# Service difficulty reports: Cessna 210J A list on [Cessna 210J](https://openairdocs.org/model/cessna-210j.md). Newest first. General aviation reporting is voluntary. - [SDR 4S42020F00000](https://openairdocs.org/sdr/4S42020F00000.md): Doubler · cracked · Jun 12, 2019 · N3320S · Cessna 210J · Fuselage Main, Bulkhead > THE FOLLOWING IS THE INFORMATION FOR THE FAA FORM 8010-4 MALFUNCTION OR DEFECT REPORT REFERENCE CRACKS IN THE MLG ACTUATOR BULKHEAD DOUBLERS ON CESSNA 210J SN 21059120 N3320S TOTAL TIME AIRFRAME IS 3837.6 HOURS. THE EFFECTED DOUBLERS WERE REMOVED FROM THIS AC - [SDR CA080328004](https://openairdocs.org/sdr/CA080328004.md): Doubler · cracked · Mar 19, 2008 · Cessna 210J · Fuselage Main, Bulkhead > DURING THE ANNUAL INSPECTION A CRACK WAS DETECTED RUNNING FROM THE ANCHOR NUT RIVET HOLE TO THE EDGE OF THE DOUBLER PLATE, THIS BRACKET IS ATTACHED TO THE REAR FRAME AT STN 209, P/N 12120402-3. AFFECTED PART REPLACED. (TC NR 20080328004) - [SDR CA080328003](https://openairdocs.org/sdr/CA080328003.md): Bracket · cracked · Mar 19, 2008 · Cessna 210J · Horizontal Stabilizer Miscellaneous Structure > DURING THE ANNUAL INSPECTION REINFORCEMENT BRACKET (P/N 12 32623-1) WAS FOUND TO HAVE A CRACK RUNNING FROM THE BOTTOM BOLT HOLE TO THE EDGE OF THE BRACKET. THE BRACKET IS ATTACHED TO THE REAR SPAR OF THE LT HORIZ STABILIZER. AFFECTED PART REPLACED. (TC NR 20 - [SDR 2008FA0000248](https://openairdocs.org/sdr/2008FA0000248.md): Throttle Switch · intermittent · Feb 4, 2008 · N1333T · Cessna 210J · Landing Gear Position and Warning > GEAR WARNING HORN WAS INOPERATIVE. AC LANDED WITH LANDING GEAR UP. SUBSEQUENT INVESTIGATION DETERMINED THROTTLE MICROSWITCH WAS MAKING INTERMITTENT CONTACT WHEN ENGAGED AND GROUND CONNECTION WAS INSUFFICIENT. CORRECTED BY REPLACING SWITCH AND REPAIRING GROU - [SDR CA070912005](https://openairdocs.org/sdr/CA070912005.md): Spar · corroded · Aug 23, 2007 · Cessna 210J · Wing Spar > (CAN) DURING A MAINTENANCE FUNCTION SEVERE CORROSION WAS DISCOVERED ON THE BOTTOM OF THE WING SPAR ENTRE SECTION. THIS SECTION OF THE SPAR HAS HIGH DENSITY FOAM GLUED TO THE SPAR WHICH PREVENTS ADEQUATE INSPECTION. THE CORROSION WAS SUCH THAT THE WING SPAR CEN - [SDR CA050720002](https://openairdocs.org/sdr/CA050720002.md): Mount Flange · cracked · Jul 11, 2005 · Cessna 210J · Engine Oil Cooler > DURING A SCHEDULED MAINTENANCE INSPECTION, THE TECHNICIAN DISCOVERED A CRACK IN THE OIL COOLER ASSEMBLY AT THE WELD WHERE THE COOLER BODY MEETS THE MOUNTING FLANGE. - [SDR CA050305001](https://openairdocs.org/sdr/CA050305001.md): Crankcase · cracked · Feb 4, 2005 · Cessna 210J · Reciprocating Engine Power Section > (CAN) VISUAL INSPECTION DETECTED CRACKED CASE. ONCE ENGINE DISMANTLED, EXCESSIVE CRACK FOUND IN THE FRONT MAIN JOURNAL AREA. LARGE SECTION OF JOURNAL COMPLETELY DETACTED FROM CASE. - [SDR 2005FA0000305](https://openairdocs.org/sdr/2005FA0000305.md): Ferrule · cracked · Feb 3, 2005 · N3301S · Cessna 210J · Propeller Assembly > DURING DISASSEMBLY FOR OVERHAUL, BLADE RETENTION FERRULE C4451 FOUND CRACKED IN BEARING FLANGE ON NR 2 BLADE. THE CRACK APPEARS TO HAVE STARTED AT AN OLD ACTUATING PIN HOLE AND IS OVER THREE INCHES LONG. S/B 196B HAD NOT BEEN ACCOMPLISHED ON THIS PROPELLER. - [SDR AUS20030744](https://openairdocs.org/sdr/AUS20030744.md): Saddle · cracked · May 30, 2003 · Cessna 210J · Main Landing Gear Attach Section > (AUS) LT MAIN LANDING GEAR SADDLE CRACKED AND LEAKING HYDRAULIC BRAKE FLUID. FURTHER INSPECTION FOUND RT MAIN LANDING GEAR SADDLE ALSO CRACKED. - [SDR 2002FA0001367](https://openairdocs.org/sdr/2002FA0001367.md): Skin · will not balance · Dec 3, 2002 · N3368S · Cessna 210J · Elevator Miscellaneous Structure > AIRCRAFT REPORTED AS NOT HAVING ENOUGH NOSE DOWN TRIM IN CRUISE FLIGHT. AFTER INSPECTION IT WAS NOTED THAT THE TRAILING EDGE OF THE LT ELEVATOR WAS CONTOURED DOWN AND A CHECK OF THE BALANCE SHOWED IT TO BE 'UNDERBALANCED' BY ALMOST TWO INCH POUNDS. THE TRAILIN - [SDR 2002FA0001302](https://openairdocs.org/sdr/2002FA0001302.md): Fitting · cracked · Jan 26, 2000 · N3366S · Cessna 210J · Horizontal Stabilizer, Attach Fittings > FITTING CRACKED DUE TO FATIGUE & VIBRATION. INSTALL IMPROVED FITTING IN HORIZONTAL STABILIZER. - [SDR 99ZZZX2203](https://openairdocs.org/sdr/99ZZZX2203.md): Skin · cracked · May 7, 1999 · N3311S · Cessna 210J · Fuselage Main, Plate/Skin > A CRACK WAS FOUND IN THE FORWARD AREA OF THE RIGHT LANDING GEAR (MAIN CUT-OUT). CESSNA ADVISED THIS WAS A COMMON PROBLEM AND PROVIDED A LETTER WITH A METHOD OF REPAIR. THE CRACK WAS APPROXIMATELY 1 INCH LONG AND RAN BENEATH A DOUBLER. - [SDR AU990446](https://openairdocs.org/sdr/AU990446.md): Bracket · corroded · Apr 20, 1999 · Cessna 210J · Vertical Stabilizer > (AUS) LOWER RUDDER ATTACHMENT BRACKET CRACKED IN HORIZONTAL PLANE. - [SDR CA990330085](https://openairdocs.org/sdr/CA990330085.md): Bulkhead · cracked · Mar 16, 1999 · Cessna 210J · Rudder Structure > (CAN) WHILE COMPLYING WITH AD 72-07-09, THE INSPECTOR DETECTED A CRACK AT THE LOWER INBOARD CORNER OF THE RIGHT RUDDER CABLE CUT-OUT OF THE AFT BULKHEAD. CRACK RUNS AT A 45 DEGREE ANGLE BELOW THE BOLT HOLE CUT-OUT. - [SDR 99ZZZX380](https://openairdocs.org/sdr/99ZZZX380.md): Ball Carriage · loose · Nov 23, 1998 · Cessna 210J · Aileron Tabs > DURING APPROACH TO LANDING, THE FLAPS SUDDENLY RETRACTED. INVESTIGATION REVEALED THE CABLE DRIVE ASSY TO WHICH THE CABLES ARE ATTACHED SEPARATED FROM THE FLAP ACTUATOR ASSY. THE CABLE DRIVE ASSY IS ATTACHED TO THE FLAP ACTUATOR BY THREADS INTERNAL TO THE CAB - [SDR 98ZZZX4529](https://openairdocs.org/sdr/98ZZZX4529.md): Spring · broken · Oct 17, 1998 · N350TM · Cessna 210J · Engine Starter > RECEIVED PART ON 10-16-98. VISUAL INSPECTION OF SPRING REVEALED A CRACK APPROXIMATELY.0625 INCH LONG ON THE FIRST COIL AT THE SPRING RETAINER CUT OUT. SUBMITTER RECOMMENDED A ONE-TIME INSPECTION OF TCM SPRINGS IN STOCK TO PREVENT PREMATURE FAILURE. BROKEN - [SDR 99ZZZX716](https://openairdocs.org/sdr/99ZZZX716.md): Hinge · cracked · Mar 20, 1998 · N3311S · Cessna 210J · Landing Gear Doors > ON ANNUAL INSPECTION, SEVERAL GEAR DOOR HINGES WERE FOUND CRACKED. CESSNA P/N'S: 1211480-6, 1211480-1, AND 1211480-3. TWO POSSIBLE CAUSES MIGHT BE IMPROPERLY RIGGED DOORS AND/OR THE AGE OF THE HINGES. - [SDR 99ZZZX715](https://openairdocs.org/sdr/99ZZZX715.md): Hinge · cracked · Mar 20, 1998 · N3311S · Cessna 210J · Landing Gear Doors > ON ANNUAL INSPECTION, SEVERAL GEAR DOOR HINGES WERE FOUND CRACKED. CESSNA P/N'S: 1211480-6, 1211480-1, AND 1211480-3. TWO POSSIBLE CAUSES MIGHT BE IMPROPERLY RIGGED DOORS AND/OR THE AGE OF THE HINGES. - [SDR 99ZZZX714](https://openairdocs.org/sdr/99ZZZX714.md): Hinge · cracked · Mar 20, 1998 · N3311S · Cessna 210J · Landing Gear Doors > ON ANNUAL INSPECTION, SEVERAL GEAR DOOR HINGES WERE FOUND CRACKED. CESSNA P/N'S: 1211480-6, 1211480-1, AND 1211480-3. TWO POSSIBLE CAUSES MIGHT BE IMPROPERLY RIGGED DOORS AND/OR THE AGE OF THE HINGES. - [SDR CA971003010](https://openairdocs.org/sdr/CA971003010.md): Doubler · broken · Sep 18, 1997 · Cessna 210J · Fuselage Main, Bulkhead > (CAN) DURING ANNUAL INSPECTION, A CRACK AT A RIVET HOLE WAS FOUND IN THE ABOVE DOUBLER. AFTER REMOVING THE DOUBLER IT WAS FOUND TO BE CRACKED INTO TWO PIECES. THE BULKHEAD ASSEMBLY WAS FOUND TO HAVE A.50 INCH CRACK RUNNING FROM EACH SIDE OF THE RIVET HOLE. - [SDR 96ZZZX4987](https://openairdocs.org/sdr/96ZZZX4987.md): Saddle · cracked · Sep 19, 1996 · N3356S · Cessna 210J · Main Landing Gear Strut/Axle/Truck > DURING ANNUAL INSPECTION AND GEAR SADDLE INSPECTION PER AD 76-14-7R2, THE OUTBOARD LT TUNNEL ASSEMBLY WAS FOUND CRACKED OUT FROM AN INSPECTION HOLE TO THE OUTER SKIN. THE CRACK STARTED JUST AFT OF A FACTORY INSTALLED DOUBLER PLATE. THE GEAR SADDLE ON THIS SI - [SDR 96ZZZX4986](https://openairdocs.org/sdr/96ZZZX4986.md): Tunnel Assy · cracked · Sep 19, 1996 · N3356S · Cessna 210J · Fuselage Miscellaneous Structure > DURING ANNUAL INSPECTION AND GEAR SADDLE INSPECTION PER AD 76-14-7R2, THE OUTBOARD LT TUNNEL ASSEMBLY WAS FOUND CRACKED OUT FROM AN INSPECTION HOLE TO THE OUTER SKIN. THE CRACK STARTED JUST AFT OF A FACTORY INSTALLED DOUBLER PLATE. THE GEAR SADDLE ON THIS SI - [SDR CA960614013](https://openairdocs.org/sdr/CA960614013.md): Cylinder · cracked · Jun 1, 1996 · Cessna 210J · Reciprocating Engine Cylinder Section > (CAN)ROUGH RUNNING ENGINE WITH A SLIGHT POWER LOSS. #2 CYLINDER HAD A SMALL HOLE IN THE HEAD AND SEVERAL CRACKS RADIATING FROM BOTH PLUG HOLES, ALSO, A 6 INCH CRACK AROUND THE HEAD AT THE TOP OF THE BARREL. - [SDR 95ZZZX5108](https://openairdocs.org/sdr/95ZZZX5108.md): Saddle · cracked · Aug 16, 1995 · N3387S · Cessna 210J · Main Landing Gear Strut/Axle/Truck > DURING ANNUAL INSPECTION AND C/W AD 76-14-07R2, FOUND LT MAIN LANDING GEAR SADDLE CRACKED IN RADIUS OF FORWARD END. ## 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 = '210J' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-210j/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.