Cessna 210M

Service difficulty reports · 94

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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 = '210M'
  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 2014FA0000711Line · leakingFUEL LINE, THAT GOES FROM THE FUEL SELECTOR TO THE FUEL BOOST PUMP WAS FOUND LEAKING PROFUSELY. HOSE LOOKED TO BE ORIGINAL EQUIPMENT.Dec 16, 2014 · N761WU · Cessna 210M · Aircraft Fuel Distribution SystemSDR CCJA201306280001Gear · failedDURING GROUND OPERATION, CAM SHAFT GEAR BROKE TWO TEETH. MOTOR AND DIRECTLY RELATED ACCESSORIES WERE REMOVED AND O/H. IT WAS UNDETERMINED BY THE O/H SHOP, THE CAUSE OF THE GEAR FAILURE.Mar 12, 2013 · N6035N · Cessna 210M · Reciprocating Engine Power SectionSDR FPI2012F00008Cylinder Head · crackedDURING A 100 HR INSPECTION/ COMPRESSION TEST/ BUBBLE LEAK CHECK FOUND NR 2 CYCLE POSITION HEAD CRACKED INTO THE COMBUSTION CHAMBER - CYLINDER ASSY.Jun 9, 2012 · N9489M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR FPI2012F00009Cylinder Head · crackedDURING A 100 HR INSPECTION/ COMPRESSION TEST/ BUBBLE LEAK CHECK, FOUND NR 4 CYLINDER POSITION HEAD CRACKED INTO THE COMBUSTION CHAMBER- REPLACED CYLINDER ASSY.May 9, 2012 · N9489M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR FPI2012F00006Cylinder Head · crackedDURING A 100 HR INSPECTION, COMPRESSION TEST AND SOAP BUBBLE TEST FOR CRACKS FOUND THE NR 6 CYLINDER HEAD CRACKED INTO THE COMBUSTION CHAMBER LEAKING COMPRESSED AIR.May 3, 2012 · N9073M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR FPI2011F00008Impulse Coupling · failedDURING INVESTIGATIONOF REPORTED MAGNETO FAIL, REMOVED LT & RT MAGS AND FOUND LT MAGNETO IMPULSE COUPLING DRIVE PADS AND CAGE WERE BROKEN. DISASSEMBLED LT MAG AND FOUND ROTOR GEAR STRIPPED AND THE BREAKER END ROLLER BEARING HAD FAILED AND COME APART AND JAMED Oct 13, 2011 · N8427M · Cessna 210M · Magneto/DistributorSDR FPI2011F00009Cylinder · crackedCURING A 100 HR INSPECTION, FOUND NR1 CYLINDER CRACKED FROM FUEL NOZZLE TO SPARK PLUG PORT. REPLACED CYLINDER ASSY.Oct 12, 2011 · N778VK · Cessna 210M · Reciprocating Engine Cylinder SectionSDR 2011FA0000543Alternator · failedALTERNATOR COOLING FAN CAME APART IN FLIGHT AFTER TAKEOFF. PART OF COOLING FAN PUNCHED A HOLE IN INDUCTION AIR BOX DOWN STREAM OF AIR FILTER AND THE ALTERNATOR BELT CAME LOOSE IN THE ENGINE COMPARTMENT. LOSS OF ENGINE POWER FROM ENGINE FOD DAMAGE RESULTED INAug 11, 2011 · N732VU · Cessna 210M · DC Generator-AlternatorSDR FPI2011F00007Cylinder · crackedDURING A 100 HR INSPECTION, COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM CYLINDER HEAD COOLING FINS ABOVE EXHAUST PORT. NO VISUAL CRACKS NOTED.Jul 20, 2011 · N9073M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR FPI2011F00006Cylinder · crackedDURING A 100 HR INSPECTION FOUND THE CYLINDER AHEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM COOLING FINS ABOVE EXHAUST PORT.Jul 20, 2011 · N9073M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR FPI2011F00005Cylinder · crackedDURING A 100 HR INSPECTION FOUND THE CYLINDER AHEAD WAS CRACKED FROM THE FUEL INJECTOR PORT TO THE UPPER SPARK PLUG BY VISUAL INSPECTION. DURING COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM COOLING FINS ABOVE EXHAUST PORT.Jul 20, 2011 · N9073M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR FPI2011F00000Gasket · failedDURING A SCHEDULED INSPECTION OF ENGINE, FOUND 5 OUT OF 5 INDUCTION GASKETS LEAKING. AFTER REMOVING INTAKE TUBES, OBSERVED THAT THE GASKETS WERE CRACKED AND TORN DURING INSTALLATION AT ASSEMBLY AT MFG AND WAS POSSIBILY CAUSE OF HIGH CHT READINGS.Apr 11, 2011 · N732YA · Cessna 210M · Reciprocating Engine Cylinder SectionSDR CA110208018Torque Tube · corroded(CAN) DURING ANNUAL INSPECTION, PILOT`S LT RUDDER PEDAL ARM PART NUMBER FOUND LOOSE ON TORQUE TUBE. THE BOLT SECURING ARM TO TORQUE TUBE FOUND TO BE EXTREMELY CORRODED. INTERNAL INSPECTION OF MOUNTING ARM AND TORQUE TUBE STUB-END REVEALED SEVERE CORROSION IN Feb 4, 2011 · Cessna 210M · Rudder Control SystemSDR 2010FA0001200Camshaft · wornMETAL PARTICLES FOUND DURING OIL CHANGE. FURTHER INVESTIGATION FOUND CAMSHAFT LOBES WORN PAST LIMITS AND LIFTER BODIES MISSING SOME METAL. AD 2009-24-52 PREVIOUSLY COMPLIED WITH AND LIFTER 675915 HAD BEEN REPLACED PRIOR TP PRIOR "0" TIME O/H PERFORMED 468.2 Nov 17, 2010 · N994RA · Cessna 210M · Reciprocating Engine Power SectionSDR 2010FA0001157Cylinder Head · crackedDURING AN ANNUAL/100HR INSP FOUND 4 OUT OF THE 6 CYLINDER HEADS CRACKED, THEY ARE ECI CYLINDERS WITH PN TIST71.4, SN'S 38519-08, 38542-17, 38947-18, 38947-30.Oct 21, 2010 · N6035N · Cessna 210M · Reciprocating Engine Cylinder SectionSDR 2010FA0001155Nut · missingTHIS ALTERNATOR, O/H WAS INSTALLED. TEST RUN-UP SHOWED NORMAL OPERATION. CHARGING SYS PROBLEMS WERE ENCOUNTERED AGAIN ON THE NEXT FLIGHT. UPON LANDING IT WAS DISCOVERED THAT THE HEX NUT ON THE ROTOR SHAFT WAS MISSING, INDICATING IMPROPER TORQUE AT UNIT O/H.Sep 20, 2010 · N5YBLG · Cessna 210M · DC Generator-AlternatorSDR 2010FA0001229Attach Bracket · crackedDURING ROUTINE ANNUAL INSP, THE RT FWD HORIZ STABILIZER ATTACH BRACKET WAS FOUND CRACKED. SB87-2 CALLS FOR KIT 210-118 TO BE INSTALLED. THE NEW FITTINGS PN 21320191 ARE BEEFED UP AND THE BULKHEAD IS ALSO. DUE TO THE CRITICAL NATURE OF THIS ATTACH FITTING, ISep 7, 2010 · N994RA · Cessna 210M · Horizontal Stabilizer, Attach FittingsSDR 2010FA0000096Torque Tube · crackedUPON LANDING, PILOT LT RUDDER TORQUE TUBE CRACKED AT PEDDLE ATTACH POINT BELOW WELD. NO EVIDENCE OF FATIGUE OR STRESS CRACKS. NOTED CLEAN FRESH BREAK.Jan 11, 2010 · N732LW · Cessna 210M · Rudder Control SystemSDR FPI2008F00000Cable · brokenMFG SERVICE KIT PN SK210174, CABLE ASSY BROKE AT THREADED END AFTER THE STOP NUT SEVEN WEEKS AFTER INSTALLATION APPEARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K)Aug 21, 2008 · N778VK · Cessna 210M · Standard Practices/StructuresSDR FPI2008F00001Cable · brokenMFG SERVICE KIT, PN SK210-174 CABLE ASSEMBLY BROKE AT THREADED END AFTER THE STOP NUT FIVE WEEKS AFTER INSTALLATION APPEARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K)Aug 14, 2008 · N8427M · Cessna 210M · Landing Gear Retraction/Extension SystemSDR 2008FA0000349Torque Link · crackedOUR REPAIR STATION HAS REPLACED SEVERAL OF THESE SAME UPPER TORQUE LINKS DUE TO FINDING THEM BENT AT INSPECTION (APPROX 5 TOTAL) THIS IS THE FIRST ONE FOUND CRACKED. PROBABLE CASUE IS WHAT I BELIEVE IS LANDING IMPACT WITH MORE THAN RECOMMENDED STRUT ESTENSIONMay 2, 2008 · N70HG · Cessna 210M · Nose/Tail Landing GearSDR 2006FA0000760Snap Ring · failed2 SNAP RINGS FAILED ON PROPELLAR BLADES. (K)Aug 2, 2006 · N965B · Cessna 210M · Propeller Blade SectionSDR N6265BBulkhead · crackedWHILE UNDERGOING AN ANNUAL INSPECTION, FOUND THE FIREWALL TO BE CRACKED ON THE LT & RT SIDE WHERE THE P/N 1250255-7 EXHAUST HANGAR BRACKETS ATTACH. THE CRACKS WERE EXTENDING OUT FROM UNDER THE HANGAR BRACKETS AND EXTENDED IN MULTIPLE DIRECTIONS. ADDITIONAL INSMay 24, 2006 · N6265B · Cessna 210M · Fuselage Main, BulkheadSDR 2006FA0000672Diode · inoperativeDURING LANDING, FORGOT TO EXTEND THE LANDING GEAR AND GEAR UP LANDING WAS CARRIED OUT. ACCIDENT INVESTIGATION INCLUDED A SATISFACTORY OPS CHECK OF LANDING GEAR RETRACTION/EXTENSION SYSTEM, BUT WARNING HORN FAILED TO OPERATE. AFTER DISASSEMBLING THE WARNING UJan 4, 2006 · Cessna 210M · Landing Gear Position and WarningSDR S3692Wheel · separatedTWO BOLTS IN RT MAIN WHEEL INNER FLANGE, BROKE ON LANDING, CAUSING WHEEL INNER FLANGE AND BRAKE DISC TO PARTIALLY SEPARATE FROM WHEEL HUB AND RUB INTO MAIN GEAR AXLE FITTING. MOUNTING BOLT HOLES IN BRAKE DISC SHOW SOME ELONGATION, POSSIBLY DUE TO LOOSE BOLTS Aug 25, 2005 · N761K · Cessna 210M · Wheel/Ski/FloatSDR 2005FA0000969Impulse Coupling · wornMAGS REMOVED FOR TROUBLESHOOTING OF ENGINE HIGH ALTITUDE OPERATION PROBLEM. DURING PREINSTALLATION INSPECTION OF COUPLINGS. ONE WAS FOUND WORN BEYOND LIMITS. (K)Jun 28, 2005 · N6175N · Cessna 210M · Magneto/DistributorSDR CCJ2005F00000Bracket · brokenTHERE WAS NO (GEAR DOWN) INDICATION WHEN THE LANDING GEAR WAS EXTENDED. PILOT DECLARED EMERGENCY AND DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY. LANDING WAS NORMAL AND UNEVENTFUL. UPON EXAMINATION IT WAS FOUND THAT THE BRACKET HOLDING THE NOSE GEAR (DOWN) Apr 13, 2005 · N6035N · Cessna 210M · Main Landing GearSDR AUS20040361Hose · loose(AUS) ENGINE FUEL HOSE LEAKING AT CONNECTION TO CHECK VALVE. FUEL LEAKING INTO ENGINE BAY. HOSE HAD NOT BEEN TIGHTENED DURING MAINTENANCE. PERSONNEL/MAINTENANCE ERROR.May 1, 2004 · Cessna 210M · Engine Fuel DistributionSDR 2004FA0000316Wire · shortedTHE 3 WIRES COMING FROM THE STATOR ARE SHORTED OUT ON THE CASE. THIS IS 4TH ALTERNATOR OVERHAUL BY FACILITY WITH THE SAME FAILURE, ALL 4 ALTERNATORS HAD LESS THAN 390 HOURS SINCE OVERHAUL. THERE NEED TO BE MORE INSULATION ON THE 3 WIRES.Apr 8, 2004 · N761SP · Cessna 210M · DC Generator-AlternatorSDR AUS20040077Wire Harness · burned(AUS) WIRING LOOM CHAFED AND BURNED BY ELEVATOR COUNTERWEIGHT.Feb 5, 2004 · Cessna 210M · Electrical Power System WiringSDR 2004FA0000202Wire · brokenAIRCRAFT LANDED WITH NO ELECTRICAL POWER. REPAIRED DAMAGED ALTERNATOR PRIMARY WIRE AND RESOLDERED CAPACITOR WIRE. TOP CHARGED BATTERY. OPS CHECKED GOOD IAW MFG C210 AMM AND AC43-1B/2A CHAPTER 11-7.Feb 3, 2004 · N732PY · Cessna 210M · Electrical Power System WiringSDR AUS20040062Hose · failed(AUS) NOSE LANDING GEAR DOOR ACTUATOR HOSE FAILED. LOSS OF HYDRAULIC FLUID.Jan 16, 2004 · Cessna 210M · Hydraulic System, MainSDR 2004FA0000319Fuel Line · corrodedFRONT FUEL LINE FROM LT WING TANK WAS IN CONTACT WITH FRESH AIR DUCT IN THE WING, AERO DUCT PN CEET 1.5 INCH. THIS CAUSED CORROSION ON THE ALUMINUM FUEL LINE. PROBLEM WAS FOUND WHEN FUEL STARTED LEAKING OUT OF THE WING. REPLACED FUEL LINE AND FRESH AIR DUCTDec 4, 2003 · N761AN · Cessna 210M · Aircraft Fuel Distribution SystemSDR XVQ2003F00000Bearing · failedAIRCRAFT WAS FORCED TO MAKE A GEAR UP LANDING, DAMAGING PROP AND ENGINE. THE CAUSE WAS FOUND TO BE THE FAILURE OF A BEARING/WHEEL ASSEMBLY THAT ACTUATES THE NOSE GEAR DOORS CLOSING MECHANISM. THE BEARING FAILED ALLOWING THE WHEEL PORTION TO SHIFT OUTBOARD EXNov 20, 2003 · N823AR · Cessna 210M · Nose/Tail Landing Gear Strut/AxleSDR AUS20031032Hub · cracked(AUS) PROPELLER HUB CRACKED IN AREA OF FOURTH THREAD AT THE 2 O'CLOCK POSITION. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).Sep 15, 2003 · Cessna 210M · Propeller Hub SectionSDR CXU2003F00000Accumulator · failedEND PLUG IN HYDRAULIC ACCUULATOR DEPARTED RELEASING HYDRAULIC FLUID AND PRESSURE. AIRCRAFT TACH READS 3679.2.Mar 27, 2003 · N965B · Cessna 210M · Landing Gear Door Retract SectionSDR AUS20030262Downlock Switch · sticking(AUS) RT MAIN LANDING GEAR DOWNLOCK SWITCH STUCK. RT LANDING GEAR COLLAPSED ON LANDING.Feb 24, 2003 · Cessna 210M · Landing Gear Position and WarningSDR AUS20030009Tube · corroded(AUS) LANDING GEAR ACCUMULATOR LINE CONTAINED A SMALL CORROSION PINHOLE. LOSS OF HYDRAULIC FLUID.Jan 3, 2003 · Cessna 210M · Landing Gear Retraction/Extension SystemSDR FPI2003F00000Line · chafedLANDING GEAR DOWN LINE CHAFED THRU BY AILERON RUDDER INTERCONNECT CABLE. WHEN SELECTING DOWN, ALL FLUID WAS PUMPED OUT OF SYSTEM. NOSE GEAR CAME DOWN AND LOCKED, MAIN GEAR DID NOT.Dec 16, 2002 · N7660E · Cessna 210M · Hydraulic System, MainSDR AUS20021162Switch · faulty(AUS) LT MAIN LANDING GEAR DOWN SWITCH INTERMITTENT IN OPERATION.Oct 15, 2002 · Cessna 210M · Landing Gear Position and WarningSDR AUS20020340Bracket · cracked(AUS) LH REAR HORIZONTAL STABILISER ATTACHMENT BRACKET CRACKED.Mar 29, 2002 · Cessna 210M · Fuselage, Stabilizer Attach FittingsSDR AUS20020345Fitting · faulty(AUS) LH WING ATTACHMENT FITTING CONTAINED A SUBSURFACE DEFECT IN THE AREA ADJACENT TO BUT NOT INTO THE MAIN WING ATTACHMENT BOLT HOLE. FOUND DURING EDDY CURRENT INSPECTION.Mar 3, 2002 · Cessna 210M · Wing, Fuselage Attach FittingsSDR 20000808SH015Mount · missingPART MANUFACTURED DEFECT. MISSING REINFORCEMENT WASHER ON UPPER HALF. (X)Jul 27, 2000 · N7660E · Cessna 210M · Engine Mount SectionSDR 20000626SH011Alternator · looseFOUND GROUND STUD TO BE LOOSE ON BACK OF ALTERNATOR. (X)Jun 26, 2000 · N761PS · Cessna 210M · Alternator-Generator DriveSDR AU000024Contactor · faulty(AUS) MAGNETO CONTACT SET FAULTY.Jan 14, 2000 · Cessna 210M · Magneto/DistributorSDR 99ZZZX4139Spark Plug · mismanufacturedUPON INSPECTION OF PLUGS, FOUND PLUGS, 4 EACH, TO TEST WEAK AND NOT APPROPRIATE FOR INSTALLATION ON AIRCRAFT. NOTE: BY DOM AIR CARRIERS, ONE OF THE FOUR SPARK PLUGS HAD A RED DISCOLORATION AT BASE OF ELECTRODE AND CERAMIC. LOT NR 4G99.Sep 30, 1999 · N761PS · Cessna 210M · Spark Plug/IgniterSDR 99ZZZX4138Spark Plug · mismanufacturedINSTALLED NEW PLUGS IN ENGINE. PERFORMED RUN-UP. OPS OK. FOUR HOURS LATER, ENGINE HAD A 600 RPM DROP. REMOVED SPARK PLUGS, FOUND A PIECE OF WIRE AROUND CENTER ELECTRODE OF 3 PLUGS AND 4 OTHER PLUGS NOT FIRING VERY HOT ON PLUG TESTER. OPENED ANOTHER SET OF Sep 29, 1999 · N9163M · Cessna 210M · Spark Plug/IgniterSDR 99ZZZX4137Spark Plug · mismanufacturedSPARK PLUGS WERE REPLACED BECAUSE OF WEAR. UPON INSPECTION OF NEW PLUGS, FOUND WIRE WRAPPED AROUND CENTER ELECTRODE ON TWO OF THE NEW PLUGS (WHICH GROUNDED IT OUT) AND ANOTHER SIX WOULD NOT TEST GOOD IAW CHAMPION TEST PROCEDURES. OBTAINED ANOTHER NEW SET OFSep 29, 1999 · N9163M · Cessna 210M · Spark Plug/IgniterSDR AU990682Bearing · failed(AUS) CRANKSHAFT BEARING FAILED. THE BEARING FELL OUT OF THE SUMP PLUG HOLE DURING ENGINE OIL DRAIN. LIMITED INFORMATION PROVIDED.Jun 16, 1999 · Cessna 210M · Reciprocating Engine Power SectionSDR 99ZZZX2724Bracket · crackedTHE BRACKET IS THE RUDDER BOTTOM ATTACH POINT. INTERGRANULAR CORROSION EXTENDING THROUGH THE RIVETS AND SPLITTING THE SEAM. PICTURES PROVIDED.Jun 1, 1999 · N1781M · Cessna 210M · Rudder, Spar/Rib
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