Cessna 210J

Service difficulty reports · 24

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

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.

SDR 4S42020F00000Doubler · crackedTHE 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 ACJun 12, 2019 · N3320S · Cessna 210J · Fuselage Main, BulkheadSDR CA080328004Doubler · crackedDURING 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)Mar 19, 2008 · Cessna 210J · Fuselage Main, BulkheadSDR CA080328003Bracket · crackedDURING 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 20Mar 19, 2008 · Cessna 210J · Horizontal Stabilizer Miscellaneous StructureSDR 2008FA0000248Throttle Switch · intermittentGEAR 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 GROUFeb 4, 2008 · N1333T · Cessna 210J · Landing Gear Position and WarningSDR CA070912005Spar · corroded(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 CENAug 23, 2007 · Cessna 210J · Wing SparSDR CA050720002Mount Flange · crackedDURING 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.Jul 11, 2005 · Cessna 210J · Engine Oil CoolerSDR CA050305001Crankcase · cracked(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.Feb 4, 2005 · Cessna 210J · Reciprocating Engine Power SectionSDR 2005FA0000305Ferrule · crackedDURING 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.Feb 3, 2005 · N3301S · Cessna 210J · Propeller AssemblySDR AUS20030744Saddle · cracked(AUS) LT MAIN LANDING GEAR SADDLE CRACKED AND LEAKING HYDRAULIC BRAKE FLUID. FURTHER INSPECTION FOUND RT MAIN LANDING GEAR SADDLE ALSO CRACKED.May 30, 2003 · Cessna 210J · Main Landing Gear Attach SectionSDR 2002FA0001367Skin · will not balanceAIRCRAFT 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 TRAILINDec 3, 2002 · N3368S · Cessna 210J · Elevator Miscellaneous StructureSDR 2002FA0001302Fitting · crackedFITTING CRACKED DUE TO FATIGUE & VIBRATION. INSTALL IMPROVED FITTING IN HORIZONTAL STABILIZER.Jan 26, 2000 · N3366S · Cessna 210J · Horizontal Stabilizer, Attach FittingsSDR 99ZZZX2203Skin · crackedA 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.May 7, 1999 · N3311S · Cessna 210J · Fuselage Main, Plate/SkinSDR AU990446Bracket · corroded(AUS) LOWER RUDDER ATTACHMENT BRACKET CRACKED IN HORIZONTAL PLANE.Apr 20, 1999 · Cessna 210J · Vertical StabilizerSDR CA990330085Bulkhead · cracked(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.Mar 16, 1999 · Cessna 210J · Rudder StructureSDR 99ZZZX380Ball Carriage · looseDURING 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 CABNov 23, 1998 · Cessna 210J · Aileron TabsSDR 98ZZZX4529Spring · brokenRECEIVED 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 Oct 17, 1998 · N350TM · Cessna 210J · Engine StarterSDR 99ZZZX716Hinge · crackedON 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.Mar 20, 1998 · N3311S · Cessna 210J · Landing Gear DoorsSDR 99ZZZX715Hinge · crackedON 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.Mar 20, 1998 · N3311S · Cessna 210J · Landing Gear DoorsSDR 99ZZZX714Hinge · crackedON 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.Mar 20, 1998 · N3311S · Cessna 210J · Landing Gear DoorsSDR CA971003010Doubler · broken(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. Sep 18, 1997 · Cessna 210J · Fuselage Main, BulkheadSDR 96ZZZX4987Saddle · crackedDURING 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 SISep 19, 1996 · N3356S · Cessna 210J · Main Landing Gear Strut/Axle/TruckSDR 96ZZZX4986Tunnel Assy · crackedDURING 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 SISep 19, 1996 · N3356S · Cessna 210J · Fuselage Miscellaneous StructureSDR CA960614013Cylinder · cracked(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 .Jun 1, 1996 · Cessna 210J · Reciprocating Engine Cylinder SectionSDR 95ZZZX5108Saddle · crackedDURING ANNUAL INSPECTION AND C/W AD 76-14-07R2, FOUND LT MAIN LANDING GEAR SADDLE CRACKED IN RADIUS OF FORWARD END.Aug 16, 1995 · N3387S · Cessna 210J · Main Landing Gear Strut/Axle/Truck
Back to Cessna 210J