessna TR182 · Torrance, CAA wheels up landing due to the failure of the hydraulic hose leading to the nose gear actuator, which depleted the hydraulic system of pressurized fluid.NTSB NYC03LA026Accident · No injuriesLimited investigationFinal reportCessna TR182 · Willoughby, OHThe pilot's failure to select the alternator to the "ON" position before initiating the flight. A factor in the accident was the tailwind which resulted in the overrun.NTSB CHI02LA218Accident · Serious injuriesLimited investigationFinal reportCessna TR182 · Copemish, MIThe in-flight engine and cabin fire caused by a fatigue fracture of the left exhaust stack assembly. An additional cause was the part's inadequate design by the aftermarket part manufacturer. A factor to the accident was the soft field in which the emergency…NTSB DEN00LA099Accident · Minor injuriesLimited investigationFinal reportCessna TR182 · Milford, UTThe failure of the turbocharger scavenging pump resulting in the total failure of the engine, and the pilot's failure to compensate for wind conditions that led him to over fly the runway during his forced landing. Factors were the pilot's diverted attention…NTSB LAX00LA019Accident · No injuriesLimited investigationFinal reportCessna TR182 · Fresno, CAInadequate maintenance inspection mandated by the FAA, and the inadequate design of the exhaust heater core/muffler and deflectors that failed to divert hot exhaust gasses away from the battery and cabin heat valve.NTSB FTW97LA111Accident · No injuriesLimited investigationFinal reportCessna TR182 · Pueblo, COImproper repair to the nose landing gear assembly. A factor was binding of the nose gear extension assembly due to the improper repair.NTSB FTW96LA402Accident · No injuriesLimited investigationFinal reportCessna TR182 · Telluride, COfailure of the generator control unit (GCU), which resulted in a total electrical failure and failure of the main landing gear to lock in place.NTSB SEA96LA013Accident · No injuriesLimited investigationFinal reportCessna TR182 · Salt Lake City, UTmaintenance personnel improperly installed a landing gear system hydraulic line and the throttle cable which resulted in chaffing and subsequent loss of hydraulic fluid disabling the landing gear extention systems.NTSB CHI92LA118Accident · Minor injuriesLimited investigationFinal reportCessna TR182 · Joliet, ILThe pilot-in-command's failure to follow emergency procedures, and the failure of the electrical system. Factors contributing to the accident were electrical arcing, and the lack of total experience in the type of aircraft by the pilot-in-command.NTSB LAX86LA332Accident · No injuriesLimited investigationFinal reportCessna TR182RG · San Jose, CAThe plt was unable to fully extend the landing gear and the acft collided with the surface of rwy 30R during landing. Post accident inspection revealed the gear down hose assembly was ruptured thus allowing for a loss of hydraulic fluid.NTSB LAX85LA263Accident · No injuriesLimited investigationFinal reportCessna TR 182 · Mesa, AZDuring initial climb on a dual instructional flight a fire erupted behind the instrument panel & the acft was returned for landing. During roll out 6 inch long flames, smoke & noxious fumes filled the cockpit. When the acft slowed to 10 mph the plts exited…NTSB MIA84LA144Accident · No injuriesLimited investigationFinal reportCessna TR182 · Daytona Beach, FLThe plt was unable to lower the landing gear and made a wheels-up landing. An exam revealed that a rod end, pn S02321-3, on the nose gear door had failed. The failure was in tension bending with no signs of preexisting fatigue or corrosion.