Cessna 210N

Service difficulty reports · 111

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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 = '210N'
  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 99ZZZX2437Camshaft · chippedDURING A ROUTINE 100-HOUR INSPECTION EXCESSIVE METAL WAS FOUND IN THE ENGINE OIL FILTER. FURTHER INVESTIGATION REVEALED A CHIPPED CAM LOBE AND LIFTER.May 10, 1999 · N961CC · Cessna 210N · Reciprocating Engine Power SectionSDR AU990511Seal · missing(AUS) ALL INLET VALVE SEALS MISSING. OIL LEAKING FROM MANIFOLD DRAINS. THE ENGINE WAS COMPLETING GROUND RUNS FOLLOWING INSTALLATION OF AN OVERHAULED ENGINE. SEVERAL OTHER DEFECTS WERE FOUND DURING THE INVESTIGATION OF THE OIL LEAKAGE. THESE DEFECTS WERE: Apr 28, 1999 · Cessna 210N · Reciprocating Engine Cylinder SectionSDR AU990476Trim Tab · corroded(AUS) ELEVATOR TRIM TAB CORRODED AND DAMAGED DUE TO FOD. THE TRIM TAB HAD ALSO BEEN REPAIRED AT SOME TIME PREVIOUSLY DUE TO TIP DAMAGE.Apr 20, 1999 · Cessna 210N · Elevator, Tab StructureSDR AU990475Collector · cracked(AUS) LEFT EXHAUST COLLECTOR CRACKED ALONG EXHAUST STUB SLIP JOINT. THE COLLECTOR HAD BEEN ILLEGALLY WELD REPAIRED. UNAPPROVED REPAIR.Apr 20, 1999 · Cessna 210N · Engine Collector/Tailpipe/NozzleSDR AU990469Cylinder · cracked(AUS) ENGINE CYLINDERS CRACKED. ALL VALVES, PISTONS, PISTON RINGS AND VALVE GUIDES WORN BEYOND LIMITS. INVESTIGATION FOUND THAT NR 2 AND NR 3 CYLINDERS HAD BEEN RELEASED BELOW MINIMUM LIMITS PER AAC 6-32 AMDT1. FOUND DURING INSPECTION IAW AD/ENG/4 AMDT7 PApr 20, 1999 · Cessna 210N · Reciprocating Engine Cylinder SectionSDR AU990468Bolt · seized(AUS) NOSE LANDING GEAR ACTUATOR TO FUSELAGE ATTACHMENT FITTING BOLT SEIZED. WHEN THE BOLT WAS REMOVED , IT WAS FOUND THAT THE BOLT WAS SEVERELY CORRODED. THE BOLT WAS ALSO THE INCORRECT PART NUMBER. THE IPC INDICATES THAT AN `AN' TYPE BOLT SHOULD BE USEApr 20, 1999 · Cessna 210N · Landing Gear Retraction/Extension SystemSDR AU990467Disc · cracked(AUS) LEFT BRAKE DISC CRACKED IN TWO PLACES ALONG THE FLANGE WHERE IT MEETS THE BRAKE DISC BODY. THE CRACKS HAD BEEN IN THE BRAKE DISC FOR AN EXTENDED PERIOD OF TIME AND THE DISC WAS CLOSE TO FAILURE.Apr 20, 1999 · Cessna 210N · BrakeSDR AU990466Floor Panel · corroded(AUS) FUSELAGE FLOOR CORRODED IN SEVERAL AREAS. SUSPECT CAUSED BY LEAKING SIDE WINDOWS ALLOWING WATER TO ENTER AND SOAK INTO THE CARPET WHICH HAD BEEN DAMP FOR A LONG PERIOD. AIRCRAFT ALSO OPERATES IN A SALT AIR ENVIRONMENT.Apr 20, 1999 · Cessna 210N · Fuselage Floor PanelSDR AU990465Rod End · misinstalled(AUS) NOSE LANDING GEAR DOOR ARM ROD ENDS INSTALLED 180 DEGREES OUT ALLOWING THE DOORS TO FOUL ON THE NACELLE LOWER SKIN IN THE FULL DOWN POSITION. WHEN THE DOORS WERE ADJUSTED TO WITHIN LIMITS, IT WAS FOUND THAT THE DOOR LOCATOR PINS WERE ALSO MISALIGNED.Apr 20, 1999 · Cessna 210N · Landing Gear Door Retract SectionSDR AU990464Downlock · out of adjust(AUS) MAIN LANDING GEAR DOWNLOCKS OUT OF ADJUSTMENT. DOWNLOCKS HAD NOT BEEN LUBRICATED FOR AN EXTENDED PERIOD CAUSING BINDING.Apr 20, 1999 · Cessna 210N · Landing Gear Retraction/Extension SystemSDR 99ZZZX1647Trunnion · crackedDURING INSPECTION OF NOSE GEAR LOWER TRUNNION FOR C/W CESSNA SEB 94-19, NO CRACKS WERE NOTED. EIGHTY HOURS LATER DURING REPLACEMENT OF LOWER TRUNNION FOR FINAL C/W SEB 94-19, CRACKS WERE NOTED ON BOTH SIDES OF TRUNNION AS DESCRIBED IN SEB 94-19. FAILURE OF TApr 19, 1999 · N5197C · Cessna 210N · Nose/Tail Landing Gear Attach SectionSDR AU990304Bolt · sheared(AUS) RIGHT MAIN LANDING GEAR ACTUATOR FORWARD MOUNT BOLT SHEARED.Mar 29, 1999 · Cessna 210N · Landing Gear ActuatorSDR AU990373Filter · contaminated(AUS) ENGINE OIL FILTER CONTAMINATED BY METAL. LIMITED INFORMATION PROVIDED.Mar 23, 1999 · Cessna 210N · Reciprocating Engine Oil SystemSDR AU990848Csu · failed(AUS) PROPELLER GOVERNOR (CSU) FAILED. PROPELLER REMAINED IN COARSE PITCH. STRIP INVESTIGATION FOUND EXTENSIVE DAMAGE IN GEAR POCKETS AND IDLER GEAR SHAFT. IDLER GEAR DAMAGED AND BEARING CENTER AND ROLLERS MISSING. BASE FACEPLATE SCORED AND DRIVE GEAR BMar 22, 1999 · Cessna 210N · Propeller GovernorSDR 99ZZZX1113Pump · failedWHEN ENGINE WAS BROUGHT BACK TO IDLE ON LANDING, ENGINE QUIT.Feb 23, 1999 · N6490N · Cessna 210N · Engine Fuel PumpSDR 99ZZZX1023Alternator · malfunctionedALTERNATOR KICKS OFF-LINE UNDER A LOAD OF MID TO HIGH INTENSITY AND WILL NOT COME ON-LINE UNTIL 1,500 RPM'S OR HIGHER.Jan 15, 1999 · N6585A · Cessna 210N · DC Generator-AlternatorSDR 99ZZZX1077Solenoid · failedPILOT REPORTED TOTAL ELECTRICAL FAILURE FOUND BATTERY CONTACTOR INOPERATIVE. NO POWER FROM BATTERY SWITCH TERMINAL. OPEN CIRCUIT. CONTACT LAST CHANGED ON 10-5-98. INFO ON CONTACTOR LABEL: W-4/RBM. PN 8781-9 COIL 24 VDC CONT. SN S-1580A1.Dec 30, 1998 · N4617C · Cessna 210N · Engine CrankingSDR AU981692Lifter · pitted(AUS) NR 6 CYLINDER VALVE LIFTER WAS REMOVED AND FOUND DEFECTIVE - LIFTER FACE DETERIORATING DUE TO PITTING. PART TC: 1,148.Dec 22, 1998 · Cessna 210N · Reciprocating Engine Cylinder SectionSDR 99ZZZX117Cylinder · crackedCOMPRESSION TEST REVEALED 58/80 FOR NR 2 CYLINDER. USED LEAK DETECTOR LIQUID TO DETECT CRACK ADJACENT TO EXHAUST PORT BETWEEN 16TH AND 17TH FIN. CRACK EXTENDS FROM EXHAUST VALVE TO SPARK PLUG HOLE.Dec 8, 1998 · N6585A · Cessna 210N · Reciprocating Engine Cylinder SectionSDR AU981420Regulator · malfunctioned(AUS) VOLTAGE REGULATOR SUSPECT FAULTY.Oct 29, 1998 · Cessna 210N · DC RegulatorSDR AU981423Sensor · broken(AUS) ENGINE CYLINDER HEAD TEMPERATURE PROBE BROKEN OFF SENDING UNIT.Oct 27, 1998 · Cessna 210N · Cylinder Head Temperature (CHT) Indicating SystemSDR AU981419Tire · deflated(AUS) RIGHT TIRE DEFLATED DURING LANDING. NIL DAMAGE FOUND TO THE TIRE. SUBMITTER SUSPECTED VALVE MAY HAVE BEEN DETACHED BY A STONE. THE LANDING STRIP WAS VERY ROUGH AND STONY.Oct 23, 1998 · Cessna 210N · TireSDR AU981426Lifter · damaged(AUS) HYDRAULIC EXHAUST VALVE LIFTER DAMAGED WITH SURFACE HARDENING CHIPPING AWAY. PART TC: 670.Oct 8, 1998 · Cessna 210N · Reciprocating Engine Power SectionSDR 98ZZZX4056Spring · brokenDURING ROUTINE MAINTENANCE, METAL FOUND IN OIL FILTER. TRACED TO BROKEN INNER VALVE SPRING OF NR 5 CYLINDER. BROKEN ENDS HAD STARTED TO EAT INTO CYLINDER HEAD. SUBMITTER SUGGESTED CAUSE AS METALLURIGICAL FAILURE OF SPRING STEEL. VALVE SPRINGS ARE A MANDATOROct 1, 1998 · N5HMSW · Cessna 210N · Reciprocating Engine Cylinder SectionSDR AU981115Support · cracked(AUS) HORIZONTAL STABILIZER REAR LEFT REINFORCEMENT BRACKET CRACKED IN TWO PLACES. PART TC: 3,108.Sep 1, 1998 · Cessna 210N · Horizontal Stabilizer StructureSDR AU980763Fcu · faulty(AUS) ENGINE FUEL CONTROL UNIT P/N 629703-2 AND FUEL FLOW DIVIDER P/N 631351-17A6 FITTED TO FACTORY. REMANUFACTURED ENGINE SUSPECT FAULTY.Jul 7, 1998 · Cessna 210N · Fuel Control/Reciprocating EnginesSDR AU980323Tire · damaged(AUS) LT MAIN LANDING GEAR TIRE CUT DURING LANDING ON ROUGH STRIP. TIRE DEFLATED.Mar 24, 1998 · Cessna 210N · TireSDR AU980324Magneto · faulty(AUS) LT MAGNETO FAULTY.Feb 18, 1998 · Cessna 210N · Magneto/DistributorSDR AU980574Elt · corroded(AUS) ELT CASE CRACKED AND CORRODED. MOUNTING TRAY ALSO CORRODED. INVESTIGATION FOUND SEVERAL OF THE BATTERIES EXTENSIVELY CORRODED ALONG WITH THE ELECTRICAL CONNECTOR AND MOUNTING POSTS.Feb 17, 1998 · Cessna 210N · Emergency Locator BeaconSDR AU971517Bolt · failed(AUS) NOSE WHEEL ATTACHMENT BOLT FAILED. WHEEL TWISTED IN NLG FORK. SUSPECT BROKEN BOLT.Nov 29, 1997 · Cessna 210N · Wheel/Ski/FloatSDR 97ZZZX4753Plug · brokenPART RECEIVED FROM STOCK. WHEN SCREWED INTO MASTER CYLINDER BY HAND, SIDE OF PLUG BROKE OFF. A SECOND PLUG WAS INSTALLED BY HAND AND IT BROKE IN THE SAME AREA. THESE PLUGS ARE MADE FROM BRITTLE PLASTIC AND WERE SUPPLIED BY CESSNA.Oct 29, 1997 · Cessna 210N · Master Cylinder/Brake ValveSDR 98ZZZX4462Valve Guide · wornDURING A ROUTINE COMPRESSION CHECK, LEAKAGE WAS FOUND PAST THE INTAKE VALVE ON THE NR 6 CYLINDER. THE REMOVED CYLINDER, INTAKE VALVE AND GUIDE WERE FOUND WORN OUT. THE VALVE LASH WAS ALSO FOUND TO BE EXCESSIVE ON THE NR'S 2, 4, AND 6 CYLINDERS. THE PUSH RODOct 21, 1997 · N961CC · Cessna 210N · Reciprocating Engine Cylinder SectionSDR AU970668Alternator · worn(AUS) ALTERNATOR BRUSHES WORN - SUSPECT CAUSED BY BRUSH BOUNCEJun 3, 1997 · Cessna 210N · DC Generator-AlternatorSDR AU970584Stud · loose(AUS) LH AND RH MAIN LANDING GEAR DOWNLOCK SUPPORT ASSEMBLY FORWARD RETAINING STUDS LOOSE - AIRCRAFT HAD BEEN RECENTLY REBUILT FOLLOWING AND ACCIDENT 242.3 HOURS PREVIOUSLY - PERSONNEL/MAINTENANCE ERRORMay 9, 1997 · Cessna 210N · Main Landing Gear Attach SectionSDR AU970543Control Cable · worn(AUS) ELEVATOR CONTROL CABLE WORN - CABLE HAD BEEN INCORRECTLY ROUTED OVER A PULLEY GUARD PNO NAS 427K11 ON THE PULLEY LOCATED SECOND FROM THE FRONT - AIRCRAFT HAD BEEN REBUILT 242.3 HOURS PREVIOUSLY FOLLOWING AN ACCIDENT - PERSONNEL/MAINTENANCE ERRORMay 9, 1997 · Cessna 210N · Elevator Control SystemSDR AU970463Crankcase · worn(AUS) CRANKCASE MAIN BEARING JOURNALS AND OUTER SHELL SURFACES WORN EXCESSIVELY - CRANKSHAFT CENTRE MAIN JOURNAL BADLY SCORED - SUSPECT INCORRECT LINE BORING DURING OVERHAULApr 30, 1997 · Cessna 210N · Reciprocating Engine Power SectionSDR 97ZZZX1881Seat Frame · brokenPILOT SEAT FRAME BROKEN WHERE BELLCRANK ATTACHES. SEAT P/N 0714025-39.Apr 9, 1997 · N9309Y · Cessna 210N · Flight Compartment EquipmentSDR 98ZZZX4461Valve Guide · wornDURING A ROUTINE COMPRESSION CHECK, EXCESSIVE LEAKAGE PAST THE PISTON RINGS WAS FOUND ON THE THE NR 2 CYLINDER. THE REMOVED CLYINDER WAS FOUND WORN OUT AND THE PISTON RINGS STUCK IN THE RING GROOVES. SUBMITTER SUGGESTED POSSIBLE CAUSE AS EXCESSIVE LEAD SLUDGMar 21, 1997 · N961CC · Cessna 210N · Reciprocating Engine Cylinder SectionSDR AU970297Torque Link · cracked(AUS) NOSE LANDING GEAR TORQUE LINK CRACKED ON FORWARD REINFORCING WEBSMar 20, 1997 · Cessna 210N · Nose/Tail Landing Gear Strut/AxleSDR AU970277Crankcase · defective(AUS) AT ENGINE OVERHAUL THE CRANKCASE WAS BOLTED TOGETHER AND TUNNELS WERE MEASURED OUT OF LIMITSMar 17, 1997 · Cessna 210N · Reciprocating Engine Power SectionSDR AU970227Bearing · failed(AUS) MAGNETO CAM END ROTOR BEARING FAILED - MAGNETO CONTAMINATED WITHMETAL DUSTMar 13, 1997 · Cessna 210N · Magneto/DistributorSDR AU970247Injector · blocked(AUS) NO2 CYLINDER FUEL INJECTOR NOZZLE BLOCKEDFeb 28, 1997 · Cessna 210N · Fuel Injector NozzleSDR AU970173Hose · deteriorated(AUS) VACUUM PUMP AIR HOSES DETERIORATED AND BREAKING UP INTERNALLY - FOUND DURING INSPECTION IAW CESSNA SEB 96-10Feb 18, 1997 · Cessna 210N · Vacuum Distribution SystemSDR AU970125Drive Shaft · worn(AUS) ENGINE DRIVEN FUEL PUMP DRIVE SHAFT WORN - DRIVE SHAFT ROUNDED -FEMALE END IN PUMP ALSO WORNFeb 13, 1997 · Cessna 210N · Engine Fuel PumpSDR AU970312Hose · failed(AUS) LANDING GEAR HYDRAULIC HOSE FAILED AT FITTING - SUSPECT INCORRECT HOSE FITTED - UNAPPROVED PART - PERSONNEL/MAINTENANCE ERRORFeb 11, 1997 · Cessna 210N · Hydraulic System, MainSDR AU961196Pipe · worn(AUS) ENGINE OIL PRESSURE PIPE LOCATED BETWEEN FIREWALL AND OIL PRESSURE GAUGE WORN THROUGH AND LEAKING DUE TO CHAFING BY SCAT HOSEAug 22, 1996 · Cessna 210N · Engine Oil Indicating SystemSDR AU961134Vent · damaged(AUS) RH FUEL TANK VENT LINE DAMAGED DUE TO EXCESSIVE BEND IN LINE - LINE PARTIALLY BLOCKEDAug 2, 1996 · Cessna 210N · Fuel StorageSDR AU961012Bearing · cracked(AUS) NOSE LANDING GEAR ACTUATOR BEARING END CRACKED IN AREA OF ROLL PINS AS INDICATED IN CESSNA SB95-20Jul 19, 1996 · Cessna 210N · Landing Gear ActuatorSDR AU960953Wheel · worn(AUS) RUDDER TRIM WHEEL GEAR PNO 1261471-5 AND SPROCKET PNO 1261462-1 HAD WORN TEETH - TEETH WERE WORN TO THE EXTENT THAT THE TEETH SLIPPED PAST EACH OTHER WITHOUT ACTIVATING THE CHAINJul 9, 1996 · Cessna 210N · Rudder Tab Control SystemSDR AU960775Wire · deteriorated(AUS) ALTERNATOR BATTERY WIRE DETERIORATED INTERNALLY - WIRE FRACTURED AND ARCINGJun 7, 1996 · Cessna 210N · DC Generating System
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