Cessna 210M

Service difficulty reports · 94

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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 = '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 99ZZZX2723Bracket · crackedTHE BRACKET IS THE RUDDER TOP ATTACH POINT. CORROSION APPEARS TO HAVE STARTED BETWEEN THE ATTACH POINT BRACKET AND THE AFT SPAR. EVENTUALLY CRACKING THE SPAR AND BRACKET.Jun 1, 1999 · N1781M · Cessna 210M · Rudder, Spar/RibSDR 99ZZZX2433Bracket · crackedDURING ROUTINE PHASE INSPECTION, HEARD SQUEEKING NOISE FROM TAIL. REMOVED PANELS, INSPECTED, FOUND TWO BRACKETS CRACKED. CAUSE UNKNOWN.May 26, 1999 · N778VK · Cessna 210M · Horizontal Stabilizer StructureSDR 99ZZZX2432Fitting · crackedDURING ROUTINE PHASE INSPECTION, HEARD SQUEEKING NOISE FROM TAIL. REMOVED PANELS, INSPECTED, FOUND TWO BRACKETS CRACKED. CAUSE UNKNOWN.May 26, 1999 · N778VK · Cessna 210M · Horizontal Stabilizer StructureSDR AU990376Lifter · worn(AUS) NR 4 CYLINDER EXHAUST VALVE LIFTER DAMAGED DUE TO BREAKING AWAY OF THE HARD FACING ON THE BOTTOM OF THE LIFTER. INVESTIGATION FOUND SIMILAR DAMAGE ON NR 1 CYLINDER EXHAUST VALVE LIFTER, NR 5 CYLINDER INLET AND EXHAUST VALVE LIFTERS, AND, NR 2 CYLINDER EXApr 12, 1999 · Cessna 210M · Reciprocating Engine Power SectionSDR 99ZZZX123Cylinder · crackedCOMRPESSION TEST REVEALED NR 1 CYLINDER 30/80, NR 5 CYLINDER 52/80, AND NR 6 CYLINDER 42/80. UPON APPLICATION OF LEAK DETECTOR LIQUID, CRACKS WERE FOUND IN ALL THREE CYLINDER HEADS.Dec 8, 1998 · N761PS · Cessna 210M · Reciprocating Engine Cylinder SectionSDR 99ZZZX122Cylinder · crackedCOMPRESSION TEST REVEALED 71/80 FOR NR 1 CYLINDER AND 25/80 FOR NR 2 CYLINDER. UPON APPLICATION OF LEAK DETECTOR LIQUID, A CRACK WAS FOUND IN NR 1 CYLINDER ADJACENT TO INTAKE PORT BETWEEN 16TH AND 17TH FIN. CRACK EXTENDS FROM EXHAUST VALVE TO SPARK PLUG HOLEDec 8, 1998 · N732QA · Cessna 210M · Reciprocating Engine Cylinder SectionSDR 99ZZZX121Cylinder · crackedCOMPRESSION TEST REVEALED 71/80 FOR NR 1 CYLINDER AND 25/80 FOR NR 2 CYLINDER. UPON APPLICATION OF LEAK DETECTOR LIQUID, A CRACK WAS FOUND IN NR 1 CYLINDER ADJACENT TO INTAKE PORT BETWEEN 16TH AND 17TH FIN. CRACK EXTENDS FROM EXHAUST VALVE TO SPARK PLUG HOLEDec 8, 1998 · N732QA · Cessna 210M · Reciprocating Engine Cylinder SectionSDR 99ZZZX120Cylinder · crackedCOMPRESSION TEST REVEALED 64/80 FOR NR 6 CYLINDER. USED LEAK DETECTOR LIQUID TO DETECT CRACK ADJACENT TO EXHAUST PORT BETWEEN 18TH AND 19TH FIN.Dec 8, 1998 · N9163M · Cessna 210M · Reciprocating Engine Cylinder SectionSDR 98ZZZX3669Pump · failedUNIT WOULD NOT PRODUCE PRESSURE TO TURN OFF PUMP. REMOVED AND SENT FOR OVERHAUL. INSTALLED SAME BACK IN AFTER OVERHAUL. REMOVED UNIT AND SENT FOR EXCHANGE. THIS OVERHAUL UNIT INSTALLED AND WORKED NORMALLY. AIRCRAFT RETURNED TO SERVICE.Sep 2, 1998 · N6554B · Cessna 210M · Hydraulic Pump (Electric/Engine), MainSDR 98ZZZX3668Pump · failedAIRCRAFT BROUGHT IN FOR MAINTENANCE. FOUND PUMP MOTOR CONTINUING TO RUN. TROUBLESHOOTING REVEALED THAT UNIT WOULD NOT PRODUCE PROPER PRESSURE TO TRIP PRESSURE SWITCH. REMOVED AND INSTALLED OVERHAULED UNIT. SYSTEM OPS NORMAL.Sep 2, 1998 · N732QA · Cessna 210M · Hydraulic Pump (Electric/Engine), MainSDR AU980710Link · cracked(AUS) NOSE LANDING GEAR UPPER TORQUE LINK CRACKED. CRACKS APPEAR TO ORIGINATE FROM CORROSION PITTING. PART TOTAL CYCLES: 5,150.Jun 23, 1998 · Cessna 210M · Landing Gear Retraction/Extension SystemSDR AU980660Hose · burnt(AUS) FLEXIBLE OIL SUPPLY LINES TO TURBOCHARGER AND OIL PRESSURE HOSE BURNT DUE TO BEING ROUTED UNDER THE REAR EXHAUST PIPE. ONE HOSE HAD BEEN BURNT SUFFICIENTLY FOR OIL LEAKAGE TO OCCUR.May 15, 1998 · Cessna 210M · Reciprocating Engine Oil SystemSDR 98ZZZX2277Circuit Breaker · failedWHILE EN ROUTE, LOST COMPLETE ELECTRICAL POWER IN TOTAL IFR CONDITIONS WITH ZERO VISIBILITY. PWM MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT DEPARTED AND THE SAME CONDITION OCCURRED AGAIN. THE CIRCUIT BREAKER WAS REPLACED AND THE CONDITION WAS NEVApr 8, 1998 · N1943M · Cessna 210M · DC Generating SystemSDR 98ZZZX1599Switch · defectiveIGNITION SWITCH, MODEL A-510. KEY CAN BE REMOVED AND FALLS OUT IN ALL POSITIONS. RECOMMEND RE-PUBLISHING WARNING FOR MECHANICS TO CHECK FOR THIS CONDITION AT EVERY INSPECTION.Apr 2, 1998 · N6265B · Cessna 210M · Ignition SwitchingSDR AU980441Lever · broken(AUS) ENGINE THROTTLE CONTROL LEVER BROKEN AT STEEL BUSH INSERT END.Mar 31, 1998 · Cessna 210M · Fuel Control/Reciprocating EnginesSDR AU980338Housing · damaged(AUS) FUEL MANIFOLD VALVE HOUSING DAMAGED IN SEAL RETAINING AREA ALLOWING FUEL TO LEAK PAST THE SEAL.Mar 30, 1998 · Cessna 210M · Fuel Controlling SystemSDR AU980322Bulkhead · cracked(AUS) FUSELAGE LOWER CENTER SECTION FRAME/BULKHEAD CRACKED. THE MAIN CRACKING WAS FROM THE OUTBOARD CUTOUT FOR THE RT MAIN LANDING GEAR LEG. CRACKING WAS ALSO COMMENCING ON THE OPPOSITE CUTOUT AND ALSO ON THE OUTER EDGE WHERE THE OUTBOARD CASTING BOLTS TO THMar 20, 1998 · Cessna 210M · Fuselage Main, BulkheadSDR CA980325031Cylinder · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. INSPECTION FOUND THE CYLINDER OVERSIZE AND THE HUB CORRODED. THE HUB WAS NOT ANODIZED, NOR WAS THE PROPELLER MODIFIED TO OIL FILLED AS PER SERVICE BULLETIN 196A.Mar 18, 1998 · Cessna 210M · Propeller Hub SectionSDR AU980139Engine · vibration(AUS) ENGINE VIBRATION FELT THROUGH FLOOR AND RUDDER PEDALS.Feb 9, 1998 · Cessna 210M · Engine (Reciprocating)SDR 98ZZZX100Magneto · failedRIGHT MAGNETO DEAD. OPENED MAG, FOUND COPPER AND CARBON DUST EVERYWHERE. FOUND BLOCK AND GEAR BEARINGS WORN SEVERELY AND GEAR DAMAGED, TEETH VERY SHARP DUE TO MISALIGNMENT OF LARGE GEAR. MAGS WERE NOT INSPECTED AT 500-HOUR INSPECTION AS RECOMMENDED.Dec 14, 1997 · N6831M · Cessna 210M · Magneto/DistributorSDR 97ZZZX5137Adapter · failedAS PART OF THE 600-HOUR INSPECTION OF OIL FILTER ADAPTER REQUIRED BY SEB 93-1R1, THE RELIEF VALVE SEALING 'DISK' WAS FOUND ASKEW AND NOT SEALING PROPERLY. FURTHER INSPECTION REVEALED THE SPRING THAT HOLDS THE 'DISK' IN PLACE HAD BEEN CHAFED MORE THAN HALFWAY Dec 2, 1997 · N6175N · Cessna 210M · Reciprocating Engine Oil SystemSDR AU971339Fitting · failed(AUS) HORIZONTAL STABILISER RH FORWARD ATTACHMENT FITTING FAILED AND SEPARATED.Oct 23, 1997 · Cessna 210M · Horizontal Stabilizer, Attach FittingsSDR 97ZZZX4651Link · brokenDURING A DISASSEMBLY INSPECTION OF PROPELLER LINK, THE BLADE ACTUATING ON THE NR 2 BLADE WAS BROKEN AT THE .4375 INCH BLADE BUTT ATTACH POINT AND THE CHROME PLATING ON THE BLADE PITCH FITTING WAS DETERIORATED AND SHOWED EXTENSIVE PITTING. SUSPECT POSSIBLE FAILSep 13, 1997 · N761VX · Cessna 210M · Propeller Blade SectionSDR AU970705Cylinder · cracked(AUS) ENGINE CYLINDER CRACKED BETWEEN TOP SPARK PLUG HOLE AND INJECTOR NOZZLEMay 10, 1997 · Cessna 210M · Reciprocating Engine Cylinder SectionSDR AU970704Cylinder · cracked(AUS) ENGINE CYLINDER CRACKED BETWEEN TOP SPARK PLUG HOLE AND INJECTOR NOZZLE - SUSPECT CYLINDER HAD BEEN WELD REPAIREDMay 10, 1997 · Cessna 210M · Reciprocating Engine Cylinder SectionSDR AU970703Cylinder · worn(AUS) NO6 CYLINDER FUEL INJECTOR NOZZLE HOLE WORN OUTMar 26, 1997 · Cessna 210M · Reciprocating Engine Cylinder SectionSDR AU970231Cylinder · stripped(AUS) ENGINE CYLINDER HEAD FUEL NOZZLE RETAINING THREADS STRIPPED - FUEL NOZZLE LOOSE - CYLINDER IS 0.0015IN PLUS OVERSIZE WITH UNKNOWN TOTAL TIME IN SERVICE - AD/CON/60 CARRIED OUT 50 HOURSPRIOR TO FAILUREMar 16, 1997 · Cessna 210M · Reciprocating Engine Cylinder SectionSDR AU970130Hub · cracked(AUS) PROPELLER HUB CRACKED IN NO2 BLADE SOCKET AREA - CRACK LENGTH APPROXIMATELY 6.35MM (0.25IN) - FOUND DURING INSPECTION IAW AD/PMC/41 FOLLOWING WIRE STRIKEFeb 18, 1997 · Cessna 210M · Propeller Hub SectionSDR 96ZZZX5007Bracket · separatedTHROTTLE BODY SUPPORT BRACKET FOUND SEPARATED AT ANNUAL INSPECTION. TIS: 156.5 HOURS, SEPARATED AT SPOT WELDS.Sep 18, 1996 · N9489M · Cessna 210M · Fuel Control/Reciprocating EnginesSDR 96ZZZX4084Wheel · failedWHEEL ASSY BLEW APART ON TAXI ON BRAKE DISC SIDE. SUSPECT CAUSE, WEAK THREADS ON 12-BOLT, 3-PIECE MCCAULEY WHEEL ASSY. REPLACED WHEEL ASSY WITH 2-PIECE, CLEVLAND.Jul 20, 1996 · N8427M · Cessna 210M · Wheel/Ski/FloatSDR AU960961Spring · broken(AUS) ENGINE OIL FILTER ADAPTER PNO 1250921-1 BYPASS SPRING BROKEN INTOTHREE PIECES - VALVE CAP PNO 0756022-1 FOUND ON OIL PRESSURE RELIEF VALVE SEAT - FURTHER INSPECTION FOUND SPRINGS ON TWO OTHER AIRCRAFT BADLY WORNJul 12, 1996 · Cessna 210M · Reciprocating Engine Oil SystemSDR AU960903Pipe · cracked(AUS) BRAKE PIPE FAILED AT FLARE - LOSS OF HYDRAULIC FLUID CAUSED BRAKE FAILURE ALLOWING AIRCRAFT TO RUN OFF AIRSTRIP AND DAMAGE PROPELLER - SUSPECT CAUSED BY ROCKS ON LANDING STRIPJun 18, 1996 · Cessna 210M · Landing Gear Brake SystemSDR 97ZZZX1169Switch · failedLANDING GEAR WOULD NOT EXTEND WHEN SELECTOR SWITCH WAS PLACED IN THE DOWN POSITION. AIRCRAFT PLACED ON JACKS TO TROUBLESHOOT GEAR SYSTEM. RIGHT MAIN GEAR UPLOCK MICROSWITCH FOUND DEFECTIVE. REPLACED S1377-1 MICROSWITCH, AND RIGGED. OPERATIONAL CHECK, GOOD.Jun 13, 1996 · N6265B · Cessna 210M · Landing Gear Retraction/Extension SystemSDR 96ZZZX3331Lifter · chippedWHILE CLEANING-INSPECTING LIFTER FOR REINSTALLATION, FOUND CAMSHAFT FACE OF LIFTER CHIPPED.Jun 12, 1996 · N732LW · Cessna 210M · Reciprocating Engine Power SectionSDR EY2R9601504Retain Ring · bentPROP ASSY RETAIN RING IS BENTMay 1, 1996 · Cessna 210M · Propeller AssemblySDR EY2R9600642Dowel · corrodedDOWEL CORRODED.May 1, 1996 · Cessna 210M · Propeller AssemblySDR 96ZZZX2981Line · chafedROUTINE MAINTENANCE, NOTICED FUEL DRIPPING ONTO FLAP HANDLE WIRING BEHIND INSTRUMENT PANEL. INVESTIGATION FOUND LINE CHAFING ON ADF RADIO RACK. THIS LINE RUNS FROM FIRE WALL TO FUEL PRESSURE GAUGE. TOTAL TIME ON AIRFRAME 11,404 HRS. TT ON PART, UNKNOWN.Apr 24, 1996 · N823AR · Cessna 210M · Fuel Indicating SystemSDR AU960297Nut · cracked(AUS) ENGINE CYLINDER HOLD DOWN NUT CRACKEDFeb 13, 1996 · Cessna 210M · Reciprocating Engine Power SectionSDR 96ZZZX2397Elevator Edge · corrodedDURING INSPECTION PRIOR TO PAINTING, FOUND CORROSION ON INBOARD LOWER SURFACE OF ELEVATOR TRAILING EDGE. TWO HOLES APPROXIMATELY .125 INCH DIAMETER ALONG WITH SMALLER PIN HOLES WERE FOUND. SUSPECT CAUSE, FOAM IN TRAILING EDGE RETAINING WATER INSIDE TRAILING Jan 25, 1996 · N761AQ · Cessna 210M · Elevator, Plate/SkinSDR 95ZZZX6544Trim Tab · corrodedTHERE IS EXCESSIVE CORROSION ON THE ELEVATOR TRIM TAB. THERE ARE PIN HOLES THROUGH THE METAL ON TOP AND LOWER PORTION OF TRIM TAB NEAR THE TRIM TAB ACTUATOR ATTACH POINT. SUBMITTER STATED THIS IS A VERY SERIOUS CONDITION.Nov 13, 1995 · N732PW · Cessna 210M · Elevator, Tab StructureSDR 96ZZZX173Downlock Hook · wornDURING ANNUAL INSPECTION, EXCESS PLAY WAS NOTICED IN MLG WHEN ON JACKS. MLG DOWNLOCK HOOKS WERE FOUND WORN AT PIVOT POINT. REPLACED WITH SERVICEABLE HOOKS AND REPLACED ATTACHING PINS (MS 20392 CLEVIS PINS).Oct 18, 1995 · N761GK · Cessna 210M · Landing Gear Retraction/Extension SystemSDR 96ZZZX164Control Wheel · corrodedDURING ANNUAL INSPECTION, FOUND CORROSION ON PILOT CONTROL WHEEL. REMOVED WHEEL AND INSPECTED CORROSION. CORROSION HAD REMOVED METAL FROM THE FOLLOWING AREAS: AROUND BOTH LOWER BOLT HOLES AT BASE OF LT GRIP, AND AROUND MAP LIGHT OPENING. SUBMITTER STATED IOct 18, 1995 · N761GK · Cessna 210M · Control Column SectionSDR 95ZZZX5229Bracket · brokenINSPECTION FOUND BRACKET FOR THROTTLE AND MIXTURE CONTROL MOUNT BROKEN.May 17, 1995 · N9036M · Cessna 210M · Mixture ControlSDR 95ZZZX2691Bracket · brokenTHE BRACKET ON WHICH THROTTLE CONTROL AND MIXTURE CONTROL CABLES ARE ATTACHED WAS FOUND BROKEN.May 17, 1995 · N9036M · Cessna 210M · Power Lever
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