# NTSB investigations: Cessna P210N: Off-field or emergency landing NTSB aviation accident and incident investigations since 1962: the probable cause, findings, aircraft, crew, weather and docket of each, linked to the FAA registry and the FAA’s own reports. ## Latest cases - [NTSB CEN22LA137](https://openairdocs.org/ntsb/CEN22LA137.md): Cessna P210N · Englewood, CO · Accident · Minor injuries · Class 3 · Limited · Final report · Mar 8, 2022 · N210GE · Destroyed > A total loss of engine power on short final for reasons that could not be determined based on the available evidence. - [NTSB ERA20LA278](https://openairdocs.org/ntsb/ERA20LA278.md): Cessna P210 · Allendale, SC · Accident · Serious injuries · Class 3 · Limited · Final report · Aug 7, 2020 · N6300W · Destroyed > A total loss of engine power as a result of fuel starvation due to contamination from a thermoplastic polymer used in the fuel system. Contributing to the accident was the pilot’s failure to report debris observed in the fuel system during previous preflight… - [NTSB ERA20CA058](https://openairdocs.org/ntsb/ERA20CA058.md): Cessna P210 · Gainesville, FL · Accident · Minor injuries · Data collection · Final report · Dec 21, 2019 · N6300W · Substantial damage > The airplane's impact by a bird during the initial climb. - [NTSB CEN19LA147](https://openairdocs.org/ntsb/CEN19LA147.md): Cessna P210 · Yankeetown, FL · Accident · Minor injuries · Class 3 · Limited · Final report · May 17, 2019 · N4861P · Substantial damage > A loss of engine power for reasons that could not be determined based on the available evidence. - [NTSB CEN18FA236](https://openairdocs.org/ntsb/CEN18FA236.md): Cessna P210N · Detroit, MI · Accident · 2 fatal · Field investigation · Final report · Jun 24, 2018 · N3896P · Substantial damage > A total loss of engine power due to fuel exhaustion. Also causal was the pilot's failure to divert earlier in the flight to another airport to ensure that the airplane had an adequate fuel reserve, and the malfunction of the landing gear extension system for… - [NTSB CEN17LA247](https://openairdocs.org/ntsb/CEN17LA247.md): Cessna P210N · Eagle, CO · Accident · No injuries · Limited investigation · Final report · Jun 30, 2017 · N210HG · Substantial damage > The loss of engine power due to fuel starvation for reasons that could not be determined because an examination of the airplane and engine did not reveal any malfunctions or failures that would have precluded normal operation. - [NTSB ERA17LA098](https://openairdocs.org/ntsb/ERA17LA098.md): Cessna P210 · Pottsville, PA · Accident · Minor injuries · Limited investigation · Final report · Jan 30, 2017 · N4796P · Substantial damage > A total loss of engine power for reasons that could not be determined because postaccident examinations of the engine and airframe did not reveal any preimpact mechanical malfunctions or failures that would have precluded normal operation. - [NTSB WPR14LA118](https://openairdocs.org/ntsb/WPR14LA118.md): Cessna P210N · Bountiful, UT · Accident · No injuries · Limited investigation · Final report · Feb 23, 2014 · N18DP · Substantial damage > Fuel starvation due to the in-flight loosening of the fuel lines attached to the fuel flow indicator as a result of inadequate maintenance. - [NTSB ERA11LA502](https://openairdocs.org/ntsb/ERA11LA502.md): Cessna P210N · South Deerfield, MA · Accident · Serious injuries · Limited investigation · Final report · Sep 23, 2011 · N210LE · Substantial damage > The failure of the electrical system due to an alternator failure during flight in instrument meteorological conditions, and the pilot’s inadequate preflight inspection and failure to use the approved checklist for the dual alternator system. Contributing to… - [NTSB CEN10FA521](https://openairdocs.org/ntsb/CEN10FA521.md): Cessna P210N · Caledonia, MI · Accident · No injuries · Field investigation · Final report · Sep 6, 2010 · N4632A · Substantial damage > A loss of engine power as a result of a fatigue failure of the crankshaft due to the loss of engine case through-bolt torque. Contributing to the accident was a mechanic's use of incorrect hardware. - [NTSB WPR10LA196](https://openairdocs.org/ntsb/WPR10LA196.md): Cessna P210N · Leavenworth, WA · Accident · No injuries · Limited investigation · Final report · Apr 4, 2010 · N3599P · Substantial damage > The failure of the number two cylinder exhaust and intake valves for undetermined reasons, which resulted in a loss of engine power. - [NTSB ERA10LA159](https://openairdocs.org/ntsb/ERA10LA159.md): Cessna P210N · Arcadia, FL · Accident · Serious injuries · Limited investigation · Final report · Mar 3, 2010 · N4797K · Substantial damage > The total loss of engine power due to a fatigue fracture of the crankshaft resulting from worn bearings. - [NTSB ERA10LA146](https://openairdocs.org/ntsb/ERA10LA146.md): Cessna P210N · Carthage, NC · Accident · Minor injuries · Limited investigation · Final report · Feb 18, 2010 · N731DS · Substantial damage > A total loss of engine power during the initial climb after takeoff for undetermined reasons. - [NTSB CEN09LA031](https://openairdocs.org/ntsb/CEN09LA031.md): Cessna 180 · Whitewater, CO · Accident · No injuries · Limited investigation · Final report · Oct 22, 2008 · N3389D · 2 aircraft · Substantial damage > Both pilots' failure to see and avoid the other airplane. Contributing factors in this accident were the Cessna 180 pilot's attention being diverted and the Cessna 210 pilot's vision being affected by the sun glare. - [NTSB LAX08LA153](https://openairdocs.org/ntsb/LAX08LA153.md): Cessna P210N · Peach Springs, AZ · Accident · No injuries · Limited investigation · Final report · May 23, 2008 · N4753K · Substantial damage > A loss of engine power due to induced catastrophic internal failure of the engine as a result of the displacement and rotation of the number 2 main bearing that resulted in a fatigue fracture of the crankshaft. - [NTSB DEN08LA069](https://openairdocs.org/ntsb/DEN08LA069.md): Cessna P210N · Elizabeth, CO · Accident · No injuries · Limited investigation · Final report · Mar 29, 2008 · N4839P · Substantial damage > the loss of engine power due to the fatigue failure of the camshaft gear. Contributing to the accident was the lack of suitable terrain for the forced landing. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ('2073454', '2073462') AND EXISTS (SELECT 1 FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' s WHERE s.case_mkey = x.case_mkey AND s.aircrafts_position = x.position AND s."tier2Number" = '440' AND s.case_mkey IN (SELECT case_mkey FROM 'https://openairdocs.org/data/latest/ntsb_events.parquet' WHERE "isDefiningEvent"))) ORDER BY c."eventDate" DESC, c."ntsbNumber" DESC ``` This list as a web page: https://openairdocs.org/ntsb-events/440/sequence?model=2073454 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.