Cessna T210L

Service difficulty reports · 78

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 = 'T210L'
  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 2024FA0000836Seat · brokenDURING THE 200HR/ANNUAL INSPECTION IT WAS FOUND THAT BOTH CESSNA SK210-175A AND SK210-175B KITS THAT WERE INSTALLED TO COMPLY WITH CESSNA SB SEB07-5R2 WERE FOUND IN AN INOP CONDITION (BROKEN). THE SWIVEL ADAPTER THAT IS HELD ONTO THE REEL ASSEMBLY WITH 2 SMALLNov 12, 2024 · N74LC · Cessna T210L · Flight Compartment EquipmentSDR 2023FA0000305Alternator · failedN4678Q, C210, DECLARED AN EMERGENCY DUE TO POSSIBLE ELECTRICAL ISSUE. THE FLIGHT LANDED SAFELY WITHOUT ISSUE.May 13, 2023 · N4678Q · Cessna T210L · Alternator-Generator DriveSDR 2023FA0000267Rod · brokenROD ASSEMBLY BROKE AT THE THREADED END OF THE ROD END.Apr 24, 2023 · N2092S · Cessna T210L · Standard Practices/StructuresSDR 2016FA0000584Alternator · low voltageVOLT METER INDICATED A DISCHARGE AT 1000 RPM. NORMAL VOLT AT 1000RPM AS PER CHECK SHOULD BE 28.5+-5. VOLT METER INDICATED AT 1000 RPM 25.0 AMPS 37. AT 1700 RPM VOLT 27.8 AMPS 42, AT 2000 RPM V27.8 AMPS 39.Nov 15, 2016 · N93285 · Cessna T210L · AC Generator-AlternatorSDR 4DSR201411240001Control Unit · seizedDURING 50 HOUR INSPECTION, MECHANIC FOUND THE MIXTURE CONTROL OPERATION TO BE VERY STIFF. FOUND THE MIXTURE CONTROL UNIT ON ENGINE SEIZED AND VERY HARD TO MOVE BY HAND, REPLACED.Nov 24, 2014 · N93285 · Cessna T210L · Mixture ControlSDR 2014FA0000560Tube · failedENROUTE, MANIFOLD PRESSURE DROPPED TO 24". INDUCTION TUBE FROM COMPRESSOR TO THROTTLEBODY FAILED WITH A 2" TO 3" HOLE ONLEFT SIDE BLEW OUT.Jul 29, 2014 · N100BG · Cessna T210L · Aircraft Fuel Distribution SystemSDR 2013FA0000181Hose · leakingFIRST GROUND RUN REVEALED A LEAKING OIL PRESSURE TO WASTGATE HOSE OR FITTING. REPLACED FITTING IN ENGINE WITH NEW STEEL FITTING. SECOND GROUND RUN, OIL LEAKED FROM HOSE AGAIN. AFTER SLIGHT ADDITIONAL TORQUE APPLIED AND THIRD GROUND RUN, THE HOSE WAS REPLACEDMar 20, 2013 · N732JJ · Cessna T210L · Reciprocating Engine Oil SystemSDR R29R2012062001Switch · loosePILOT REPORTED NO GEAR DOWN INDICATION UPON LOWERING THE LANDING GEAR HANDLE. IFE WAS DECLARED, GEAR WAS VISUALLY CONFIRMED DOWN BY GROUND CREW AND ACFT LANDED UNEVENTFULLY. IT WAS DISCOVERED THAT THE JAMB NUT THAT SECURES THE DOWN LOCK SWITCH HAD LOOSENED TOJun 20, 2012 · N732BB · Cessna T210L · Landing Gear Position and WarningSDR 2011FA0000805Cylinder · fractured6 NEW CYLINDERS WERE INSTALLED AUG 10, 2008 AT 2812 TOTAL TIME. THE CYLINDERS EXPERIENCED A FAILURE OF THE VALVE GUIDES ON 3 OF THE 6 AT 384 HOURS TIME IN SERVICE. ALL 3 FAILED VALVE GUIDES BROKE OFF AT THE INSERT POINT AND 1 COMPLETELY DISINTEGRATED, CONTAMINNov 15, 2011 · N732GS · Cessna T210L · Reciprocating Engine Cylinder SectionSDR 2009FA0000004Bolt · failedDURING CLIMB TO CRUISE ENGINE MADE A LOUD NOISE AND QUIT RUNNING, ENGINE REMAINED WINDMILLING TO LANDING. VISUAL INSP REVEALED NR 3 CYLINDER ROD BOLT MISSING, ROD CAP EXITED ENG THRU UPPER CASE, NO EVIDENCE OF OIL STARVATION.Dec 10, 2008 · N9426K · Cessna T210L · Reciprocating Engine Power SectionSDR 2008FA0000546Control Cable · defectiveORDERED NEW FLAP FOLLOW UP CABLE; TO REPLACED ORIGINAL CABLE WHICH HAD BECOME DEFECTIVE DUE TO NORMAL USAGE AND AGE.Jul 17, 2008 · N2423S · Cessna T210L · Trailing Edge Flap Control SystemSDR 2008FA0000499Control Cable · defectiveORDERED NEW MFG FLAP FOLLOW UP CABLE; TO REPLACE ORIGINAL CABLE WHICH HAD BECOME DEFECTIVE DUE TO NORMAL USAGE AND AGE. THIS CABLE IS SIMILAR TO A THROTTLE CABLE WITH AN INSIDE CABLE WHICH SLIDES IN AN OUTSIDE HOUSING. UPON INSTALLATION, OF NEW MFG FLAP FOLLJul 16, 2008 · N2423S · Cessna T210L · Trailing Edge Flap Control SystemSDR CA061019009Spring · broken(CAN) NOTE THE SERIAL NUMBER ON THE ENGINE ON THIS FORM IS INCORRECT IT IS 217469-R. THE IMPULSE COUPLING SPRING WAS FOUND BROKEN. CUSTOMER HAD COMPLAINED OF ROUGH RUNNING CHECK MAG DROP, REMOVED MAGS AND INSPECTED. THE SPRINGS WERE BROKEN IN BOTH MAGNETOS,Oct 18, 2006 · Cessna T210L · Magneto/DistributorSDR CA061109004Bracket · loose(CAN) BRACKET P/N 1243019-2 FOUND LOOSE AGAINST TORQUE TUBE P/N 1234650-2. LOOSE FASTENERS REMOVED AND REPLACED. (TC NR 20061109004)Sep 22, 2006 · Cessna T210L · Elevator StructureSDR AOC06001Actuator · brokenUPON LANDING, THE NOSE LANDING GEAR COLLAPSED, CAUSING MAJOR DAMAGE TO THE PROPELLER AND DAMAGE TO THE NOSE SECTION OF THE AIRCRAFT. INSPECTION AFTER RECOVERY REVEALED THE THE BEARING END (P/N - 1280600-5) HAD BROKEN, ALSO SHEARING THE PINS (P/N - 1280209-1).Mar 16, 2006 · N57977 · Cessna T210L · Landing Gear Retraction/Extension SystemSDR AU510001486Crankcase · damaged(AUS) CRANKCASE HOLED. LOSS OF POWER IN NR 4 AND NR 6 CYLINDERS. (CASA# 510001486)Dec 12, 2005 · Cessna T210L · Reciprocating Engine Power SectionSDR 2005FA0000697Pressure Switch · failedLANDING GEAR FAILED TO FULLY RETRACT AFTER TAKEOFF. FOUND THAT THE WIRE SOLDERED TO THE HYDRAULIC POWER PACK PRESSURE SWITCH HAD CORRODED BENEATH THE HEAT-SHRINK TUBING, NEAR THE SOLDER JOINT. SUSPECTED: THE MFG OF THE PRESSURE SWITCH ASSY USED ACID CORE SODec 14, 2004 · N2164S · Cessna T210L · Hydraulic Indicating SystemSDR CA040622005Belt · failed(CAN) THE ALTERNATOR DRIVE BELT CAME OFF IN FLIGHT.Jun 6, 2004 · Cessna T210L · Alternator-Generator DriveSDR 2004FA0000432Pump · inoperativeENGINE DRIVEN FUEL PUMP NO METERED OR UN METERED FUEL PRESSURE WHILE ENGINE RUNNING. FUEL PUMP RECENTLY INSTALLED HAD 2.7 HOURS ON IT, AFTER OVERHAUL. INSTALLED NEWLY OVERHAULD PUMP. OPS CHECK GOOD. PROBABLE CAUSE OF PUMP FAILURE, UNKNOWN.May 21, 2004 · N93379 · Cessna T210L · Engine Fuel PumpSDR 21200004Autopilot Sys · defectiveAIRCRAFT PORPOISES WHILE IN ALTITUDE HOLD MODE. DISABLE ALTITUDE HOLD MODE. MAINTENANCE CONFIRMS DEFECTIVE UNIT BY MANUFACTURER. MANUFACTURER UNABLE TO SUPPLY REPLACEMENT PART.Feb 21, 2004 · N2084S · Cessna T210L · Autopilot SystemSDR 2004FA0000198Oil Cooler · crackedLOWER OB FLANGE OF ENGINE OIL COOLER IS CRACKED AND LEAKING.Feb 4, 2004 · N732HN · Cessna T210L · Engine Oil CoolerSDR FPI2003F00015Mount · crackedTOP FORWARD MOUNT FLANGE CRACKED UNDER NORMAL OPERATION. TOP AT BOTTOM FLANGES ARE NOT TRUE.Dec 9, 2003 · N732HN · Cessna T210L · Engine Oil CoolerSDR FPI2003F00014Oil Cooler · crackedBOTTOM COOLER TO ENGINE MOUNT EAR CRACKED. OCCURRED UNDER NORMAL OPERATION.Nov 7, 2003 · N732HN · Cessna T210L · Engine Oil CoolerSDR B30R2003003Cylinder · crackedDURING ANNUAL ENGINE INSPECTION A MECHANIC NOTED BLUE FUEL STAIN IN THE AREA OF THE NR 1 CYLINDER FUEL DRAIN PORT. BLUE FUEL STAIN WAS REMOVED AND ENGINE FUEL SYSTEM WAS PRESSURIZED. AT THIS TIME FUEL STARTED TO DRIP FROM IN BETWEEN THE FIRST TWO COOLING FINS Jun 2, 2003 · N732JF · Cessna T210L · Reciprocating Engine Cylinder SectionSDR 2003FA0000032Cowling · wornIT IS POSSIBLE THAT DUE TO NORMAL WEAR OF THE ENGINE COWL CAUSED CONTACT WITH THE NLG DOOR EDGE PREVENTING THE NLG FROM FULLY EXTENDING. IN ADDITION IT IS POSSIBLE THAT DUE TO THE INCORPORATION OF STC SA 5934SW, REMOVING HYDRAULIC POWER FROM THE NLG, ACTUATIODec 31, 2002 · N11KR · Cessna T210L · Nacelle/Pylon, Plate/SkinSDR 2003FA0000000Alternator · seizedPILOT REPORTED THAT THE LOW VOLTAGE LIGHT ILLUMINATED ON TAXI. MECHANIC FOUND THAT THE ALTERNATOR HAD SEIZED AND THE BELT HAD BROKEN. WHEN THE ALTERNATOR WAS REMOVED, THE MECHANIC NOTED THAT THERE WAS A NOTICEABLE CATCH WHILE ROTATION THE PULLEY. ADDITIONALNov 26, 2002 · N2317G · Cessna T210L · AC Generator-AlternatorSDR DFJ2002F00000Diode · defectiveLANDING GEAR WOULD NOT EXTEND UNTIL STARTING SYSTEM WITH HAND PUMP. FOUND DEFECTIVE DIODE IN DOWN SIDE OF GEAR SELECTOR SWITCH TO CONTACTOR. DIODE LOOKED NORMAL AND HAD NO EXTERNAL DAMAGE.Oct 25, 2002 · N6864C · Cessna T210L · Aileron Control SystemSDR 2002FA0000990Magneto · corrodedDURING MAINTENANCE, ITS WAS NOTED THAT THE MAGNETOS WERE HAVING TROUBLE HOLDING THEIR TIMING POSITIONS. RT MAGNETO WAS DISASSEMBLED AND FOUND THAT THE DRIVE AND DRIVEN GEARS HAD ROTTED TO THE POINT OF LOSING TEETH. NOTED THAT THE CARBON BUTTON THAT RIDES ON Aug 14, 2002 · N59132 · Cessna T210L · Magneto/DistributorSDR 2002FA0000989Magneto · corrodedDURING MAINTENANCE, IT WAS NOTED THAT THE MAGNETOS WERE HAVING TROUBLE HOLDING THEIR TIMING POSITIONS. RT MAGNETO WAS DISASSEMBLED AND FOUND THAT THE DRIVE AND DRIVEN GEARS HAD ROTTED TO THE POINT OF LOSING TEETH. NOTED THAT THE CARBON BUTTON THAT RIDES ON TAug 14, 2002 · N59132 · Cessna T210L · Magneto/DistributorSDR 11482Wheel · crackedON PRECAUTIONARY INSPECTION FOUND CRACKS AT WHEEL/HUB FLANGE MOUNTING BOLT HOLES ON BOTH WHEELS. REPLACED BOTH WHEELS WITH CLEVELAND TWO PIECE WHEELS. WE HAVE FOUND 6 OF THE SAME WHEEL(HUBS)CRACKED ON 172/182/210 CESSNA AIRCRAFT IN THE LAST WEEK. RECOMMEND IMMJul 31, 2002 · N94148 · Cessna T210L · Wheel/Ski/FloatSDR 2002FA0000588Alternator · failedALTERNATOR FAILED IN FLIGHT. PILOT SMELLED ELECTRICAL BURNING ODOR. FLIGHT COMPLETED WITHOUT INCIDENT. ALTERNATOR REPLACEMENT CORRECTED PROBLEM. THIS IS THE 2ND ALTERNATOR FAILURE ON THIS ENGINE WITHIN 300.7 HOURS. FAILED ALTERNATOR NOT DISASSEMBLED TO DEApr 22, 2002 · N1226M · Cessna T210L · AC Generator-AlternatorSDR 2002FA0000214Line · corrodedLINE DEVELOPED PINHOLE LEAK DUE TO CORROSION WHERE CABIN VENT SCEET HOSE RESTED ON TOP OF IT.Feb 13, 2002 · N711PJ · Cessna T210L · Aircraft Fuel Distribution SystemSDR 2001FA0000361Rib · crackedLEFT WING RIB CRACKED WHERE LEFT FLAP BELLCRACK SUPPORT BRACKETS ARE MOUNTED, CRACK RUNS FROM INBOARD LOWER SUPPORT BRACKET RIVET HOLE APPROX. ONE(1) INCH IN LENGTH DOWN AND TO THE LEFT. PROBABLE CAUSE: FLAPS EXTENDED AT TOO HIGH OF AN AIRSPEED.Sep 20, 2001 · N375AB · Cessna T210L · Wing, Rib/BulkheadSDR NMO192Hose · failedDURING LANDING, NOSE GEAR EXTENDED AND LOCKED, BUT MAIN GEAR DID NOT LOCK INTO PLACE. PILOT TRIED TO LOCK MAIN GEAR USING HAND HYDRAULIC PUMP WITH NO SUCCESS. AIRCRAFT LANDED WITH LOCKED NOSE GEAR AND COLLAPSED MAIN GEAR. SUFFERED DAMAGE TO REAR OF FUSELAGE, LSep 12, 2001 · N6721M · Cessna T210L · Landing Gear Retraction/Extension SystemSDR 20010613CW002Control Cable · slippedDURING 100 HR INSPECTION, FOUND FLAPS NOT WORKING PROPERLY, FOUND CONTROL PUSH/PULL CABLE OUTER HOUSING WHERE HOUSING IS CLAMPED, SLIPPING IN CLAMP BUSHING. ORDER NEW CABLE FROM CESSNA, IT WAS TOO SHORT, CALLED CESSNA AND FOUND THEIR STOCK WAS MANUFACTURED WRMay 26, 2001 · N93344 · Cessna T210L · Trailing Edge Flap Control SystemSDR 20000821SH009Magneto · corrodedPRESSURIZED SLICK MAGNETOS ON CESSNA T210L. DURING ANNUAL, INSPECTED MAGS INTERNALLY FOR CONDITION. FOUND SEVERE MOISTURE-CASED CORROSION ALL AROUND INSIDE. MAGNETO MANUAL CALLS FOR INSPECTION OF 6200 SERIES EACH 100 HOURS, NOTHING FOUND FOR INSPECTION OF 6Aug 11, 2000 · N94203 · Cessna T210L · Magneto/DistributorSDR 20000821SH008Magneto · corrodedPRESSURIZED SLICK MAGNETOS ON CESSNA T210L. DURING ANNUAL, INSPECTED MAGS INTERNALLY FOR CONDITION. FOUND SEVERE MOISTURE-CASED CORROSION ALL AROUND INSIDE. MAGNETO MANUAL CALLS FOR INSPECTION OF 6200 SERIES EACH 100 HOURS, NOTHING FOUND FOR INSPECTION OF 6Aug 11, 2000 · N94203 · Cessna T210L · Magneto/DistributorSDR B3OR200000002Skin Panel · looseAIRCRAFT WAS TEST FLOWN DUE TO HIGH CO LEVEL DISCOVERED IN ANOTHER 210 SERIES FLEET AIRCRAFT. PILOTS FOUND UNACCEPTABLE LEVEL OF CO IN CABIN USING TOXIBEE CO DETECTOR. MAINTENANCE FOUND EXHAUST GASES ENTERING TAILCONE THROUGH VENT HOLE FOR STC SA71RM AIR CONDIJul 26, 2000 · N732JF · Cessna T210L · Fuselage Main, Plate/SkinSDR CA000802024Bracket · cracked(CAN) DURING THE INSPECTION OF THE STABILIZER, A CRACK WAS FOUND ON THE INBOARD LT STABILIZER BRACKET TO ELEVATOR P/N 1232624-1 ATTACHED TO THE SPAR. PROBLEM WAS REPAIRED.Jul 14, 2000 · Cessna T210L · Elevator Control SystemSDR CA000802023Solenoid · failed(CAN) AFTER TAKEOFF AND LANDING SELECTED UP AND LOCKED. LANDING GEAR CIRCUIT BREAKER TRIPPED. (PROBLEM RETURNED INTERMITTENTLY.) PROBLEM TRACED TO DEFECTIVE LANDING GEAR SOLENOID. SOLENOID REPLACED, PROBLEM SOLVED.Jul 14, 2000 · Cessna T210L · Landing Gear Retraction/Extension SystemSDR 20000522SH016Riser · crackedMAINTENANCE LOOKED AT ACFT BEFORE FLIGHT. COWLING WAS REMOVED AND EXHAUST SOOT WAS SEEN AROUND LOWER SIDE OF NR 4 CYLINDER. FURTHER INVESTIGATION REVEALED A CRACK AROUND THE EXHAUST RISER THAT WAS ABOUT 270 DEGREES AROUND THE PIPE. HEAT EXCHANGER PORTION OFMay 15, 2000 · N732JF · Cessna T210L · Engine Collector/Tailpipe/NozzleSDR 20000417SH016Link · crackedDURING ROUTINE INSPECTION, FOUND UPPER TORQUE LINK CRACKED. SUBMITTER STATED THIS PART NUMBER LINK WAS FOUND CRACKED ON ANOTHER T210L IN THE SAME FLEET. (X)Mar 13, 2000 · N6864C · Cessna T210L · Landing Gear Retraction/Extension SystemSDR 99ZZZX2978Skin · crackedTHE TRAILING EDGE OF THE AIRCRAFT WING INBOARD OF THE SPEED BRAKE LOCATION. THE DISTURBED AIR BEHIND THE EXTENDED SPEED BRAKES WAS WORKING THE TRAILING EDGE OF THE WING CAUSING CRACKS AROUND THE TRAILING EDGE ATTACHMENT RIVETS.Jul 1, 1999 · N4687Q · Cessna T210L · Wing, Plate/SkinSDR 99ZZZX2772Reinforcement · crackedREINFORCEMENT P/N 1232623-2 NOTED AS CRACKED. THE AIRCRAFT HAD NOT HAD SE84-17 C/W, SO THE NEW BRACKETS ORDERED. IT WAS SUGGESTED CHANGE COULD BE DONE WITHOUT COMPLETELY REMOVING THE HORIZONTAL STABILIZER. SUBMITTER ELECTED TO REMOVE THE STABILIZER AND INSPJun 25, 1999 · N61170 · Cessna T210L · Horizontal Stabilizer StructureSDR 99ZZZX2771Fitting · looseREINFORCEMENT P/N 1232623-2 NOTED AS CRACKED. THE AIRCRAFT HAD NOT HAD SE84-17 C/W, SO THE NEW BRACKETS ORDERED. IT WAS SUGGESTED CHANGE COULD BE DONE WITHOUT COMPLETELY REMOVING THE HORIZONTAL STABILIZER. SUBMITTER ELECTED TO REMOVE THE STABILIZER AND INSPJun 25, 1999 · N61170 · Cessna T210L · Horizontal Stabilizer StructureSDR 99ZZZX1193Control Cable · malfunctionedWHEN FLAP FOLLOW-UP CABLE IS INSTALLED IN AIRCRAFT, IT HAS AN INTERNAL BIND WHICH CAUSES THE BELLCRANK IN THE LEFT WING TO 'JERK' AS THE MOTION OF THE BELLCRANK OVERCOMES THE BINDING OF THE CABLE. THIS 'JERKING' CAUSES THE RIB TO WHICH THE BELLCRANK IS ATTACHMar 8, 1999 · N10419 · Cessna T210L · Trailing Edge Flap Control SystemSDR 99ZZZX1195Reinforcement · crackedWHEN A 1 INCH LONG CRACK WAS NOTED ON ANOTHER T210 HORIZONTAL STABILIZER AFT SPAR, THIS AIRCRAFT WAS INSPECTED AND A CRACK WAS NOTED ON THE AFT SPAR REINFORCEMENT. WHEN THE STABILIZER WAS REMOVED, THE LEFT FORWARD FITTING (PN 0732601-5) WAS NOTED TO HAVE 4 OFJan 18, 1999 · N93155 · Cessna T210L · Horizontal Stabilizer StructureSDR 99ZZZX706Battery Box · leakingDURING ANNUAL INSPECTION, BATTERY ACID WAS FOUND TO HAVE LEAKED INTO COCKPIT ONTO LEFT RUDDER PEDAL, ATTACHING TUBING, AND GENERAL AREA BELOW PEDAL. ACID HAD FLOWED THROUGH CORRODED RIVET HOLE ONTO SEAT FOR CABIN HEAT AND DRIPPED INTO FLOOR AREA. SUBMITTER BJul 15, 1998 · N2259S · Cessna T210L · Battery Box StructureSDR 98ZZZX2356Plunger · wornFUEL STRAINER PLUNGER NIPPLE WEARING.Jun 13, 1998 · N732GR · Cessna T210L · Aircraft Fuel Filter/StrainerSDR 98ZZZX2037Cowling · mismanufacturedTHIS NEW COWL WAS PURCHASED FROM CESSNA AND IT HAS TWO PROBLEMS. 1. THE TOP LEADING EDGE IS TOO THICK IN PLACES (FILLER OR ADHESIVE) AND WILL NOT CONTOUR WITH EXISTING NOSE COWL. 2. ON THE AFT EDGE, THERE IS NOT ENOUGH MATERIAL, AN APPROXIMATE .25 INCH GAMay 13, 1998 · N2317G · Cessna T210L · Engine Cowling System
Back to Cessna T210L