# Service difficulty reports: Cessna 210K A list on [Cessna 210K](https://openairdocs.org/model/cessna-210k.md). Newest first. General aviation reporting is voluntary. - [SDR 2018FA0000518](https://openairdocs.org/sdr/2018FA0000518.md): Pump · broken · Jul 23, 2018 · N9410M · Cessna 210K · Hydraulic Pump (Electric/Engine), Main > HYDRAULIC PUMP LEAKS 5606 FROM HOUSING PARTING SURFACES DURING OPERATION. TWO HOUSING BOLTS APPEAR TO BE STRIPPED, BROKEN AND HOUSING SEAL IS EXTRUDING PAST PARTING SURFACES AROUND LEAKAGE AREA. - [SDR 2015FA0000212](https://openairdocs.org/sdr/2015FA0000212.md): Actuator · binding · May 14, 2015 · N8149G · Cessna 210K · Landing Gear Actuator > LOCK ACTUATOR BINDING AND WOULD NOT LOCK IN THE DOWN POSITION. GEAR UP LANDING. - [SDR CTUR2015FA0000020](https://openairdocs.org/sdr/CTUR2015FA0000020.md): Retaining Ring · dislodged · Dec 31, 2014 · N8229M · Cessna 210K · Landing Gear Actuator > THE RETAINING RING DISLODGED FROM THE RETAINING RING GROVE, WHICH ALLOWED THE PISTON AND ROD AND MAIN GEAR ACTUATOR GLAND TO SEPARATE FROM THE MAIN GEAR ACTUATOR CYLINDER PREVENT HYDRAULIC PRESSURE FROM BUILDING WHICH IS NECESSARY TO OPEN THE MAIN. - [SDR 2013FA0000634](https://openairdocs.org/sdr/2013FA0000634.md): Plug · failed · Nov 15, 2013 · N9443M · Cessna 210K · Reciprocating Engine Power Section > AT CRUISE 6500 FT, NR 3 PISTON PIN ALUMINUM END PLUG BROKE OFF THE STEEL PIN. THIS CAUSED DAMAGE TO THE PISTON, RINGS, CYLINDER AND ULTIMATELY STOPPED THE ENGINE, SEIZED. - [SDR 2013FA0000132](https://openairdocs.org/sdr/2013FA0000132.md): O-Ring · failed · Feb 20, 2013 · N210Y · Cessna 210K · Nose/Tail Landing Gear Strut/Axle > INTERNAL O-RING FAILED AND UPLOCK WOULD NOT RELEASE NOSE GEAR, RESULTING IN GEAR NOT EXTENDING, PROP DAMAGE, SUDDEN ENGINE STOPPAGE, AND LOWER SKIN DAMAGE. - [SDR FAA0607002](https://openairdocs.org/sdr/FAA0607002.md): Firewall · cracked · Jun 27, 2006 · N8142G · Cessna 210K · Fuselage Main, Bulkhead > WHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD. - [SDR FAA0607001](https://openairdocs.org/sdr/FAA0607001.md): Firewall · cracked · Jun 27, 2006 · N8142G · Cessna 210K · Fuselage Main, Bulkhead > WHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD. - [SDR N8142G](https://openairdocs.org/sdr/N8142G.md): Firewall · cracked · Jun 27, 2006 · N8142G · Cessna 210K · Fuselage Main, Bulkhead > WHILE UNDERGOING AN ANNUAL INSPECTION THE ENGINE FIREWALL WAS FOUND TO BE CRACKED WHERE THE EXHAUST HANGER BRACKETS ATTACH ON THE LT SIDE. ADDITIONAL CRACKING WAS ALSO FOUND ON THE INNER BULKHEAD. - [SDR AUS20021036](https://openairdocs.org/sdr/AUS20021036.md): Actuator · cracked · Sep 8, 2002 · Cessna 210K · Landing Gear Actuator > (AUS) LH MAIN LANDING GEAR COULD NOT BE EXTENDED. THE FAULT WAS TRACED TO A BROKEN ACTUATOR PISTON/RACK. BREAK OCCURRED IN THE RACK AREA TWO TEETH IN FROM THE END AND ORIGINATING AT THE BASE OF THESECOND TOOTH. THE CRACK FACE SHOWS EVIDENCE OF BEACH MARKS' I - [SDR RFS20011](https://openairdocs.org/sdr/RFS20011.md): Bolt · cracked · Aug 8, 2001 · N8142G · Cessna 210K · Landing Gear Actuator > WHILE REPLACING THE RT MLG ACTUATOR AS PART OF COMPIANCE WITH CESSNA SEB01-2, IT WAS DISCOVERED THAT ONE OF THE THREE NAS ATTACH BOLTS WAS BROKEN.IT WAS ONLY BEING HELD IN PLACE BY THE SAFETY WIRE LINKING THE THREE BOLTS. THE BOLT HAD FAILED BETWEEN THE FIRST - [SDR AU980432](https://openairdocs.org/sdr/AU980432.md): Bearing · seized · Mar 24, 1998 · Cessna 210K · Flight Control System > (AUS) ALL ELEVATOR, ELEVATOR BELLCRANK AND RUDDER BEARINGS SEIZED. - [SDR AU980430](https://openairdocs.org/sdr/AU980430.md): Floor · corroded · Mar 24, 1998 · Cessna 210K · Fuselage Floor Panel > (AUS) BOTH PILOT'S AND COPILOT'S FLOOR SKINS BADLY CORRODED FORWARD OF DOOR. - [SDR AU980429](https://openairdocs.org/sdr/AU980429.md): Bushing · loose · Mar 24, 1998 · Cessna 210K · Alternator-Generator Drive > (AUS) ALTERNATOR ATTACHMENT BUSHES VERY LOOSE AND EXCESSIVELY WORN. - [SDR AU980428](https://openairdocs.org/sdr/AU980428.md): Fitting · worn · Mar 24, 1998 · Cessna 210K · Engine Fuel Distribution > (AUS) FUEL PRESSURE FITTING ON ENGINE FUEL PUMP CHAFED THROUGH. - [SDR AU980427](https://openairdocs.org/sdr/AU980427.md): Light · inoperative · Mar 24, 1998 · Cessna 210K · Lighting System > (AUS) ROTATING BEACON, LANDING LIGHT, TAXI LIGHT AND PANEL LIGHTING INOPERATIVE. PERSONNEL/MAINTENANCE ERROR. - [SDR AU980398](https://openairdocs.org/sdr/AU980398.md): Filter · crushed · Mar 24, 1998 · Cessna 210K · Aircraft Fuel Filter/Strainer > (AUS) FUEL FILTER ASSEMBLY STRAINER FOUND CRUSHED ALLOWING UNFILTERED FUEL INTO FUEL PUMP AND ENGINE SYSTEM. PERSONNEL/MAINTENANCE ERROR. - [SDR AU980360](https://openairdocs.org/sdr/AU980360.md): Control Cable · corroded · Mar 24, 1998 · Cessna 210K · Elevator Tab Control System > (AUS) ELEVATOR TRIM CABLES P/N 126075-9 AND P/N 126075-10 CORRODED. - [SDR AU980359](https://openairdocs.org/sdr/AU980359.md): Screw · distorted · Mar 24, 1998 · Cessna 210K · Elevator Tab Control System > (AUS) ELEVATOR TRIM ACTUATOR SCREW BENT. - [SDR AU980353](https://openairdocs.org/sdr/AU980353.md): Spar · corroded · Mar 24, 1998 · Cessna 210K · Wing Spar > (AUS) WING SPAR ASSEMBLY CONTAINED DEEP PITTING CORROSION ON THE LOWER WING ATTACHMENT LUG. CAUSED BY A BROKEN AND RUSTY SCAT HOSE WIRE RESTING ON THE SPAR. - [SDR AU980351](https://openairdocs.org/sdr/AU980351.md): Bearing · failed · Mar 24, 1998 · Cessna 210K · Main Landing Gear Strut/Axle/Truck > (AUS) LT MAIN LANDING GEAR AFT TRUNNION SPHERICAL BEARING OUTER RACE SHATTERED. INCORRECT BEARING FITTED. A BUSH SHOULD BE FITTED IN THIS AREA AND NOT A SPHERICAL BEARING. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART. - [SDR AU980358](https://openairdocs.org/sdr/AU980358.md): Bulkhead · cracked · Mar 23, 1998 · Cessna 210K · Fuselage Main, Bulkhead > (AUS) FUSELAGE BULKHEAD LOCATED AT STN 209 CRACKED. BULKHEAD HAD BEEN INCORRECTLY REPAIRED PREVIOUSLY ALLOWING CRACKING AT HORIZONTAL STABILIZER ATTACHMENT POINTS. PERSONNEL/MAINTENANCE ERROR. - [SDR EY2R9600042](https://openairdocs.org/sdr/EY2R9600042.md): Hub · cracked · Mar 1, 1996 · Cessna 210K · Propeller Hub Section > HUB CRACKED IN NR 1 SOCKET - [SDR EY2R9600041](https://openairdocs.org/sdr/EY2R9600041.md): Hub · cracked · Mar 1, 1996 · Cessna 210K · Propeller Hub Section > HUB CRACKED IN BLADE SOCKET - [SDR 95ZZZX511](https://openairdocs.org/sdr/95ZZZX511.md): Uplock Valve · missing part · Jan 4, 1995 · N8223M · Cessna 210K · Landing Gear Retraction/Extension System > AIRCRAFT NOSE GEAR COLLAPSED AFTER A LANDING GROUND ROLL WITH MINOR DAMAGE TO AIRCAFT AND PROP BLADES. INSPECTION FOUND NOSE GEAR UPLOCK VALVE, THAT HAD BEEN REPLACED PRIOR TO FLIGHT WITH A USED UNIT, MISSING A SMALL CHECK BALL CAUSING A LARGER CHECK BALL TO ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = '210K' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-210k/reports --- 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.