Cessna 210L

Service difficulty reports · 184

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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 = '210L'
  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 2020FA0000281Wire · brokenWIRE BROKE IN-BETWEEN VOLTAGE REGULATOR AND ALTERNATOR. WIRE MAY HAVE CHAFFED OR BEEN UNDER STRESS.Jun 4, 2020 · N1565X · Cessna 210L · Electrical Power System WiringSDR XGNA2020051100008Circuit Breaker · not closedPILOTS REPORTED GEAR WOULDN'T COME UP. RETURNED TO BASE WITHOUT FURTHER INCIDENT.May 10, 2020 · N2110S · Cessna 210L · Landing Gear Retraction/Extension SystemSDR XGNA2020042000005Landing Gear · intermittentIMMEDIATELY UPON ROTATION DEPARTING MQY THE GREEN GEAR INDICATOR LIGHT WENT OFF. ONCE AIRBORNE, THE PILOT TRIED TO RETRACT THE GEAR, BUT NOTHING HAPPENED. HE THEN PUT THE GEAR HANDLE IN THE DOWN POSITION BUT HE DID NOT GET A SAFE GEAR INDICATION. HE MADE A LOApr 19, 2020 · N2110S · Cessna 210L · Landing Gear Retraction/Extension SystemSDR CA190308025Cylinder · cracked(CAN) OIL NOTED ON LOWER COWLING, INSPECTION SHOWED OIL LEAKING FROM PUSHROD HOUSING ON NR 1 CYLINDER. PART REMOVED AND FOUND TO BE CRACKED AROUND 50% OF ITS CIRCUMFERENCE AT THE SPRING RETENTION FERRULE.Mar 6, 2019 · Cessna 210L · Reciprocating Engine Cylinder SectionSDR 2019FA0000055Actuator · failedLEFT LANDING GEAR FAILED TO FULLY EXTEND IN THE DOWN AND LOCKED POSITION AFTER PILOT SELECTED GEAR DOWN FOR LANDING. THE FOLLOWING STATEMENT IS FROM THE PILOT: WITH THE GEAR STILL DOWN AND THE GEAR LEVER STILL IN THE DOWN POSITION, POPPED THE GEAR PUMP CIRCUITJan 7, 2019 · N732B · Cessna 210L · Landing Gear ActuatorSDR 2017FA0000288Actuator · malfunctionedLANDING GEAR FAILED TO RETRACT AND EXTEND AFTER TAKEOFF. MLG DOOR ACTUATOR MALFUNCTIONED.Jul 17, 2017 · N732F · Cessna 210L · Landing Gear Door ActuatorSDR 2016FA0000461Hydraulic Line · failedTHE GEAR FAILED TO EXTEND AND LOCK PRIOR TO LANDING, PILOT ATTEMPTED EMERGENCY GEAR PROCEDURES (MANUAL PUMP) WHICH FAILED TO POSITION GEAR TO THE DOWN AND LOCKED POSITION. CHECK OF THE HYDRAULIC FLUID LEVEL IN RESERVOIR, THERE WAS NO READING ON THE DIPSTICK, Sep 23, 2016 · N13KS · Cessna 210L · Hydraulic System, MainSDR 2016FA0000123Cylinder · crackedNR 3 CYCLINDER BARREL CRACKED AT APPROXIMATELY 1" BELOW TOP DEAD CENTER. CRACK IS .75 PERCENT OF WAY AROUND AND DID NOT SEPARATE BARREL FROM HEAD.Mar 9, 2016 · N222SJ · Cessna 210L · Reciprocating Engine Cylinder SectionSDR CA150727016Powerpack · faulty(CAN) ON TAKEOFF WHEN THE LANDING GEAR WAS RETRACTED THE LANDING GEAR HYDRAULIC POWER PACK CONTINUED TO RUN EVERY 10 SECONDS. WHEN GEAR DOWN WAS SELECTED THE FREQUENCY OF RUN ON INCREASED. THE PILOT LANDED WITHOUT FURTHER INCIDENT AND RETURNED TO BASE FOR MAJul 21, 2015 · Cessna 210L · Hydraulic Pump (Electric/Engine), MainSDR CA150716009Pump · failed(CAN) DURING A ROUTINE LANDING, AFTER TOUCHDOWN, AS THE AIRCRAFT WAS SLOWING THE ENGINE STOPPED. THE PILOT RESTARTED THE ENGINE AND TAXIED OFF THE RUNWAY TO HIS HOME BASE WITHOUT FURTHER INCIDENT AND REPORTED TO MAINTENANCE. AFTER INSPECTING THE AIRCRAFT AND FJul 4, 2015 · Cessna 210L · Engine Fuel PumpSDR CA150716008Rib · cracked(CAN) DURING A 100 HR INSPECTION A CRACK WAS FOUND ON THE TOP SKIN OF THE L/H HORIZONTAL STABILIZER P/N 1232600-29 LEADING EDGE COMING FROM ONE OF THE RIVETS ATTACHING A LEADING EDGE RIB. FURTHER INVESTIGATION USING A BORE-SCOPE TO LOOK INSIDE THE STABILIZER FJul 4, 2015 · Cessna 210L · Horizontal Stabilizer, Spar/RibSDR 2015FA0000334Connecting Rod · failedNR 4 PISTON CONNECTING ROD FAILED AT CONNECTING ROD CAP BEARING AREA CAUSING SEPARATION OF CRANK SHAFT TO CONNECTING ROD. CRANKSHAFT REMAINED AS 1 PIECE WITH PISTON AND ROD BEING PUSHED INTO CYLINDER OUT OF WAY OF SPINNING CRANKSHAFT. NO OTHER INFORMATION AVMay 1, 2015 · N732JZ · Cessna 210L · Reciprocating Engine Power SectionSDR BSYA20140715001Battery · failedPILOT HAD A COMPLETE ELEC FAILURE AFTER TAKEOFF & RETURNED SAFELY.Jul 15, 2014 · N732CQ · Cessna 210L · Battery/Charger SystemSDR BSYA201404Unknown · malfunctionedEN ROUTE FROM BUF TO TEB, PILOT LOST ALL INTERIOR LIGHTS & NOTICED SPARKS COMING OUT OF THE INSTRUMENT PANEL. PILOT DECLARED AN EMERGENCY & DIVERTED, LANDED SAFELY AT AVP. MAINTENANCE IS INSPECTING.Feb 14, 2014 · N8WE · Cessna 210L · Flight Compartment EquipmentSDR BSYA201401Engine · power loss20 MILES FROM ADS, PILOT NOTICED LOSING POWER FROM THE ENG & STARTED FLUTTERING & MISFIRING. PILOT DECLARED AN EMERGENCY WITH ADS TOWER. PILOT WAS ABLE TO KEEP THE ENG FROM QUITTING & WAS ABLE TO RESTORE BACK TO FULL POWER. PILOT UPDATED ADS AIRPORT & WAS AJan 9, 2014 · N2137S · Cessna 210L · Engine (Reciprocating)SDR BSYR20131128001Engine · power lossEN ROUTE FROM TEB TO BUF, ENG LOST ALL POWER. PILOT ATTEMPTED TO LAND ON A ROAD, IN PROCESS, ACFT CLIPPED A POWER LINE & CRASHED NEAR SR 706 IN MONTROSE PA. PILOT WAS OK AFTER ACCIDENT & WAS TAKEN TO THE HOSPITAL TO GET CHECKED OUT. LOCAL AUTHORITIES WERE NNov 28, 2013 · N777BK · Cessna 210L · Engine (Reciprocating)SDR 2013FA0000585Restraint · cutHAD THE SEAT RESTRAIN MOD MADE TO ACFT TO KEEP SEAT FROM GOING BACKWARD IF PINS FAILS. THE RELEASE CABLE BROKE AND YOU COULD NOT RELEASE SEAT. IT WOULD ONLY GO FORWARD AND THE LOCK IN THE MORE FORWARD POSITION . TRAPPING ME IN THE SEAT. ON LANDING, I COULD NOOct 1, 2013 · N546WC · Cessna 210L · Flight Compartment EquipmentSDR BSYR201309052057Landing Gear · inoperativeON APPROACH, LANDING GEAR WOULD NOT EXTEND. PILOT PROCEEDED TO PUMP GEAR DOWN AND LOCKED AND LANDED SAFELY WITHOUT INCIDENT. MX IS INSPECTING.Sep 5, 2013 · N93111 · Cessna 210L · Landing Gear Retraction/Extension SystemSDR BSYR20130905056Alternator · abnormalAFTER TAKEOFF, PILOT NOTICED ALTERNATOR CYCLING ON AND OFF. PILOT NOTIFIED TOWER OF ISSUE AND RETURNED AND LANDED SAFELY WITHOUT INCIDENT. MX IS INSPECTING.Sep 4, 2013 · N2013S · Cessna 210L · DC Generator-AlternatorSDR BSYR20130828055Landing Gear · inoperativeON APPROACH, NOSE GEAR WOULD NOT COME DOWN WHEN EXTENDED. PILOT HAND PUMPED GEAR DOWN AND LANDED SAFELY WITHOUT INCIDENT. OPENAug 27, 2013 · N59240 · Cessna 210L · Landing Gear Retraction/Extension SystemSDR BSYR20130723054Landing Gear · malfunctionedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. PILOT RETURNED AND LANDED SAFELY WITHOUT INCIDENT. OPENJul 22, 2013 · N274CS · Cessna 210L · Landing Gear Retraction/Extension SystemSDR BSYR20120515048Alternator · failedEN ROUT FROM MLS TO BIL, PILOT EXPERIENCED ALTERNATOR FAILURE APPROXIMATELY 20 MINUTES AFTER DEPARTING. ATC WAS NOTIFIED AND PILOT PROCEEDED TO BIL AND LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE IS INSPECTING.May 14, 2013 · N59141 · Cessna 210L · DC Generator-AlternatorSDR BSYR20120503046Indicator · out of toleranceFLIGHT DEPARTED OMA FOR DSM, JUST AFTER AIRCRAFT LEVELED OFF THE AIRSPEED INDICATOR QUIT WORKING. PILOT DECLARED AN EMERGENCY AND CONTINUED TO DSM. PILOT SAID HALF WAY INTO FLIGHT AIRSPEED INDICATOR STARTED WORKING. PILOT LANDED SAFELY AT DSM WITHOUT INCIDEMay 2, 2013 · N59240 · Cessna 210L · Airspeed/Mach IndicatorSDR 5RJR2013020811562Crankcase · contaminatedACFT ON RAMP OVERNIGHT 0-10 FARENHEIT. OPERATOR HAD HARD TIME STARTING ENGINE. AIRCRAFT WARMED UP. LATER STARTED NORMAL. CREW TOOK OFF NORMAL. ABOUT 15-20 MINUTES INTO CRUISE, CREW FELT A SHUTTER IN CONTROLS & RUDDER PEDALS, ENGINE STUMBLING WORSENED. ACJan 25, 2013 · N732BC · Cessna 210L · Reciprocating Engine Oil SystemSDR FPI2012F00011Cylinder Head · crackedDURING 100 HR INSPECTION, COMPRESSION TEST, LEAK CHECK WITH SOAPY WATER FOUND A CRACK IN CYLINDER HEAD FROM TOP OF SPARK PLUG HOLE TO INTAKE VALVE. REPLACED WITH NEW CYLINDER ASSY.Jun 29, 2012 · N2437S · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2012F00010Cylinder · leakingDURING A 100 HOUR INSPECTION, COMPRESSION TEST LEAK CHECK WITH SOAPY WATER, A CRACK WAS FOUND AT FIRST FIN, INTO COMBUSTION CHAMBER. REPLACED WITH NEW CYLINDER ASSY.Jun 29, 2012 · N2437S · Cessna 210L · Reciprocating Engine Cylinder SectionSDR 2012F00094Control Panel · inoperativeEMERGENCY LIGHTS COMING ON WHEN AIRCRAFT POWER TURNED OFF.May 18, 2012 · N5DJ · Cessna 210L · Emergency LightingSDR FPI2012F00007Cylinder Head · crackedDURING A 100 HR INSP, COMPRESSION TEST AND SOAP BUBBLE TEST FOR CRACKS FOUND NR 1 CYLINDER HEAD CRACKED.Apr 11, 2012 · N59130 · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2012F00005Cylinder · crackedDURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LONG. REPLACED PROT 4 TO 6 INCHES LONG. REPLACED BOTH WITH NEW CYLINDER ASSY. NR 3 CYLINDER, SN 61105Mar 2, 2012 · N2437S · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPIA2012F00004Cylinder · crackedDURING A 100 HR INSPECTION-COMPRESSION TEST, FOUND NR 3 CYLINDAER AND NR 5 CYLINDER HEAD CRACKED AT THE TOP OF CYLINDER SLEEVE AT EXHAUST PORT 4 TO 6 INCHES LONG. REPLACED PROT 4 TO 6 INCHES LONG. REPLACED BOTH WITH NEW CYLINDER ASSY. NR 3 CYLINDER, SN 61105Mar 2, 2012 · N2437S · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2012F00002Cylinder · crackedDURING A 100 HR INSP COMPRESSION TEST, FOUND NR 2 CYLINDER HEAD CRACKED FROM 1ST FIN INBD OF UPPER SPARK PLUG OVER EXHAUST VALVE TO UPPER SPARK PLUG HOLE USING SOAPY WATER. DURING COMPRESSION TEST BUBBLED FROM CRACK.Jan 3, 2012 · N59130 · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2012F00000Cylinder Head · crackedDURING A 100 HR INSP, COMPRESSION TEST FOUND NR 1 CYLINDER HEAD CRACKED ABOVE EXHAUST VALVE TO SPARK PLUG UPPER USING SOAP WATER SOLUTION DURING COMPRESSION TEST. REPLACED WITH NEW ASSY.Dec 20, 2011 · N2495S · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2011F00010Cylinder Head · crackedDURING A 100 HR INSPECTION, FOUND NR1 CYLINDER CRACKED BETWEEN THE COOLING FINS OF THE EASTHEAD ABOVE THE INTAKE PORT BEHIND FUEL NOZZLE PORT.Oct 28, 2011 · N7874J · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2011F00004Cylinder · 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 · N300EW · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2011F00003Cylinder · 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 · N300EW · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2011F00002Cylinder · crackedDURING A 100 HR INSPECTION FOUND THE CYLINDER HEAD 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 · N300EW · Cessna 210L · Reciprocating Engine Cylinder SectionSDR FPI2011F00001Shaft · out of positionRECEIVED NEW FUEL SELECTOR SHAFT AND WAS FOUND TO BE ASSEMBLED 180 DEGREES OUT. THE HANDLE TO SELECT FUEL TANK POINTS TO THE OPPOSITE TANK OF WHICH IS BEING USED. RECEIVED REPLACEMENT FOR ABOVE PAR AND IT ALSO WAS ASSEMBLED 180 DEGREES OUT. ADVISED MFG OF PMar 30, 2011 · N2667S · Cessna 210L · Fuel Selector/Shut-Off ValveSDR 2011FA0000053Wheel Half · failedLT WHEEL ASSY CAME APART AT OUTER WHEEL HALF DURING TAXI OF ACFT.Jan 27, 2011 · N5318V · Cessna 210L · Wheel/Ski/FloatSDR FPI2010F00002Shuttle Valve · brokenDURING ANNUAL INSP OF ACFT, INSP OF SHUTTLE VALVE OF STANDBY VACUUM SYS FOUND THE VACUUM PUMP SIDE, VALVE SPRING BROKEN. REPLACED WITH NEW PART.Nov 1, 2010 · N5489V · Cessna 210L · Vacuum Distribution SystemSDR WUMR2011001Actuator · false activationDURING FLIGHT THE LT GEAR "DOWNLOCK ACTUATOR" FAILED WHILE THE GEAR WAS IN THE "UP" POSITION. THE DOWNLOCK HAS AN INTERNAL FAILURE WHICH ALLOWED IT TO COLLAPSE INTO THE "LOCKED" POSITION. THE NEXT TIME THE PILOT SELECTED "GEAR DOWN", THE LT GEAR WAS UNABLE TO Oct 28, 2010 · N2455S · Cessna 210L · Landing Gear ActuatorSDR CA101018013Switch · failedSNAG: LANDING LIGHT SWITCH TO VERIFY, LANDING LIGHT SWITCH (1) PN: TA-201-TW-B. REPLACED NEW IAW SB SEB09-6 (DUE SPARKING COMING OUT THROUGH KNOB WHEN PUTTING SWITCH AT ON POSITION) CONNECTING, WIRES, TERMINALS, CHECKED OK SWITCH SECURED AND FUNCTIONAL CHECKEDOct 15, 2010 · Cessna 210L · Exterior LightingSDR CA100719005Fastener · missing(CAN) UPON TAXI, PILOT NOTICED RIGHT MAIN WHEEL LOCKED UP DURING TAXI. MAINTENANCE WAS DISPATCHED AND UPON INVESTIGATION WAS FOUND THAT RIGHT MAIN WHEEL ASSEMBLY P/N C163006-0103 WAS IN FAILURE MODE. THE INNER WHEEL FLANGE P/N D30210 WAS SEPARATING FROM THE Jul 14, 2010 · Cessna 210L · Wheel/Ski/FloatSDR FPI2010F00001Spring · inoperativeENGINE WAS REMOVED FOR INTERNAL VIBRATION AND REPAIRED BY MFG. REPLACED CRANKSHAFT ENGINE, REINSTALLED IN ACFT. AFTER APPROXIMATELY 16 CYCLES, THE STARTER WAS ENGAGED WITHOUT ENGINE TURNING. REMOVED STARTER ADAPTOR, P/N 643259A18. INSPECTED AND FOUND CLUTCJun 18, 2010 · N30326 · Cessna 210L · Engine StarterSDR FPI2010F00000Cable Assy · brokenMFG SERVICE KIT: PN SK210-174. CABLE ASSY CABLE BROKEN AT SWEDGE END EYELET AT THREADED END.Mar 25, 2010 · N30326 · Cessna 210L · Landing Gear Retraction/Extension SystemSDR CA100116001Terminal · shorted(CAN) ON APPROACH, THE PILOT SELECTED GEAR DOWN IN ANTICIPATION FOR LANDING. AFTER DOING THIS, SPARKS WERE NOTICED BEHIND THE INSTRUMENT PANEL BELOW THE RADIO STACK. THE PILOT RETURNED THE GEAR SELECTOR TO THE UP POSITION AND PULLED THE GEAR PUMP CIRCUIT BREAJan 15, 2010 · Cessna 210L · Landing Gear System WiringSDR CA090929003Landing Gear · obstructed(CAN) UPON APPROACH, PILOT SELECTED MLG DOWN, & DID NOT GET A MLG DOWN INDICATION & HYDRAULIC MOTOR DID NOT SHUT-OFF. PILOT PULLED MLG CIRCUIT BREAKER & USED EMERGENCY EXTENSION PUMP. PILOT SAID HAND PUMP PRESSURED UP IMMEDIATELY. VISUAL ON LT & RT MLG INDICATSep 27, 2009 · Cessna 210L · Nose/Tail Landing GearSDR CA090622020Exhaust Valve · stuck(CAN) ACFT WAS UNDERGOING A 50 HR INSP. INSP REVEALED AN OIL LEAK ON RT SIDE OF ENG. INVESTIGATION REVEALED EXHAUST PUSH TUBE SEALS WERE LEAKING. REMOVAL OF THE PUSH TUBE AND ROD REVEALED PUSH ROD WAS BENT. OIL LEAK WAS CAUSED BY PUSH ROD DISPLACING SEALS OJun 19, 2009 · Cessna 210L · Reciprocating Engine Cylinder SectionSDR 2008FA0000302Gasket · failedTHE OIL COOLER ADAPTER GASKET TAILED IN FLIGHT CAUSING (2) QUARTS OF OIL IN ONE HOUR TO BE PUMPED INTO THE ENGINE COWLING. THIS ENGINE IS A FACTORY REMANUFACTURED ENGINE WITH 140 HOURS SINCE REMAIN. ON INSPECTION AND DISASSEMBLY THE OIL COOLER ADAPTER BOLTS Apr 19, 2008 · N132WB · Cessna 210L · Engine Oil CoolerSDR 2008FA0000222Downlock Switch · brokenEXAMINATION OF THE LANDING GEAR SYSTEM REVEALED THAT THE LT LDG DOWN LIMIT SWITCH PLUNGER WAS DAMAGED AND STUCK IN THE DEPRESSED POSITION WITH APPROX .012 INCH AIRGAP BETWEEN PLUNGER TIP AND STRIKER PLATE. WITH SIMULATED AIR LOADS APPLIED TO THE LT MAIN GEAR Nov 16, 2007 · N987M · Cessna 210L · Landing Gear Position and WarningSDR CA070410003Bolt · broken(CAN) ON SCHEDULED INSPECTION APPRENTICE FOUND ONE ATTACH BOLT BACKED OUT OF HOLE. ON REMOVING THE BOLT FULLY HE FOUND THE BOLT TO BE BROKEN. THE AIRCRAFT WAS JACKED UP AND THE ACTUATOR WAS REMOVED. THE OTHER 2 ATTACH BOLTS WERE INSPECTED AND FOUND WORN. THE AMar 27, 2007 · Cessna 210L · Landing Gear Actuator
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