NTSB investigations: Continental TSIO-520 series
65 cases on aircraft whose registry engine model is Continental TSIO-520 series, 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
| 1982 | 3 |
|---|---|
| 1983 | 1 |
| 1984 | 2 |
| 1985 | 3 |
| 1986 | 3 |
| 1987 | 5 |
| 1988 | 2 |
| 1989 | 4 |
| 1992 | 2 |
| 1994 | 1 |
| 1995 | 3 |
| 1996 | 3 |
| 1997 | 2 |
| 1999 | 3 |
| 2000 | 3 |
| 2001 | 5 |
| 2002 | 1 |
| 2003 | 6 |
| 2004 | 4 |
| 2005 | 3 |
| 2006 | 4 |
| 2007 | 2 |
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.engine_model_code IN ('17040')
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.engine_model_code IN ('17040')
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 ANC07LA021Accident · No injuriesLimited investigationFinal reportCessna 402C · Cordova, AKThe failure of the right main landing gear linkage during the landing roll, which resulted in a loss of directional control and the collapse of the right main landing gear. A factor associated with the accident was the failure of company maintenance personnel…NTSB CHI07LA064Accident · No injuriesLimited investigationFinal reportCessna 414A · Dickinson, NDThe undetermined failure of the emergency landing gear system and the retraction of the right main landing gear during landing.NTSB DEN07CA039Accident · No injuriesData collectionFinal reportCessna T210M · Broomfield, COthe failure of the mechanic to comply with the required replacement schedule resulting in the failure of the hydraulic line and the resulting gear up landing.NTSB SEA07LA002Accident · No injuriesLimited investigationFinal reportCessna 340A · Kalispell, MTThe fracture of the adjusting bellcrank in overstress due to binding in a linkage forward of the bell crank.NTSB DFW06CA175Accident · No injuriesData collectionFinal reportCessna C340A · San Antonio, TXThe collapse of the left main landing gear as result of the failure of the gear pivot bolt for undetermined reasons.NTSB CHI06LA080Accident · No injuriesLimited investigationFinal reportCessna 421C · Indianapolis, INThe main landing gear malfunctioned and failed to extend during the landing approach for an undetermined reason, which resulted in a main gear up landing.NTSB SEA05LA084Accident · Minor injuriesLimited investigationFinal reportCessna T210N · Kalispell, MTAn airborne fire which was fueled by leaking hydraulic fluid (the ignition source for the fire was undetermined) from the landing gear hydraulic system located under the cockpit instrument panel due to inadequate maintenance from other maintenance personnel.…NTSB NYC05IA052Incident · No injuriesIncident investigationFinal reportCessna 402C · Hyannis, MAThe mechanic's inadequate inspection, which failed to discover cracks in the left wing spar around wing station 114.NTSB LAX05LA065Accident · No injuriesLimited investigationFinal reportCessna T210M · Mesa, AZthe pilot's failure to use the emergency gear extension procedure to manually extend the landing gear to the down and locked position.NTSB LAX05FA046Accident · 1 fatalField investigationFinal reportCessna T207A · Meadview, AZa loss of control due to the in-flight separation of the right elevator and elevator trim tab control surfaces. The precipitating reason for the elevator separation could not be resolved as related to the tab foam core issue with the available evidence.NTSB LAX05CA030Accident · No injuriesData collectionFinal reportCessna P210N · Rancho Cordova, CAThe pilot's failure to refuel the airplane prior to fuel exhaustion, which resulted in a loss of engine power. Contributing factors were the pilot's improper in-flight decision to continue the flight at night after experiencing the total failure of the…NTSB CHI04LA183Accident · No injuriesLimited investigationFinal reportCessna 340A · Mason City, IAThe proper touchdown point not obtain/maintained by the pilot following a single-engine approach to landing. Contributing factors were the vacuum pump oil leak, the low oil pressure of the propeller control system, and the unfeathered propeller.NTSB LAX04LA230Accident · No injuriesLimited investigationFinal reportCessna T210M · Santa Rosa, CAMaintenance personnel's improper installation and servicing of a retaining ring, which resulted in the failure of the landing gear door actuator and failure of the landing gear extension system during landing.NTSB SEA04FA022Accident · 4 fatalField investigationFinal reportBeech S35 · Warren, ORThe vacuum pump failure and the pilot's failure to maintain control of the airplane. Factors contributing to the accident included the instrument meteorological weather conditions and the pilot's improper recovery from the descent.NTSB ANC04LA011Accident · No injuriesLimited investigationFinal reportCessna 402 · Galena, AKWater contamination and freezing of the landing gear actuator that prevented the extension of the right main landing gear, resulting in a gear-up landing. Factors contributing to the accident were freezing temperatures at the accident location, and inadequate…NTSB CHI03LA159Accident · No injuriesLimited investigationFinal reportCessna T210N · Tribune, KSThe in-flight separation of the turbocharger exhaust band clamp resulting in an in-flight fire and uncommanded landing gear extension. Also causal was the improper maintenance by unknown personnel.NTSB MIA03IA110Incident · No injuriesIncident investigationFinal reportCessna 402C · Miami, FLThe inadequate annual inspection of the airplane by other maintenance personnel for failure to note an incorrect washer was installed securing the upper and lower torque links, resulting in separation of the upper and lower links and subsequent rotation of…NTSB FTW03FA093Accident · 3 fatalField investigationFinal reportCessna T210N · Mission, TXThe pilot's failure to maintain aircraft control, which resulted in his exceeding the airplane's design limitation. Contributing factors were the pilot's decision to fly the airplane with known deficiencies with the attitude indicator, and the failure of the…NTSB LAX03LA075Accident · No injuriesLimited investigationFinal reportCessna T210L · El Monte, CAthe alternator switch contact failure, which resulted in a complete electrical failure.NTSB LAX03TA048Accident · No injuriesFinal reportCessna T210L · Agua Caliente, CAThe failure of the right main landing gear actuator during the landing roll, which resulted in a collapse of the right main land gear, and loss of directional control.NTSB DEN02TA011Accident · No injuriesFinal reportCessna 206 · Casper, WYfailure to maintain aircraft control during landing. Contributing factors were the crosswind and gusting wind conditions.NTSB SEA01LA165Accident · No injuriesLimited investigationFinal reportCessna T210L · Olympia, WAThe inability of the landing gear to fully extend due to the failure of a hydraulic hose in the nose gear extension system.NTSB SEA01LA105Accident · No injuriesLimited investigationFinal reportCessna T210M · Portland, ORA burst hydraulic line and consequent total loss of hydraulic fluid from the landing gear, which disabled landing gear operation.NTSB NYC01FA109Accident · 2 fatalField investigationFinal reportBeech A-36 · Middletown, RIThe pilot's failure to maintain airspeed while landing.NTSB DEN01LA087Accident · No injuriesLimited investigationFinal reportMooney M20K · Bountiful, UTthe failure of the airplane's electrical system for an undetermined reason, which resulted in the collapse of the left main gear on landing.NTSB SEA00FA142Accident · 1 fatalField investigationFinal reportCessna TU-206G · Pistol Creek, IDA loss of engine power due to the fracture of the #2 cylinder intake valve stem and the puncturing of the #2 piston dome by the intake valve head. Factors include no suitable landing site within the maneuvering abilities of the aircraft, and coniferous trees…NTSB SEA00LA090Accident · No injuriesLimited investigationFinal reportCessna T210M · Boise, IDThe deterioration and subsequent leakage of a hydraulic line which resulted in the total loss of hydraulic fluid and the inability of the pilot to extend the landing gear into the locked position.NTSB MIA00LA109Accident · Minor injuriesLimited investigationFinal reportCessna 402C · Fort Lauderdale, FLSeparation of the right main landing gear tire recap during takeoff resulting in the pilot's loss of directional control, the aircraft departing the runway, collapse of the landing gear, and collision with the airport fence.NTSB NYC99IA175Incident · No injuriesIncident investigationFinal reportPiper PA-46-310P · Belmar, NJThe failure of the turbocharger clamp, resulting from improper welding settings during manufacture.NTSB CHI99FA177Accident · 2 fatalField investigationFinal reportCessna 340A · Phillipsburg, KSthe pilot not maintaining flying speed. Factors to the accident were the fuel transfer problem of unknown origin.NTSB FTW99FA123Accident · 1 fatalField investigationFinal reportCessna 402C · Goldsby, OKThe fatigue failure of the right wing spar as a result of inadequate quality control during manufacture of the spar. A factor was the inadequate inspection of the right wing by maintenance personnel, which failed to detect the crack.NTSB FTW98TA051Incident · No injuriesFinal reportCessna P210N · Bryce Canyon, UTThe failure of the resistor (inverter) in the door seal pressurization air pump due to continuous operation. Factors were a failure in the door seal pressurization system, its inadequate design by the manufacturer, its inadequate written instructions for…NTSB LAX97FA143Accident · 2 fatalField investigationFinal reportCessna T210N · Grand Canyon, AZThe pilot's failure to maintain aircraft control due to spatial disorientation and his lack of proficiency in conducting instrument flight. Contributing were the inoperative alternator, cockpit lighting, and vacuum system.NTSB IAD96LA153Accident · No injuriesLimited investigationFinal reportCessna 188 · Pataskala, OHdeterioration and fuel leakage from an engine fuel hose (with a service life that had been exceed, due to inadequate maintenance), which resulted in an engine compartment fire and subsequent damage to the airplane.NTSB FTW96LA295Accident · No injuriesLimited investigationFinal reportCessna T210L · Terrell, TXthe mechanic's improper installation of the left main landing gear brake line, which resulted in chaffing and failure of the brake line, loss of hydraulic fluid, and inoperative brake(s).NTSB CHI96FA171Accident · No injuriesField investigationFinal reportCessna 401 · Great Bend, KSthe failure of the exhaust header. Additional factors include the visual restrictions which prevented a detailed examination of the exhaust system, and the inadequate inspection procedures required in AD 75-23-08 R5.NTSB SEA95LA200Accident · No injuriesLimited investigationFinal reportCessna 210 · Sunriver, ORThe failure of the landing gear hydraulic drive motor.NTSB CHI95LA096Accident · No injuriesLimited investigationFinal reportCessna T210N · Rockford, ILA disconnect of the alternator belt, and failure of the pilot to attain a down and locked condition of the gear with the emergency extension system.NTSB FTW95LA120Accident · No injuriesLimited investigationFinal reportCessna T210M · Montrose, COThe bent landing gear emergency extension assembly and the accumulation of airframe ice which interfered with landing gear activation. A factor was the alternator failure for unknown reasons.NTSB CHI95IA052Incident · No injuriesIncident investigationFinal reportCessna 402 · Saint Louis, MOimproper maintenance installation (fuel line fitting)by other maintenance personnel. A factor was the cross threaded fuel line fitting.NTSB FTW92GA227Accident · No injuriesFinal reportCessna T210L · Spring, TXThe pilot under instruction failure to follow the landing checklist and the instructor pilot's inadequate supervision. A factor was the overheated landing gear motor.NTSB ATL92LA133Accident · No injuriesLimited investigationFinal reportCessna 402B · Tuscaloosa, ALThe improper installation of the emergency exit, by an unknown person, which resulted in its separation, in flight.NTSB MKC89LA163Accident · No injuriesLimited investigationFinal reportBeech 58 · Cedar Rapids, IAThe failure of the pilot in command to maintain alignment with the runway and excessive aircraft control in close proximity to the ground. Contributing to the accident was the pilot's diverted attention which resulted from having to shut down the left engine.NTSB CHI89LA136Accident · No injuriesLimited investigationFinal reportCessna 335 · Pontiac, MIFailure of the right main landing gear extension/retraction component resulting from unacceptable loads incurred due to improper adjustment.NTSB LAX89LA233Accident · Serious injuriesLimited investigationFinal reportCessna P210N · Los Angeles, CAAn undertorqued oil line fitting, due to its improper installation by maintenance personnel, which resulted in a loose oil line fitting, an oil line leak, oil exhaustion, and subsequent failure of the engine.NTSB LAX89LA223Accident · Serious injuriesLimited investigationFinal reportCessna T210N · Herlong, CAFuel starvation, after the pilot diverted his attention to an electrical problem, and his failure to reposition the fuel selector switch, either before the engine lost power or during emergency procedures. Factors related to the accident were: the tripped…NTSB BFO88IA065Incident · No injuriesIncident investigationFinal reportCessna T210R · Washington, DCImproper maintenance resulting in the routing of wire which caused an electrical short and inflight smoke.NTSB ATL88LA105Accident · Minor injuriesLimited investigationFinal reportCessna 340A · Lincolnton, NCJust after lift off for a LCL flt, the plt-in-cmd, who was in the right seat, noted the front edge of the nose baggage compt to 'pop open'. He assumed control of the acft and attempted to 'tear drop' a return to the opposite runway. During the maneuver, the…NTSB MIA88LA030Accident · No injuriesLimited investigationFinal reportCessna T-210N · Tallahassee, FLDuring ldg gear extension plt did not get safe down indication. Attempts to use emergency extension pump were unsuccessful. Acft was landed nose gear extended main gear retracted. Post accident inspection of the acft revealed the left main gear down lock…NTSB SEA88LA005Accident · No injuriesLimited investigationFinal reportCessna 340A · Tacoma, WAAs the plt was taxiing to the active rwy, the acft's right brake became inop due to a loss of hydraulic fluid. Subsequently, the acft went off the side of the taxiway, contd over an embankment & was damaged. The loss of hydraulic fluid was due to a leak in…