# Service difficulty reports: Cessna T210N

A list on [Cessna T210N](https://openairdocs.org/model/cessna-t210n.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 193 reports

- [SDR 2024FA0000620](https://openairdocs.org/sdr/2024FA0000620.md): Alternator · loose · Aug 18, 2024 · N1625U · Cessna T210N · AC Generator-Alternator
  > WE RECENTLY REPLACED AN ALTERNATOR DUE TO THE CHARGING SYSTEM DROPPING OUT IN FLIGHT, AND UPON EXAMINATION OF THE REMOVED ONE, IT WAS FOUND THAT TWO OF THE FOUR CASE SCREWS ARE LOOSE, BUT SAFETY WIRES ARE STILL IN PLACE. PLANE POWER MODEL ASG1200-1-PMA 24V,
- [SDR 2017F00155](https://openairdocs.org/sdr/2017F00155.md): Fuel Nozzle · clogged · Jul 11, 2017 · N6993N · Cessna T210N · Fuel Injector Nozzle
  > POWER LOSS AFTER TAKEOFF RESULTING IN RETURN TO AIRPORT. FUEL FLOW WAS REPORTED HIGH AND MANIFOLD PRESSURE NORMAL. SUSPECTED PARTIALLY PLUGGED FUEL INJECTOR NOZZLE.
- [SDR 2015FA0000496](https://openairdocs.org/sdr/2015FA0000496.md): Hub · cracked · Oct 19, 2015 · N6621A · Cessna T210N · Propeller Hub Section
  > DURING ROUTINE INSPECTION, CRACKS WERE DISCOVERED IN THE HUB AT AFT EDGE, MATING SURFACE TO ENGINE CRANK FLANGE. THE MOST PROMINENT CRACK IS ABOUT.5" LONG. THERE IS NO DAMAGE HISTORY FOR THIS PROP. THE PROP IS INSTALLED UNDER STC SA3104SO TO AN ENGINE INSTA
- [SDR 2015FA0000493](https://openairdocs.org/sdr/2015FA0000493.md): Coil · failed · Oct 12, 2015 · N79ME · Cessna T210N · Magneto/Distributor
  > MAGNETO, SN 14020225 FAILED IN FLIGHT IN JULY 2014. PART TT APPROXIMATELY 16 HOURS. FOUND BAD CONDENSOR ON WARRANTY REPLACEMENT MAGNETO, SN 14020227, PART TT 184. FAILURES AT 16 AND 184 HOURS ARE UNUSUAL. BECAUSE MAGNETOS ARE OFTEN SOLD IN PAIRS IT IS POS
- [SDR 2015FA0000492](https://openairdocs.org/sdr/2015FA0000492.md): Condenser · failed · Oct 12, 2015 · N79ME · Cessna T210N · Magneto/Distributor
  > FOUND BAD CONDENSOR ON MAGNETO, SN 14020225 IN JULY 2014. PART TT APPROXIMATELY 16 HOURS. ON OCTOBER 9, 2015 FOUND BAD CONDENSOR ON WARRANTY REPLACEMENT MAGNETO, SN 14020227, PART TT 184. FAILURES AT 16 AND 184 HOURS ARE UNUSUAL. BECAUSE MAGNETOS ARE OFTEN
- [SDR BGJA20150706001](https://openairdocs.org/sdr/BGJA20150706001.md): Circuit Breaker · failed · Mar 9, 2015 · N39BE · Cessna T210N · Exterior Lighting
  > THE NAVIGATION LIGHTS CB FAILED. THE BREAKER FAILED IN SUCH A WAY THAT THE BREAKER REMAINED IN THE ON POSITION & COULD NOT BE TURNED OFF. THE CLIP INSIDE THE BREAKER HAD BROKEN FREE & THEN FALLEN DOWN INSIDE THE BREAKER WHERE IT HAD WEDGED ITSELF BETWEEN THE
- [SDR 2014FA0000558](https://openairdocs.org/sdr/2014FA0000558.md): Fuel Line · leaking · Sep 25, 2014 · N6355C · Cessna T210N · Aircraft Fuel Distribution System
  > FUEL LINE HAS DARK STAIN HALF WAY BETWEEN ATTACHMENT AND FITTING. LINE PITTED UNDER PLASTIC ANTI-CHAFING MATERIAL, FUEL WEEP CAUSING STAIN. FOUND DURING ANNUAL.
- [SDR BSYA2012063](https://openairdocs.org/sdr/BSYA2012063.md): Indication Sys · malfunctioned · Dec 18, 2013 · N6622N · Cessna T210N · Landing Gear Position and Warning
  > ON FINAL INTO ORL, PILOT WAS NOT GETTING GREEN DOWN & LOCK INDICATION AFTER GEAR WAS SELECTED DOWN. PILOT RECYCLED GEAR & HAND PUMPED, NO HELP. PILOT DID A FLY BY THE TOWER TO VERIFY GEAR WAS DOWN. PILOT PROCEEDED TO LAND AT ORL, GREEN DOWN & LOCK INDICATIO
- [SDR 2013FA0000573](https://openairdocs.org/sdr/2013FA0000573.md): Rudder Bar · broken · Sep 19, 2013 · N5416U · Cessna T210N · Rudder Control System
  > DURING TAXI PILOT WAS ATTEMPTING TO CENTER THE NOSE WHEEL FOR RUN-UP PRIOR TO TAKE-OFF. WHEN PILOT PUSHED LEFT RUDDER PEDAL A LOUD POP WAS HEARD FOLLOWED BY THE LEFT PEDAL GOING LIMP. CO-PILOT STILL HAD FULL CONTROL ON HIS SIDE. CO-PILOT THEN TAXIED BACK TO RA
- [SDR 2013FA0000320](https://openairdocs.org/sdr/2013FA0000320.md): Alternator · inoperative · Jun 5, 2013 · N210VV · Cessna T210N · DC Generating System
  > ACFT LOST ALL ELECTICAL OPERATION IN FLIGHT. ACFT RETURNED TO DEPARTED AIRPORT AND MADE A MANUEL GEAR EXTENTION LANDING AND SAFE ROLL OUT TO THE PARKING RAMP. MX INSPECTED AND TROUBLESHOOT PROBLEM AND FOUND A DEFECTIVE ANTERNATOR. R & R ALTERNATOR WITH O/H
- [SDR CKE2013F00000](https://openairdocs.org/sdr/CKE2013F00000.md): Bushing · loose · Mar 12, 2013 · N5168A · Cessna T210N · Fuel Injector Nozzle
  > FUEL INJECTOR BUSHINGS DID NOT STAY IN PLACE WHEN FUEL INJECTORS WERE REMOVED. INJECTORS WERE REMOVED FOR CLEANING. THIS ENGINE HAS 185 TSMOH AND 5 OUT OF THE 6 BUSHINGS LOOSENED WITH THE INJECTOR. PROBABLE CAUSE IS THAT THE LOCTITE 620 DOES NOT HOLD THE BU
- [SDR 2013FA0000014](https://openairdocs.org/sdr/2013FA0000014.md): Cylinder Head · cracked · Dec 15, 2012 · N4631C · Cessna T210N · Reciprocating Engine Cylinder Section
  > COMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MOR
- [SDR 2013FA0000013](https://openairdocs.org/sdr/2013FA0000013.md): Cylinder Head · cracked · Dec 15, 2012 · N4631C · Cessna T210N · Reciprocating Engine Cylinder Section
  > COMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MOR
- [SDR 2013FA0000012](https://openairdocs.org/sdr/2013FA0000012.md): Cylinder Head · cracked · Dec 15, 2012 · N4631C · Cessna T210N · Reciprocating Engine Cylinder Section
  > COMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS NOT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MOR
- [SDR 2013FA0000011](https://openairdocs.org/sdr/2013FA0000011.md): Cylinder Head · cracked · Dec 15, 2012 · N4631C · Cessna T210N · Reciprocating Engine Cylinder Section
  > COMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MOR
- [SDR 2013FA0000010](https://openairdocs.org/sdr/2013FA0000010.md): Cylinder Head · cracked · Dec 15, 2012 · N4631C · Cessna T210N · Reciprocating Engine Cylinder Section
  > COMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MOR
- [SDR 2013FA0000009](https://openairdocs.org/sdr/2013FA0000009.md): Cylinder Head · cracked · Dec 15, 2012 · N4631C · Cessna T210N · Reciprocating Engine Cylinder Section
  > COMPRESSION CHECK AT ANNUAL REVEALED CRACKED HEAD-AD 2004-08-10 NA DUE TO SN AND "A" STAMP. THIS CYLINDER SEEMS TO HAVE SAME PROBLEM AS AD BUT WAS INT INCLUDED. NOTIFIED MFG. AD MAY NEED TO BE EXPANDED. FURTHER TESTING WITH SCRAP AND WATER. REVEALED 4 MOR
- [SDR 2012FA0000222](https://openairdocs.org/sdr/2012FA0000222.md): Contactor · shorted · Feb 14, 2012 · N9242T · Cessna T210N · Electrical Power System Wiring
  > PILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSP AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE AN ELECT
- [SDR 2012FA0000221](https://openairdocs.org/sdr/2012FA0000221.md): Battery · damaged · Feb 14, 2012 · N9242T · Cessna T210N · Battery/Charger System
  > PILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSP AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE AN ELECT
- [SDR 2012FA0000220](https://openairdocs.org/sdr/2012FA0000220.md): Starter · burned · Feb 14, 2012 · N9242T · Cessna T210N · Engine Starter
  > PILOT REPORTED THAT ON LANDING, ACFT LOST ALL ELECTRICAL POWER. PERFORMED INSPECTION AND TROUBLESHOOTING. FOUND BATTERY, STARTER AND STARTER RELAY AT FAULT. ACFT HAD A BURNED WIRE, ELECTRICAL ODOR. FOUND THAT THE STARTER STAYED ENGAGED AND IT ACTED LIKE AN
- [SDR SQP2011F00000](https://openairdocs.org/sdr/SQP2011F00000.md): Cylinder Head · separated · Aug 29, 2011 · N6993N · Cessna T210N · Reciprocating Engine Cylinder Section
  > PILOT REPORTED LOUD BANG ON CLIMBOUT. RETURNED WITHOUT INCIDENT TO FIELD. UPON EXAMINATION FOUND NR 4 CYLINDER HEAD SEPARATED FROM CYLINDER AT 5TH COOLING FIN ON HEAD. ENGINE TSO AND CYLINDER TSN 817.6 HRS. LAST COMPRESSION CHECK WAS AT 100 HR INSPECTION 1
- [SDR 2010FA0001213](https://openairdocs.org/sdr/2010FA0001213.md): Rod Bolt · loose · Dec 2, 2010 · N6564N · Cessna T210N · Reciprocating Engine Power Section
  > PILOT EXPERIENCED ENGINE SUDDEN STOPPAGE IN FLIGHT AND MADE UNSCHEDULED LANDING. ANALYSIS OF THE CATASTROPHIC ENGINE FAILURE INDICATED FAILURE OCCURED WHEN THE NR5 CONNECTING ROD SEPARATED. THE CAUSE OF FAILURE OF THE CONNECTING ROD WAS A LOOSE ROD BOLT IN THE
- [SDR 2010FA0001177](https://openairdocs.org/sdr/2010FA0001177.md): Case · punctured · Nov 15, 2010 · N6179Y · Cessna T210N · Engine (Reciprocating)
  > PILOT REPORTED LOSSING OIL PRESSURE FOLLOWED BY LOSS OF POWER. AFTER FORCED LANDING ON DIRT ROAD, INSP SHOWED CONNECTING ROD HAD PENETRATED UPPER LT SIDE OF MAIN CASE.
- [SDR 2010FA0000937](https://openairdocs.org/sdr/2010FA0000937.md): Stop Pin · missing · Aug 19, 2010 · N2145U · Cessna T210N · Mixture Control
  > PILOT REPORTED ENGINE WOULD NOT SHUTDOWN WITH MIXTURE LEAN, UPON INSP OF CAUSE, FOUND MIXTURE STOP PIN MISSING AND HAD FALLEN OUT DURING OPERATION.
- [SDR 2010FA0000719](https://openairdocs.org/sdr/2010FA0000719.md): Stator · failed · Jul 10, 2010 · N6638N · Cessna T210N · DC Generator-Alternator
  > STATOR POST ON ALTERNATOR FELL OUT IN FLIGHT, ALTERNATOR FAILED AFTER 44 HOURS SINCE O/H.
- [SDR 2010FA0000030](https://openairdocs.org/sdr/2010FA0000030.md): Adapter · broken · Dec 18, 2009 · N4702C · Cessna T210N · Engine Starter
  > DURING 100HR INSP FOUND GEAR TOOTH IN OIL SUMP DRAIN PLUG. INVESTIGATED, FOUND STARTER DRIVE TOOTH BROKEN AND MATCHED TOOTH TO GEAR. NO FURTHER DAMAGE NOTED.
- [SDR FPI2009F00000](https://openairdocs.org/sdr/FPI2009F00000.md): Attach Bracket · cracked · May 21, 2009 · N2145U · Cessna T210N · Horizontal Stabilizer, Attach Fittings
  > CRACK FOUND IN LT HORIZONTAL STAB BRACE. FOUND DURING 100 HR PHASE INSP.
- [SDR 2008FA0000894](https://openairdocs.org/sdr/2008FA0000894.md): Pump · sheared · Dec 15, 2008 · N5340Y · Cessna T210N · Engine Fuel Pump
  > ON SECOND TEST FLIGHT AFTER FACTORY REBUILT ENG INSTALLATION, ENG QUIT DURING TAKEOFF, JUST AFTER LIFTOFF, ALTITUDE LESS THAN 5 FT AGL. PILOT LANDED ACFT AND ROLLED OUT WITHOUT FURTHER INCIDENT. DURING THIS EVENT, PILOT REPORTED THAT AT TAKEOFF INITIATION, POW
- [SDR 2008FA0000443](https://openairdocs.org/sdr/2008FA0000443.md): Guide · out of tolerance · Jun 17, 2008 · N6621A · Cessna T210N · Reciprocating Engine Cylinder Section
  > AFTER NUMEROUS ATTEMPTS TO TROUBLESHOOT FREQUENT ENGINE MISFIRES OCCURRING PRIMARILY IN THE INITIAL CLIMB STAGES OF FLIGHT, THE ENGINE VALVE TRAIN WAS INSPECTED FOR STICKING VALVES. DIMENSIONAL INSPECTIONS OF THE EXHAUST VALVE GUIDES IN ALL 6 CYLINDERS REVEAL
- [SDR 2008FA0000107](https://openairdocs.org/sdr/2008FA0000107.md): Powerpack · worn · Feb 9, 2008 · N127TC · Cessna T210N · Hydraulic System, Main
  > SMOKE IN COCKPIT, GEAR NOT FULLY RETRACTED, EXTENDED OK. FOUND HYDRAULIC POWERPACK MOTOR (ORIGINAL) WORNOUT. REMOVED AND REPLACED WITH O/H UNIT. OPS, OK.
- [SDR 2007FA0000641](https://openairdocs.org/sdr/2007FA0000641.md): Line · mismanufactured · Jul 6, 2007 · N4631C · Cessna T210N · Aircraft Fuel Distribution System
  > NEW FUEL INJECTOR LINE NR 5 CYL RAM PMA REPLACEMENT. INSTALLED ON ENGINES, WELD DEFECT ALLOWED DEVIPER END BAIL TO COME LOOSE FROM LINE. NOTED FUEL LEAN ON TOP OF ENGINE AT ANNUAL 100 HR INSP. (K)
- [SDR 2007FA0000399](https://openairdocs.org/sdr/2007FA0000399.md): Magneto · corroded · Apr 18, 2007 · N5361Y · Cessna T210N · Magneto/Distributor
  > EMERGENCY RETURN TO FIELD: INSPECTION REQUIREMENTS FOR MAGNETO (PN 6320) ARC NOT ADEQUATE TO INSURE PROPER VENTING (PRESSURIZED MAG). SB2-80C SPECIFIES ONLY EXTERNAL INSPECTION IS REQUIRED EVERY 100 HOURS AND AN INTERNAL INSPECTION AFTER 500 HOURS. THE SUBE
- [SDR 2007FA0000398](https://openairdocs.org/sdr/2007FA0000398.md): Magneto · corroded · Apr 18, 2007 · N5361Y · Cessna T210N · Magneto/Distributor
  > EMERGENCY RETURN TO FIELD: INSPECTION REQUIREMENTS FOR MAGNETO (PN 6320) ARC NOT ADEQUATE TO INSURE PROPER VENTING (PRESSURIZED MAG). SB 2-80C SPECIFIES ONLY EXTERNAL INSPECTION IS REQUIRED EVERY 100 HOURS AND AN INTERNAL INSPECTION AFTER 500 HOURS. THE SUB
- [SDR 2006FA0001202](https://openairdocs.org/sdr/2006FA0001202.md): Turbocharger · failed · Oct 6, 2006 · N6363L · Cessna T210N · Exhaust Turbocharger
  > NEW TURBO ASSY WAS INSTALLED 6/30/06. FOUR MONTHS LATER ON 10/6/06 (41 HOURS TT) THE TURBO SHAFT TIGHTENED UP ENOUGH TO NOT PRODUCE TAKEOFF POWER ON NEXT FLIGHT. OIL PRESSURE AND OIL VOLUME DELIVERED TO TURBO BEARINGS WAS VERIFIED TO BE ADEQUATE. CUSTOMER P
- [SDR 2006FA0000718](https://openairdocs.org/sdr/2006FA0000718.md): Elt · inoperative · Jul 13, 2006 · N178JD · Cessna T210N · Emergency Locator Beacon
  > FOUND ELT TOTALLY INOPERATIVE DURING ANNUAL INSPECTION, BATTERY VOLTAGE OK. UNABLE TO DETERMINE IF IMPACT SWITCH WAS ALSO INOPERATIVE. (K)
- [SDR 2006FA0001201](https://openairdocs.org/sdr/2006FA0001201.md): Turbocharger · failed · Jun 30, 2006 · N6363L · Cessna T210N · Exhaust Turbocharger
  > NEW TURBO ASSY WAS INSTALLED 3/27/2006. (3) MONTHS LATER ON 6/30/06 (32 HOURS TT) THE TURBO SHAFT TIGHTENED UP ENOUGH TO NOT PRODUCE TAKEOFF POWER ON NEXT FLIGHT. OIL PRESSURE AND OIL VOLUME DELIVERED TO TURBO BEARINGS WAS VERIFIED TO BE ADEQUATE. CUSTOMER
- [SDR 2006FA0000514](https://openairdocs.org/sdr/2006FA0000514.md): Cylinder · eroded · Apr 20, 2006 · N5337Y · Cessna T210N · Reciprocating Engine Cylinder Section
  > FOUND NR 6 PISTON ERODED FROM POSSIBLE DETONATION BY UNKNOWN CAUSES. FOUND NR5 CYLINDER CONNECTING ROD CAP MISSING AND INTERNAL DAMAGE TO THE CRANKCASE. NO OIL WAS NOTED ON THE DIPSTICK PRESUMED TO BE FORCED OUT OF THE ENGINE DUE TO EXCESSIVE BLOW BY FROM TH
- [SDR 2006FA0001070](https://openairdocs.org/sdr/2006FA0001070.md): Bearing · seized · Feb 23, 2006 · N6622N · Cessna T210N · Engine Starter
  > OVERHAULER W/O NR 84062, O/H DATE 10/06/2006. STARTER BEARING SEIZED AFTER INSTALLATION STARTER MOTOR FAILED. (K)
- [SDR CA060201001](https://openairdocs.org/sdr/CA060201001.md): Spar · cracked · Feb 1, 2006 · Cessna T210N · Wing Spar
  > A 100 HR INSPECTION WAS STARTED A CRACK WAS DISCOVERED AT THE RIGHT FRONT SPAROUT BOARD END WHERE IT ATTACHES TO THE SUB SPAR. THE CRACK IS VERTICAL RUNNING APPROXIMATELY 1 1/2 TO TWO INCHES IN LENGTH. THE CRACK STARTS AT THE TOP AND RUNS DOWN THROUGH A RIVE
- [SDR 2005FA0001242](https://openairdocs.org/sdr/2005FA0001242.md): Pin · backed out · Aug 29, 2005 · N6239Y · Cessna T210N · Elevator Tab Control System
  > THE PIN THAT HOLDS THE DRIVE GEAR ONTO THE ACTUATOR DRUM HAD FALLEN OUT WHEN THE AIRCRAFT WAS TRIMMED NOSE UP. THE PILOT HAD TO PUSH ON THE YOKE WITH GREAT FORCE TO PITCH THE AIRCRAFT DOWN. AFTER EXAMINING THE ACTUATOR I NOTICED THAT THE HOLE FOR THE PIN WAS E
- [SDR 2005FA0001238](https://openairdocs.org/sdr/2005FA0001238.md): Pin · backed out · Aug 29, 2005 · N6239Y · Cessna T210N · Elevator Tab Control System
  > THE PIN THAT HOLDS THE DRIVE GEAR ONTO THE ACTUATOR DRUM HAD FALLEN OUT WHEN THE AIRCRAFT WAS TRIMMED NOSE UP. THE PILOT HAD TO PUSH ON THE YOKE WITH GREAT FORCE TO PITCH THE AIRCRAFT DOWN. AFTER EXAMINING THE ACTUATOR, NOTICED THAT THE HOLE FOR THE PIN WAS E
- [SDR 2005FA0001204](https://openairdocs.org/sdr/2005FA0001204.md): Alternator · seized · Aug 23, 2005 · N5416U · Cessna T210N · DC Generator-Alternator
  > AIRCRAFT WAS RUN UP PRIOR TO 50 HOUR INSPECTION AND NO DEFECTS WERE FOUND DURING RUN UP. AFTER INSPECTION, PERFORMED POST INSPECTION RUN AND NOTICED A LOUD SQUEALING NOISE AND SMOKE COMING FROM ENGINE COMPARTMENT. ENGINE WAS SHUTDOWN AND INSPECTION REVEALED TH
- [SDR 2005FA0001133](https://openairdocs.org/sdr/2005FA0001133.md): Cylinder Head · damaged · Jul 19, 2005 · N50QH · Cessna T210N · Reciprocating Engine Cylinder Section
  > DURING CRUISE FLIGHT, A LOUD BANG FROM THE ENGINE COMPARTMENT WAS FOLLOWED BY LOSS OF POWER AND SIGNIFICANT ENGINE VIBRATION. THE PILOT MADE AN EMERGENCY LANDING ON A DIRT ROAD WITH NO DAMAGE TO THE AIRCRAFT. THE NR 1 CYLINDER HEAD HAD FRACTURED COMPLETELY T
- [SDR 2005FA0000999](https://openairdocs.org/sdr/2005FA0000999.md): Cylinder Head · separated · Jun 1, 2005 · N7235F · Cessna T210N · Reciprocating Engine Cylinder Section
  > NR 2 CYLINDER HEAD SEPARATED FROM BARREL. OCURRENCE OCCURRED DURING DEPARTURE FROM AIRPORT, ENROUTE. PROBABLE CAUSE IS WORN CYLINDER OR POSSIBLE OVERBOOST. RECOMMEND WHEN PERFORMING COMPRESSION TEST THAT YOU PRESSURIZE AND SOAP CYLINDER AT BARREL AND HEAD A
- [SDR 2005FA0000586](https://openairdocs.org/sdr/2005FA0000586.md): Governor · plugged · Apr 10, 2005 · N5130A · Cessna T210N · Propeller Governor
  > DEPARTING SOFT FIELD POWER AND RPM FINE ON INITIAL ROLL. AFTER WHEELS BECAME LIGHT, POWER BLED OFF, YIELDING NO FURTHER ACCELERATION OR LIFT. ABORTED TAKE-OFF, NOSE WHEEL GOUGED INTO SOFT SAND, BREAKING NOSE FORK, PITCHING NOSE OF AIRCRAFT INTO DIRT. PROP B
- [SDR 2005FA0000580](https://openairdocs.org/sdr/2005FA0000580.md): Encoder · erratic · Mar 11, 2005 · N5434A · Cessna T210N · Altimeter, Barometric/Encoder
  > ALTITUDE OUTPUT BECAME ERRATIC, VARYING SEVERAL HUNDRED FT BOTH ABOVE AND BELOW THE ACTUAL ALTITUDE OVER A PERIOD OF 30 MINUTES. PROBABLY CAUSED BY INTERMITTENT HEATER THERMOSTAT.
- [SDR 2005FA0000216](https://openairdocs.org/sdr/2005FA0000216.md): Connecting Rod · failed · Feb 9, 2005 · N5130A · Cessna T210N · Reciprocating Engine Power Section
  > NR 2 CONNECTING ROD FAILED BREAKING CRANKCASE, KNOCKING LT MAG FROM MOUNT. ROD SHOWED FRICTION WELDING TO CRANK PRIOR TO FAIURE. COUNTERWEIGHT DAMAGED BY IMPACT WITH ROD. APPEARS ENG CONTINUED TO OPERATE BRIEFLY FOLLOWING ROD SEIZURE. PILOT ACCOMPLISHED SU
- [SDR B3OR20040719](https://openairdocs.org/sdr/B3OR20040719.md): Hinge · loose · Jul 19, 2004 · N5515Y · Cessna T210N · Engine Air Intake System
  > ANNUAL INSP, ALTERNATE AIR SOURCE DOOR WAS LOOSE. MECHANIC FOUND DOOR SPRING P/N 1250728-1, HINGE PIN P/N MS20253P2-364 IN INDUCTION AIR BOX DUCTING. PIN AND SPRING WERE RE-ASSEMBLED WITH DOOR. WHEN PARTS WERE RE-ASSEMBLED, BOTH UPPER AND LOWER ENDS OF HINGE
- [SDR CA050125015](https://openairdocs.org/sdr/CA050125015.md): Piston · disintegrated · Jul 16, 2004 · Cessna T210N · Reciprocating Engine Power Section
  > (CAN) ENGINE HAD 450 HOURS SINCE TOTAL O/H, WAS PERFORMING NORMAL. CYL LEAK TEST WERE MIN. 60/80 AND OIL CONSUMPTION WAS 1 LT-13 HRS. AC WAS IN BASE LEG WITH POWER REDUCED GRADUALLY BACK TO 20 IN., PROP NEAR FINE, MIXTURE NEAR RICH. VIBRATION STARTED IN ENG
- [SDR B3OR20040709](https://openairdocs.org/sdr/B3OR20040709.md): Line · cut · Jul 9, 2004 · N5515Y · Cessna T210N · Landing Gear Brake System
  > PILOTS ENTERED THE AC AND TAXIED DOWN THE TAXIWAY. AS BRAKES WERE BEING APPLIED, IT WAS NOTICED THAT RT BRAKE WAS NOT OPERATING. AC EXITED TAXI WAY AT A LOW SPEED CAME TO A STOP IN ABOUT FOUR INCHES OF MUD ALONGSIDE OF TAXIWAY. THERE WAS NO DAMAGE TO AC OR PRO

Next page: https://openairdocs.org/model/cessna-t210n/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'T210N'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-t210n/reports

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