NTSB investigations: Continental E185 series
22 cases on aircraft whose registry engine model is Continental E185 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
| 1983 | 2 |
|---|---|
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1991 | 1 |
| 1992 | 3 |
| 1993 | 1 |
| 1994 | 2 |
| 1995 | 3 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 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.engine_model_code IN ('17014')
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 ('17014')
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 CHI98LA125Accident · No injuriesLimited investigationFinal reportBeech B35 · Bentonville, ARthe damage to the empennage was due to flutter.NTSB CHI97IA122Incident · No injuriesIncident investigationFinal reportBeech 35 · Spokane, WAthe vibration of the fuselage was due to flutter.NTSB ATL97LA027Accident · No injuriesLimited investigationFinal reportBeech 35 · Lafayette, GAfailure of maintenance personnel to balance the ruddervator assemblies after they had been reskinned and painted, which resulted in flutter and subsequent damage to the empennage.NTSB CHI96LA274Accident · No injuriesLimited investigationFinal reportBeech 35 · Yankton, SDan improper in-flight decision by the pilot when he shut the engine off as the airplane approached the landing runway. Factors associated with this accident were an inadequate maintenance inspection by the mechanic when the actuating arm fracture was not…NTSB SEA96LA181Accident · No injuriesLimited investigationFinal reportBeech 35 · Spokane, WAfailure (cracking) of the aft fuselage bulkhead for undetermined reason(s).NTSB CHI96LA235Accident · No injuriesLimited investigationFinal reportBeech B35 · Chesterfield, MOimproperly balanced ruddervators and improperly installed ruddervator (elevator) trim tabs, due to improper maintenance, which resulted in ruddervator flutter and substantial damage in the area of the aft fuselage. Factors relating to the accident were:…NTSB FTW95LA258Accident · Serious injuriesLimited investigationFinal reportBeech 35 · Kingston, OKA malfunction of the propeller governor due to a loose control cable.NTSB CHI95LA186Accident · No injuriesLimited investigationFinal reportBeech A35 · Jacksonville, ILimproper maintenance and inspection of the airplane's ruddervators.NTSB LAX95LA189Accident · Minor injuriesLimited investigationFinal reportRyan Navion · Flagstaff, AZThe owner/pilot improper installation of the propeller by failing to properly connect the pitch change mechanism.NTSB FTW94LA189Accident · No injuriesLimited investigationFinal reportBeech 35 · Mckinney, TXThe ailerons being locked by a foreign object.NTSB SEA94LA080Accident · No injuriesLimited investigationFinal reportUnrein 80-P51D · Scapp00se, ORThe inadvertent unlocking of the tailwheel lock. Factors include the manufacturer's inadequate tailwheel lock.NTSB MIA93FA200Accident · 1 fatalField investigationFinal reportBeech C35 · Ocklawaha, FLFailure of a propeller blade for an undetermined reason, and failure of the pilot to maintain adequate airspeed, which resulted in an inadvertent stall. Factors related to the accident were: low pass performed by the pilot, and his possible impairment from…NTSB SEA93LA019Accident · No injuriesLimited investigationFinal reportBeech A35 · Vancouver, WADesign stress limits of the aircraft were exceeded.NTSB FTW92LA072Accident · Serious injuriesLimited investigationFinal reportRyan Navion A · Oklahoma City, OKThe propeller hydraulic control pitch setting being incorrect for undetermined reasons. A factor in the accident was the pilot's failure to identify and correct the pitch setting as the propeller went to a higher setting.NTSB DEN92FA028Accident · No injuriesField investigationFinal reportBeech 35 · Nucla, COImproper static balance of the ruddervators following rebuilding/repainting, which resulted in empennage flutter.NTSB SEA91FA261Accident · No injuriesField investigationFinal reportBeech 35 · Walla Walla, WAImproper static balance of the ruddervators following rebuilding/repainting, which resulted in empennage flutter. Improper installation of the trim tabs and an encounter with turbulence were related factors.NTSB NYC88LA130Accident · No injuriesLimited investigationFinal reportBeech 35 · New Haven, CTDuring engine start the throttle jammed in the full forward position and could not be pulled back to the idle position to retard the power. The aircraft started rolling and collided with an unoccupied parked aircraft. Examination of the throttle control…NTSB LAX87LA252Accident · No injuriesLimited investigationFinal reportBeech A35 · Santa Rosa, CAThe plt was participating in a cafe-400 (comparative acft flt efficiency) contest over a 400 mi, round robin course. While dscndg fm 7000' at the end of the flt, the plt slowed the acft to 140 mph to observe traffic. When clear, he increased the speed to 160…NTSB MIA86LA245Accident · No injuriesLimited investigationFinal reportBeech G-35 · Lantana, FLShortly after takeoff the cabin door opened. The pilot continued the short flight to his home airfield. During approach he stated that due to the increased noise in the cabin he forgot to lower the landing gear. The aircraft contacted the runway with the…NTSB MIA86LA006Accident · No injuriesLimited investigationFinal reportNorth American Navion · Tallahassee, FLThe plt stated that while doing touch-and-go landings at quincy, FL, the left main strut fell off the acft. He then returned to Tallahassee and made an intentional gear-up landing. Examination of the main landing gear scissor ass'y revealed that it failed due…NTSB MIA83LA241Accident · No injuriesLimited investigationFinal reportBeech A35 · Orlando, FLThe pilot heard a loud bang when the gear was retracted. After many attempts to extend the gear, the pilot burned off fuel, had the rwy foamed & a gear up landing was made. During the last annual inspection the landing gear actuator was removed and the worm…NTSB FTW83LA169Accident · Minor injuriesLimited investigationFinal reportBeech 35 · El Paso, TXOn a flt after an annual inspn, the plt could not retract the gear, using the normal electrical sys. It remained extended with the green safe light on & the gear pointer indicating down. He tried to assist the normal sys with the manual handcrank, although…