Cessna T210M

Service difficulty reports · 110

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 = 'T210M'
  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 2024FA0000268Cylinder Head · separatedTHE PILOT REPORTED A LOSS OF MANIFOLD PRESSURE IN FLIGHT ALONG WITH A REDUCTION IN POWER AND CRUISE SPEED. THE AIRCRAFT SAT UNTIL THE 28TH OF MARCH AWAITING MAINTENANCE. UPON INVESTIGATION, THE CYLINDER HEAD WAS FOUND TO HAVE SEPARATED FROM THE CYLINDER BODY AMar 15, 2024 · N732SE · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 2020FA0000377Ring · brokenELECTRICAL SYSTEM FAILURE. FOUND BROKEN RING TERMINAL AT POSITIVE TERMINAL OF ALTERNATOR. FOUND VOLTAGE REGULATOR INOP.Aug 18, 2020 · N761PM · Cessna T210M · AC Generator-AlternatorSDR 2020FA0000335Not Reported · corrodedEXTREME CORROSION FOUND ON PARTS INSIDE PROP HUB POST OVERHAUL WITH LESS THAN 40 HOURS FROM OVERHAUL. OPERATOR SUSPECTS UNAPPROVED PARTS MAY HAVE BEEN USED AND REPLACEMENT KIT PARTS NOT REPLACED IAW MANDATORY REPLACEMENT KIT MANUAL PROCEDURES.Jul 15, 2020 · N68BM · Cessna T210M · Propeller AssemblySDR SQPA20190919002Bolt · missingNOSE GEAR CAME LOOSE FROM NOSE GEAR FORK. NOSE GEAR BOLT FORK FOUND TO BE MISSING. NO WORK RECENTLY PERFORMED ON NOSE GEAR. NO EMERGENCY MEASURES TAKEN. NO ADS, SBS, STCS OR ICA'S APPLY. BOLT WAS NOT FOUND POST EVENT. SUGGEST PREFLIGHT INSPECTION TO ENSURE BOLAug 13, 2019 · N732DW · Cessna T210M · Nose/Tail Landing Gear Strut/AxleSDR SQPA20190919001Door · buckledLT GEAR DOOR BUCKED IN FLIGHT. SUSPECT GEAR DOOR WAS DAMAGED DUE TO OVERSPEED. NO WORK RECENTLY PERFORMED ON LANDING GEAR. NO EMERGENCY ACTIONS TAKEN. NO APPLICABLE ADS, SBS, STCS OR ICAS. SUGGEST VISUAL INSPECTION OF ADHESIVE ATTACHING STRUCTOR TO DOOR EVERY Aug 13, 2019 · N73TG · Cessna T210M · Landing Gear DoorsSDR NF2R201812210002Lifter · galled#1 CYLINDER LOW COMPRESSION 59/80 LEAKING THROUGH EXHAUST VALVE. FOUND LIFTERS SHOWING PITTING AND STRESS.Apr 16, 2015 · N15DA · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 2014FA0000074Spar · looseDURING ANNUAL INSPECTION, FOUND MOVEMENT IN THE RT WING SPAR FITTINGS, BETWEEN THE RT WING MAIN SPAR ATTACH BRACKETS AND THE FUSELAGE CARRY-THROUGH SPAR ATTACH BRACKETS.Feb 14, 2014 · N761GQ · Cessna T210M · Wing SparSDR 2014FA0000046Lifter · spalledTWO SPALLED EXHUAST LIFTERS WHICH DAMAGE CAM.May 13, 2013 · N732YK · Cessna T210M · Reciprocating Engine Power SectionSDR 2012FA0000716Pump · leakingPILOT WROTE-UP "FUEL FLOW METER INOP" DURING INITIAL START-UP. FOUND NO OR VERY LOW FUEL FLOW INDICATION AT IDLE BUT ENGINE RAN NORMAL, FOUND NORMAL FUEL FLOW INDICATION AT MID TO HIGH POWER SETTINGS WITH ENGINE RUNNING NORMALLY. FOUND GAUGE TO BEOPERATING PROOct 22, 2012 · N7072 · Cessna T210M · Engine Fuel PumpSDR 2012FA0000672Engine · power lossDURING A FINAL APPROACH, PILOT APPLIED THROTTLE TO ARREST HIS SINK RATE BUT THE ENGINE DID NOT RESPOND. POST ACCIDENT INVESTIGATION REVEALED AT LEAST 5 GALLONS WAS AVAILABLE IN EACH WING TANK.Oct 2, 2012 · N6181N · Cessna T210M · Engine (Turbine/Turboprop)SDR 2011FA0000797Housing · wornCOPILOT SEAT ROLLER HOUSING TANG LENGTH WORN BELOW LIMIT OF AD 2011-10-09.Dec 8, 2011 · N732YK · Cessna T210M · Flight Compartment EquipmentSDR 2011FA0000437Contactor · inoperativeBATTERY CONTACTOR FAILED TO OPEN WHEN DEENERGIZED BY MASTER SWITCH.Jul 2, 2011 · N732YK · Cessna T210M · Battery/Charger SystemSDR 2010FA0001164Camshaft · wornWORN CAMSHAFT (PN 655384, SN 34962) DISCOVERED DURING CYLINDER CHANGE (LOW COMPRESSION) CYLINDERS NR3 & NR4 INTAKE LOBES ONLY. NEW LIFTERS WERE INSTALLED WITH THE NEW CAMSHAFT AT INSTALLATION. INITIATOR STATES THIS HAS BEEN A PROBLEM MORE THAT A FEW TIMES. MFNov 3, 2010 · N761BT · Cessna T210M · Reciprocating Engine Power SectionSDR 2010FA0001170Hub · failedRT MAIN WHEEL HUB BROKE ON LANDING, AFTER NORMAL TOUCHDOWN WITH NO BRAKING. BROKEN AREA OF WHEEL HAS CORROSION AT BOTTOM OF THREADS. WHEEL TURNED SIDEWAYS DAMAGING BRAKE TORQUE PLATE AXEL AND BRAKE LINE.Oct 28, 2010 · N732XF · Cessna T210M · Wheel/Ski/FloatSDR 2010FA0001215Fitting · broken(GBBR) THE ENGINE SUFFERED CATASTROPHIC FAILURE DUE TO ENGINE OIL STARVATION CAUSED BY THE FAILURE/BREAKAGE OF THE TURBOCHARGER OIL RETURN LINE FITTING AT THE REAR OF THE ENGINE. THE LOSS OF ENGINE OIL ULTIMATELY RESULTED IN AN UNCONTAINED FAILURE OF THE NR4 Oct 4, 2010 · N6689B · Cessna T210M · Reciprocating Engine Oil SystemSDR GBBR155EFitting · broken(GGBR) THE ENGINE SUFFERED CATASTROPHIC FAILURE DUE TO ENGINE OIL STARVATION CAUSED BY THE FAILURE/BREAKAGE OF THE TURBOCHARGER RETURN OIL LINE FITTING AT THE REAR OF THE ENGINE. THE LOSS OF ENGINE OIL ULTIMATELY RESULTED IN THE UNCONTAINED FAILURE OF THE NR 4Sep 24, 2010 · N6689B · Cessna T210M · Turbine Engine Oil SystemSDR J7B2010F00001Cylinder · leakingCYLINDER ASSY IS LEAKING. FUEL, EXHAUST, AND OIL STAIN BETWEEN CYLINDER BARREL AND HEAD. OCCURRED UNDER NORMAL USAGE.Aug 13, 2010 · N761ST · Cessna T210M · Reciprocating Engine Cylinder SectionSDR J7B2010F00000Cylinder · leakingCYLINDER ASSY IS LEAKING. FUEL, EXHAUST, AND OIL STAIN BETWEEN CYLINDER BARREL AND HEAD. OCCURRED UNDER NORMAL USAGE.Aug 13, 2010 · N761ST · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 2010FA0000756Check Valve · failedP/N S2361-1, LOT 60507, OIL CHECK VALVE FROM TURBOCHARGER, INSTALLED NEW ON 12 APRIL 2010, 60 HOURS IN SERVICE PRIOR TO FAILURE. RECEIVED "LOW OIL PRESSURE" ALERT FROM AURACLE 2100 SYSTEM, IMMEDIATELY TURNED TO NEAREST AIRPORT (KDTS) AND MADE EMERGENCY LANDINJul 17, 2010 · N734JC · Cessna T210M · Exhaust TurbochargerSDR 2009FA0000791Line · corrodedINSP FOUND MINOR FUEL LEAK AT THE FWD FUEL LINE WHERE IT COMES IN CONTACT WITH FRESH AIR VENT DUCTING LOACTED IN WING L/E. AIR DUCTING CAUSES CORROSION PITS TO FORM. LINE WAS REPLACED. INSPECTED (5) OTHER SIMULAR ACFT AND FOUND SAME RESULTS IN ALL EXCEPT (1Jun 17, 2009 · N761BT · Cessna T210M · Aircraft Fuel Distribution SystemSDR 2009FA0000005Hose · burstRT NLG DOOR ACTUATOR HOSE FAILED CAUSING COMPLETE HYD FLUID LOSS . RESULTING IN LT MAIN GEAR NOT ABLE TO BE FULLY EXTENDED TO DOWN AND LOCKED POSITION. ACFT MADE EMERGENCY LANDING WITH LT MAIN GEAR PARTIALLY EXTENDED. MINOR DAMAGE. FAILED HOSE APPEARS TO BEDec 23, 2008 · N732UR · Cessna T210M · Hydraulic System, MainSDR GAJ2008F00000Pulley · frozenTHE COPILOT RETRACTABLE STEP MALFUNCTIONED DUE TO PULLEYS FREEZING. FWD PULLEY IS HARD TO SEE ON AFT NOSE GEAR WELL AND IS IN A VERY DIRTY ENVIRONMENT. THE REAR PULLEY IS IMPOSSIBLE TO SEE. THE REAR PULLEY STOPPED ROTATING (FROZE) CAUSING SEVERE WEAR TO THE CAAug 25, 2008 · N7067Z · Cessna T210M · Flight Control SystemSDR 2008FA0000085Line · chafedREPLACED HYDRAULIC TUBE (PN 128509-4) DUE TO CHAFFING FROM LONG SCREW IN WRONG LOCATION OF INSPECTION COVER PLATE. THIS WAS FOUND BY INSPECTION AS DESCRIBED IN SEB07-03 FOR 182 SERIES, AND WHICH 182'S HAVE A SUPERSEDED PN AVAILABLE TO NULLIFY THE POTENTIAL PRFeb 21, 2008 · N761AV · Cessna T210M · Hydraulic System, MainSDR 2008FA0000084Line · chafedREPLACED HYDRAULIC TUBE 128509-4 DUE TO CHAFING FROM LONG SCREW IN WRONG LOCATION OF INSPECTION COVER PLATE. THIS WAS FOUND BY INSPECTION AS DESCRIBED IN MFG SEB07-03 AND WHICH HAVE A SUPERSEDED PN AVAILABLE TO NULLIFY THE POTENTIAL PROBLEM. THIS SERIES AND Feb 21, 2008 · N761AV · Cessna T210M · Hydraulic System, MainSDR 2007FA0000817Alternator · failedOVERHAULED DOFF10300B ALTERNATOR FAILED AFTER 458 HOURS IN 35 MONTHS OF USE.Sep 17, 2007 · N732YK · Cessna T210M · DC Generator-AlternatorSDR 2007FA0000572Bearing · brokenWHILE PERFORMING RUN UP OF AIRCRAFT DURING ANNUAL INSPECTION IT WAS NOTICED THAT PILOT RT RUDDER PEDAL HAD AN UNUSUAL FEEL WHILE BRAKING. DURING THE INSPECTION OF THE RUDDER PEDALS IT WAS FOUND THT THE EACH OF THE PILOT SIDE S1675-1 RUDDER IB BEARING HALF HADMay 25, 2007 · N808FS · Cessna T210M · Rudder Control SystemSDR 2006FA0001163Cable · brokenTHE PILOT EXTENDED THE LANDING GEAR PRIOR TO LANDING, AND THE NOSEGEAR WOULD NOT EXTEND INTO THE DOWN-AND-LOCKED POSITION (THE MAINS LOCKED). DURING LANDING, THE NOSEGEAR COLLAPSED. POST INCIDENT INSPECTION SHOWED THAT THE PASSENGER STEP CABLE BROKE AT THE FAug 23, 2006 · N6169N · Cessna T210M · Entrance StairsSDR 2006FA0000426Alternator · failedALTERNATOR FAILED, PLATE SCREWS FELL OUT. (K)Apr 12, 2006 · Cessna T210M · DC Generator-AlternatorSDR 2005FA0001645Probe · failedOUTSIDE AIR TEMP PROBE FAILED SELF TEST INDICATING OPEN.Dec 29, 2005 · Cessna T210M · Engine Indicating SystemSDR 2005R0124Altimeter · bindsALTIMETER HANDS ARE BENT & INTERFERE WITH EACH OTHER.Jun 28, 2005 · N732XE · Cessna T210M · Altimeter, Barometric/EncoderSDR 2005FA0000836Circuit Board · looseELECTRIC PITCH TRIM SYSTEM RAN AWAY ON APPROACH. AUTOPILOT/ TRIM DISCONNECT HAD NO EFFECT. PILOT DISENGAGED PITCH TRIM CIRCUIT BREAKER TO STOP THE RUNAWAY. AFTER THE CIRCUIT BREAKER WAS DISENGAGED, THE CONTROL WHEEL VIBRATED ON THE APPROACH AT APPROXIMATELYJun 1, 2005 · N6033N · Cessna T210M · Flight Control System WiringSDR 2005FA0000024Bolt · loose3 OF THE 4 BOLTS THAT ATTACH THE METAL PLATE THAT THE ACTUATOR IS MOUNTED ON TO THE WASTEGATE BODY WERE MISSING. FOURTH BOLT WAS BACKED OUT ABOUT HALF WAY. ALL THREE BOLTS FOUND LOOSE IN ENGINE COMPARTMENT. WASTEGATE ASSEMBLY ONLY 287 FROM OVERHAUL BY MAIN Jan 17, 2005 · N732YK · Cessna T210M · FastenersSDR 2005FA0000444Exhaust Valve · brokenPILOT REPORTED HEARING A BANG AND NOTICED AN ENGINE VIBRATION AND REDUCTION IN TEMPERATURE ON HIS ENGINE MONITOR. PILOT REPORTED AN EMERGENCY TO ATC AND MADE A SAFE LANDING AT AIRPORT. MAINTENANCE PERFORMED AN ENGINE COMPRESSION TEST AND FOUND CYLINDER NR 1 Dec 23, 2004 · N761QK · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 2005FA0001298Alternator · failedOVERHAULED ALTERNATOR FAILED IN FLIGHT AFTER 351 HOURS IN SERVICE.Dec 9, 2004 · N732YK · Cessna T210M · AC Generation SystemSDR 2004FA0000807Exhaust Valve · burnedEXHAUST VALVE LEAKAGE ON COMPRESSION CHECK. BURNED VALVE VERIFIED BORESCOPE INSPECTION. VALVE STEM AND GUIDE WORN BEYOND SERVICE LIMITS.Oct 17, 2004 · N732YK · Cessna T210M · Reciprocating Engine Power SectionSDR 2004FA0000659Fuel Strainer · looseAD 2000-06-01 HAS STAND PIPE MEASUREMENT AT 1.68 INCHES. FOUND STAND PIPE LONG AT 1.75.6. REPLACED WITH NEW FUEL STRAINER WITH STAND PIPE AT 1.68 (AT FLIGHT ICE FOUND STAND PIPE LOOSE ON OTHER AND LIKE AIRCRAFT. AC; 8159 TT 3667.Jun 30, 2004 · N8159M · Cessna T210M · Aircraft Fuel Filter/StrainerSDR 06282004Retaining Ring · wornA RETAINING RING SEPERATED FROM THE LT MAIN LANDING GEAR DOOR HYDRAULIC ACTUATOR. THIS LEAD TO A LOSS OF HYDRAULIC FLUID AND FAILURE OF THE LANDING GEAR SYSTEM. AIRCRAFT WAS FORCED TO LAND WITH THE NOSE GEAR EXTENDED AND NO MAIN WHEELS. PILOT REPORTED THAT TJun 28, 2004 · N121JR · Cessna T210M · Landing Gear Door ActuatorSDR 2004FA0000800Latch · failedDURING THE ANNUAL INSPECTION, FOUND THE PN 1250938-8, MAGNET LATCH ON THE ALTERNATE AIR DOOR WITH ONE OF ITS STEEL BONDED PLATES LOOSE AND READY TO FALL INTO THE TURBO, COULD CAUSE INFLIGHT FAILURE. INSTALLED THE NEW IMPROVED CATCH PN C100200. RECOMMEND MANDJun 3, 2004 · N7568M · Cessna T210M · Engine Air Intake SystemSDR 2004FA0000770Plate · separatedENGINE ALTERNATE AIR DOOR IS HELD CLOSED WITH A MAGNETIC LATCH ORIGINAL PN 1250938-8. THE MAGNETIC LATCH HAS 2 STEEL SMALL PLATES BONDED TO THE MAGNET THAT MAKE CONTACT WITH THE ALTERNATE AIR DOOR. ONE STEEL PLATE CAME DEBONDED FROM AGE VIBRATION. PLATE WASJun 3, 2004 · N732WP · Cessna T210M · Engine Air Intake SystemSDR PO82004F00000Alternator · failedALTERNATOR FAILED INFLIGHT AFTER 134 HOURS TSO. UNIT SENT OUT TO A CERTIFIED REPAIR STATION FOR REPAIR. TEARDOWN REPORT STATED ONE BAD BEARING AND A FAILED STATOR. PREVIOUS OVERHAULED ALTERNATOR LASTED FIVE MINUTES BEFORE AND THE OVERHAULED UNIT PRIOR TO THMar 1, 2004 · N6246B · Cessna T210M · DC Generator-AlternatorSDR FPI2004F00001Distributor Gear · looseDISTRIBUTOR GEAR FINGER LOOSENED UP AT SHAFT.Feb 17, 2004 · N7398M · Cessna T210M · Magneto/DistributorSDR 2004FA0000021Vernatherm · failedVERNATHERM FAILED TO BYPASS OIL COOLER WHEN OIL TEMPS LOW.Dec 26, 2003 · N732YK · Cessna T210M · Engine Oil Indicating SystemSDR 2003FA0001119Exhaust Valve · wornCYLINDER FAILED COMPRESSION CHECK DUE TO EXHAUST VALVE LEAKAGE. VISUAL INSPECTION REVEALED BURNED EXHAUST VALVE WITH NO SIGNS OF OVER TEMP OR CARBON BUILD UP. VALVE STEM AND GUIDE WORN BEYOND SERVICE LIMITS. EXHAUST VALVES IN CYLINDERS 4 AND 5 EXPERIENCE IDSep 19, 2003 · N732YK · Cessna T210M · Reciprocating Engine Cylinder SectionSDR CA030916002Points · broken(CAN) POINT ASSEMBLY CONTACT ARM FAILED.Sep 15, 2003 · Cessna T210M · Magneto/DistributorSDR RCO2003F00000Alternator · brokenWHILE INSTALLING A 135 AMP ALTERNATOR KIT UNDER A STC FROM MFG, IT LOOKED LIKE THE COOLING FAN PN 8-4 HAD A SMALL CRACK IN IT. THIS PULLEY IS A ONE-PIECE CAST ASSEMBLY MADE OF ALUMINUM. WHEN THE ALTERANTOR WAS REMOVED FOR CLOSER INSP, THE PULLEY WAS FOUND TOJun 6, 2003 · N732XE · Cessna T210M · AC Generator-AlternatorSDR 2003FA0000360Alternator · seizedUPON FIRST START OF THE DAY A LOUD SQUEALING NOISE WAS HEARD ALONG WITH WHITE SMOKE EXITING THE COWL FLAPS AND THE PILOT SHUT DOWN ENGINE. UPON REMOVING THE COWLING IT BECAME OBVIOUS THAT THE ALTERNATOR HAD SEIZED AND THAT THE BELT WAS BADLY BURNED. LATER EXAApr 1, 2003 · N6246B · Cessna T210M · AC Generator-AlternatorSDR FLTICE0303002Control Panel · erraticCPS-OWNER FOUND THAT THE TKS QUANTITY INDICATOR FLUCTUATES IN FLIGHT FROM 9.8 TO LOWER LEVELS. THIS PROBLEM IS INTERMITTENT. REPLACED QUANTITY INDICATOR.Mar 18, 2003 · N77CF · Cessna T210M · Airfoil Anti/De-ice SystemSDR BYK2002F00000Turbocharger · fodTOTAL FAILURE OF TURBO CHARGER DURING TAKE OFF ROLL DUE TO THE STEEL STRIP FOR INDUCTION ALTERNATE AIR DOOR MAGNET WEDGED INTO TURBO INLET BLADES. LEADING EDGES OF ALL INTAKE TURBINE BLADES DAMAGED. DISSIMILAR METAL CORROSION OF STEEL STRIP ATTACHMENT ALUMINNov 19, 2002 · N761HS · Cessna T210M · Exhaust TurbochargerSDR 2002FA0000508Switch · failedGEAR FAILED TO INDICATE UP AND LOCKED ON RETRACTION.Mar 30, 2002 · N732YK · Cessna T210M · Landing Gear Position and WarningSDR 2001FA0000459Cylinder · out of toleranceCUSTOMER COMPLAINED OF INTERMITTENT ROUGHNESS. REMOVAL OF CYLINDERS REVEALED STICKING INTAKE VALVES. GUIDE TO VALVE TOLERANCE TOO TIGHT, BELOW MFG MINIMUM LIMITS. MFG CLAIMS TOLERANCE TOO TIGHT FROM NORMAL OPERATION. NO BUILD UP NOTED OF ANY KIND ON VALVE Sep 28, 2001 · N761RD · Cessna T210M · Reciprocating Engine Cylinder Section
Back to Cessna T210M