# Service difficulty reports: Cessna P210N

A list on [Cessna P210N](https://openairdocs.org/model/cessna-p210n.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 97 reports

- [SDR 2025FA0000674](https://openairdocs.org/sdr/2025FA0000674.md): Pin · disengaged · Oct 1, 2025 · N4925K · Cessna P210N · Flight Compartment Equipment
  > SEAT BACK CAM RETAINING PINS LOOSE, MISSING AND OR SHEARED FOUND SAFETY-WIRED IN PLACE. THERE APPEARS TO BE MANY OF THESE INFINITE ADJUSTABLE LOWER SEAT FRAMES WITH THE NAS SPLIT-PINS SAFETY-WIRED IN PLACE. THERE IS NO REQUIREMENT TO ADD SAFETY-WIRE TO THESE S
- [SDR 2025FA0000374](https://openairdocs.org/sdr/2025FA0000374.md): Pump · leaking · May 23, 2025 · N6320P · Cessna P210N · Hydraulic Pump (Electric/Engine), Main
  > FAILED DURING LANDING. UPON INSPECTION AFTER A COLLAPSE OF LANDING GEAR UPON TOUCHDOWN INCIDENT, THE HYDRAULIC PUMP WAS FOUND TO BE LEAKING INTERNALLY.
- [SDR 2023FA0000117](https://openairdocs.org/sdr/2023FA0000117.md): Barrel · broken · Mar 8, 2023 · N66WS · Cessna P210N · Landing Gear Retraction/Extension System
  > THE SHAPE OF THE FORWARD NOSE GEAR DOOR HINGES DO NOT ALLOW THE DOORS TO OPEN WITH THE BARREL LINKAGE DISCONNECTED. IF THE BARREL LINKAGE BREAKS, THE NOSE GEAR WILL NOT PUSH THE GEAR DOORS OPEN. IF THE HINGES WERE SHAPED SLIGHTLY DIFFERENT, THIS PROBLEM WOULD
- [SDR 2020FA0000381](https://openairdocs.org/sdr/2020FA0000381.md): Drive Belt · broken · Jul 31, 2020 · N4840K · Cessna P210N · DC Generator-Alternator
  > WHILE INBOUND TO SNA THE AIRCRAFT RADIOS WENT DEAD AND THE BATTERY WENT DEAD. THE PILOT CONTACTED SNA TOWER USING HIS CELL PHONE AND WAS CLEARED TO LAND. AFTER LANDING IT WAS DISCOVERED THE ALTERNATOR DRIVE BELT FAILED AND THE AIRCRAFT WAS RUNNING ON BATTERY
- [SDR M3VY2018071600239](https://openairdocs.org/sdr/M3VY2018071600239.md): Radar · damaged · Mar 22, 2018 · N67JK · Cessna P210N · Weather Radar System
  > WEATHER RADAR POD. DURING ANNUAL INSPECTION IT WAS NOTED THAT THE RADAR SUPPORT POD WAS GAPING BY APPROX 1/2 INCH AT THE REAR END AND THE BLACK WEATHER SEAL WAS DISPLACED. ON FURTHER INVESTIGATION IT WAS ESTABLISHED THAT THE REAR POD SUPPORT WAS LOOSE. ON R
- [SDR 2018FA0000440](https://openairdocs.org/sdr/2018FA0000440.md): Lifter · spalled · Feb 14, 2018 · N4752K · Cessna P210N · Reciprocating Engine Power Section
  > DAMAGED BEYOND REPAIR.
- [SDR AK62018F00000](https://openairdocs.org/sdr/AK62018F00000.md): Brace · cracked · Nov 1, 2017 · N507HH · Cessna P210N · Nose/Tail Landing Gear Attach Section
  > THE LEFT NOSE TRUNNION SUPPORT BRACE HAD A STRESS CRACK AT THE TRUNNION MOUNT EAR. THE CRACK FINALLY CAUSED A FAILURE ON TAKEOFF AT KACT ON 10/25/2017. THIS FAILURE IN TURN CAUSED THE RIGHT TRUNNION SUPPORT TO FAIL AND ULTIMATELY COMPLETE NOSE GEAR COLLAPSE.
- [SDR 2016FA0000306](https://openairdocs.org/sdr/2016FA0000306.md): Return Spring · broken · Jun 23, 2016 · N210PF · Cessna P210N · Propeller Controlling System
  > WHILE IN CRUISE FLIGHT ABOVE 10,000 FEET, THERE WAS INSUFFICIENT PITCH TO REDUCE RPM TO CRUISE CONDITION. PROPELLER HUB DISASSEMBLED, AND FOUND A BROKEN PROPELLER RETURN SPRING WAS INTERFERING WITH THE HIGH PITCH STOP, SUCH THAT ONLY 27 DEGREES OF PITCH WERE
- [SDR 2016FA0000028](https://openairdocs.org/sdr/2016FA0000028.md): Line · leaking · Jan 26, 2016 · N4988 · Cessna P210N · Aircraft Fuel Distribution System
  > DURING ANNUAL INSPECTION, A FUEL ODOR WAS NOTED IN THE COCKPIT. INVESTIGATION FOUND THE ALUMINUM FUEL PRESSURE LINE HAS CORRODED THROUGH AT THE POINT WHERE A WIRE BUNDLE WAS ZIP TIED AGAINST THE FUEL PRESSURE LINE.
- [SDR ZSDA2014082200001](https://openairdocs.org/sdr/ZSDA2014082200001.md): Brake Sys · contaminated · Aug 6, 2014 · N731CY · Cessna P210N · Landing Gear Brake System
  > AIRCRAFT DEPARTED TAXIWAY. NO DAMAGE TO AIRCRAFT. AIRCRAFT TOWED TO HANGAR. FOUND AIR BUBBLES IN BRAKE LINE WHILE BLEEDING BRAKES. TOPPED OFF RESERVOIR. INSPECTED FOR LEAKS, NONE. FOUND BRAKE PEDAL WAS FIRM. RETURNED ACFT TO SERVICE.
- [SDR 2013FA0000470](https://openairdocs.org/sdr/2013FA0000470.md): Pin · broken · Aug 15, 2013 · N6328P · Cessna P210N · Nose/Tail Landing Gear Strut/Axle
  > NOSE GEAR COLLASPED ON LANDING ROLL OUT. THERE ARE 2 PINS INSTALLED IN THE END OF THE NOSE GEAR ACTUATOR BEARING END. THE DOWN LOCK HOOKS ENGAGE ON THESE 2 PINS IN THE DOWN POSITION. THESE PINS ARE HELD IN PLACE BY A ROLL PIN THROUGH THE BEARING END INTO A
- [SDR 2013FA0000174](https://openairdocs.org/sdr/2013FA0000174.md): Barrel · separated · Mar 18, 2013 · N44475 · Cessna P210N · Reciprocating Engine Cylinder Section
  > NR 2 CYLINDER BARREL SEPARATED FROM HEAD DURING FLIGHT. ENGINE STARTED RUNNING ROUGH AND PILOT RETURNED TO THE AIRPORT.
- [SDR 2011FA0000414](https://openairdocs.org/sdr/2011FA0000414.md): Cylinder · peeling · Apr 20, 2011 · Cessna P210N · Reciprocating Engine Cylinder Section
  > THE NICKLE HAS PEELED AWAY FROM THE CYLINDER WALL CREATING A METAL CONTAMINATION OF THE ENGINE.
- [SDR 2011F00084](https://openairdocs.org/sdr/2011F00084.md): Cylinder · peeling · Apr 20, 2011 · Cessna P210N · Reciprocating Engine Cylinder Section
  > THE NICKLE HAS PEELED AWAY FROM THE CYLINDER WALL CREATING A METAL CONTAMINATION OF THE ENGINE.
- [SDR 2011FA0000323](https://openairdocs.org/sdr/2011FA0000323.md): Cylinder · delaminated · Apr 20, 2011 · Cessna P210N · Reciprocating Engine Cylinder Section
  > NICKLE PULLED AWAY FROM BARREL OF CYLINDER.
- [SDR 2009FA0000146](https://openairdocs.org/sdr/2009FA0000146.md): Torque Link · bent · Feb 12, 2009 · N4740K · Cessna P210N · Landing Gear System
  > WE ARE FINDING SEVERAL DEFECTIVE UPPER TORQUE LINKS BENT, CRACKED OR BOTH WITH INCREASING POTENTIAL FOR FAILURE. (K)
- [SDR 2007FA0001045](https://openairdocs.org/sdr/2007FA0001045.md): Alternator · failed · Nov 13, 2007 · N4814K · Cessna P210N · AC Generation System
  > DURING NIGHT IMC APPROACH, LOW VOLTAGE LIGHT ILLUMINATED AND BUS VOLTAGE DROPPED BELOW 24 VOLTS. PILOT RECYCLED ALTERNATOR SWITCH BUT WAS UNABLE TO KEEP ALTERNATOR ON LINE. PILOT REDUCED LOADS AND SUCCESSFULLY EXECUTED APPROACH AND LANDED WITHOUT INCIDENT.
- [SDR 2007FA0001046](https://openairdocs.org/sdr/2007FA0001046.md): Alternator · failed · Nov 10, 2007 · N4814K · Cessna P210N · AC Generation System
  > DURING DAY VMC FLIGHT, LOW VOLTAGE LIGHT ILLUMINATED AND BUS VOLTAGE DROPPED BELOW 24 VOLTS. PILOT MINIMIZED LOADS, DID A MANUAL GEAR EXTENSION, AND LANDED WITHOUT INCIDENT. CHARGING SYSTEM TROUBLESHOOT BY MECHANIC. FOUND ALTERNATOR OUTPUT TO BE 26 VOLTS UN
- [SDR 2006FA0000469](https://openairdocs.org/sdr/2006FA0000469.md): Turbocharger · leaking · Apr 26, 2006 · N4773P · Cessna P210N · Exhaust Turbine System (Reciprocating)
  > OIL LEAKING OUT FROM JOINT IN CENTER OF TURBO. FIRST RUN ON OVERHAULED UNIT JUST INSTALLED ON AIRCRAFT. (K)
- [SDR AU510001658](https://openairdocs.org/sdr/AU510001658.md): Cylinder · failed · Dec 12, 2005 · Cessna P210N · Reciprocating Engine Cylinder Section
  > NR 2 CYLINDER HEAD SEPARATED FROM BARREL. FURTHER INVESTIGATION FOUND THAT ALL CYLINDERS (6OFF) SHOULD HAVE BEEN REPLACED IN JULY 2004 IAW ECI SB 04-1.
- [SDR 2005FA0001135](https://openairdocs.org/sdr/2005FA0001135.md): Switch · broken · Aug 7, 2005 · N152BT · Cessna P210N · Landing Gear Retraction/Extension System
  > NO CONFIRMATION OF LANDING GEAR DOWN AND LOCKED. NO GREEN LIGHTS. GEAR APPEARED DOWN VISUALLY. ON INSPECTION ONCE ON THE GROUND IT WAS DOWN AND PROPERLY LOCK. MALFUNCTION WAS THE GEAR INDICATOR POSITION MICRO SWITCH ON THE LT MAIN BROKEN WIRE AT THE SWITC
- [SDR 2005FA0000872](https://openairdocs.org/sdr/2005FA0000872.md): Valve · misinstalled · Jun 7, 2005 · N4946K · Cessna P210N · Exhaust Turbocharger
  > RECEIVED TURBO CHARGER CHECK VALVE AND INSTALLED IN CORRECT ORIENTATION. RAN ENGINE AND THE TURBO CHARGER CAVITATED DUE TO LOSS OF OIL SUPPLY. FURTHER INVESTIGATION REVEALED THE NEW CHECK VALVE WAS BACKWARDS INTERNALLY IE: THE CHECK VALVE WAS AT THE OPPOSITE
- [SDR 2005FA0000795](https://openairdocs.org/sdr/2005FA0000795.md): Alternator · burned out · May 26, 2005 · N732RS · Cessna P210N · AC Generation System
  > OWNER STARTED HEARING RADIO STATIC AND AFTER A FEW MINUTES, LOST ELECTRICAL POWER. ON THE GROUND, MECHANIC CHECKED REGULATOR, CHECKED OK, CHANGED ALTERNATOR OPS CHECKED OK. PART ONLY HAS 68 HOURS ON THE OVERHAUL.
- [SDR 2005FA0000127](https://openairdocs.org/sdr/2005FA0000127.md): Heater · cracked · Oct 25, 2004 · N43CE · Cessna P210N · Air Intake Anti/De-Ice System
  > PILOT REPORTED SMELLING A BURNED ODOR WHILE DESCENDING IN SEVERE ICING CONDITIONS. ON A POST FLIGHT INSPECTION OF THE AIRCRAFT A V SHAPED CRACK WITH THE TIP MISSING WAS FOUND IN THE ENGINE INLET HEATER. IT APPEARS THAT PART OF THE HEATER HAS SHORTED OUT CAUS
- [SDR 2004FA0000675](https://openairdocs.org/sdr/2004FA0000675.md): Crankshaft · broken · Jul 20, 2004 · N7736K · Cessna P210N · Reciprocating Engine Power Section
  > TSIO-520-T CRANKSHAFT BROKE AT 1776 HOURS SINCE FACTORY REMANUFACTURE. OPERATED BEYOND RECOMMENDED OVERHAUL, CRANK FAILED CAUSING UNSCHEDULED LANDING THAT RESULTED IN AN AIRCRAFT ACCIDENT.
- [SDR TRK2004F00000](https://openairdocs.org/sdr/TRK2004F00000.md): Pulley · separated · Jul 1, 2004 · N210TS · Cessna P210N · AC Generation System
  > THE ALTERNATOR WAS REPLACED AND THE NUT FOR THE PULLEY WHICH IS PART OF THE STC WAS TORQUED IAW THE STC. APPROXIMATELY 10 HOURS LATER THE PULLEY CAME OFF THE ALTERNATOR. THERE IS NO WOODRUFF KEY, TAPERED PULLEY SHAFT OR ANY TYPE OF SAFETY USED DURING THE INS
- [SDR 2004FA0000231](https://openairdocs.org/sdr/2004FA0000231.md): Actuator · cracked · Apr 23, 2003 · N210PF · Cessna P210N · Landing Gear Actuator
  > LT MLG ACTUATOR CRACKED ALLOWING ALL HYDRAULIC FLUID TO LEAK OB ON RETRACTION AFTER TAKEOFF. COULD NOT EXTEND LANDING GEAR WHICH RESULTED IN A GEAR UP LANDING. NOTE, THIS ACTUATOR WAS PREVIOUSLY OVERHAULED ON 04/21/1983 AT 833 HOURS TIME IN SERVICE. THERE A
- [SDR 2003FA0000373](https://openairdocs.org/sdr/2003FA0000373.md): Lifter · spalled · Mar 28, 2003 · N102KY · Cessna P210N · Reciprocating Engine Cylinder Section
  > REMOVED NR 2 CYL FOR BLOW BY. PULLED LIFTER ASSEMBLY TO INSPECTION CONDITION FOUND EXHAUST LIFTERBODY SPALLING. DISASSEMBLED ENGINE SENT CAM OUT. CAM WAS ALSO BAD, COULD NOT BE RECONDITIONED.
- [SDR 2003FA0000587](https://openairdocs.org/sdr/2003FA0000587.md): Distributor Gear · failed · Mar 26, 2003 · N82DF · Cessna P210N · Magneto/Distributor
  > THIS PRESSURIZED MAGNETO WAS REMOVED AND DISASSEMBLED FOR THE 500 HOUR INSPECTION. ALL THE INTERNAL HARDWARE WAS FOUND RUSTED. THE DISTRIBUTOR GEAR, DRIVE GEAR AND DISTRIBUTOR BLOCK WAS FOUND COVERED IN A FILM AND NOTICEABLY SOFTER THAN NEW EXAMPLES. THIS I
- [SDR 2003FA0000586](https://openairdocs.org/sdr/2003FA0000586.md): Distributor Gear · damaged · Mar 26, 2003 · N82DF · Cessna P210N · Magneto/Distributor
  > THIS PRESSURIZED MAGNETO WAS REMOVED AND DISASSEMBLED FOR THE 500 HOUR INSPECTION. ALL OF THE INTERNAL HARDWARE WAS FOUND RUSTED. THE DISTRIBUTOR GEAR, DRIVEGEAR AND DISTRIBUTOR BLOCK WAS FOUND COVERED IN A FILM AND NOTICEABLY SOFTER THAN NEW EXAMPLES. THIS
- [SDR CA030409005](https://openairdocs.org/sdr/CA030409005.md): Crankcase · damaged · Jan 31, 2003 · Cessna P210N · Reciprocating Engine Power Section
  > (CAN) AT INSPECTION A SMALL AMOUNT OF ALUMINIUM WAS FOUND IN THE OIL FILTER. CYLINDERS WERE REMOVED FROM THE ENGINE TO INVESTIGATE THE SOURCE OF THE FILTER CONTAMINATION. IT WAS FOUND THAT THE NR 2 MAIN BEARING HAD SHIFTED FORWARD AND WAS LOOSE CAUSING WEAR IN
- [SDR 2003FA0000397](https://openairdocs.org/sdr/2003FA0000397.md): Bumper Block · debonded · Nov 26, 2002 · N5555S · Cessna P210N · Landing Gear Retraction/Extension System
  > LT AND RT MAIN LANDING GEAR SHELL BUMPER DEBONDS, THE BUMPER EDGES CURL OVER PREVENTING MAIN GEAR STRUT FROM MAKING FULL DOWN TRAVEL. THIS CONDITION PREVENTS MAIN GEAR STRUT FROM CONTACTING DOWNLOCKS AND PROPER DOWNLOCK SWITCH ACTUATION, THEREFORE AN UNSAFE C
- [SDR AUS20020547](https://openairdocs.org/sdr/AUS20020547.md): Csu · faulty · Mar 5, 2002 · Cessna P210N · Propeller Governor
  > (AUS) PROPELLER GOVERNOR (CSU) FAULTY. SUSPECT CAUSED BY FAULTY SPEEDER SPRING.
- [SDR F342002F00000](https://openairdocs.org/sdr/F342002F00000.md): Downlock Switch · inoperative · Jan 2, 2002 · N102KY · Cessna P210N · Landing Gear Position and Warning
  > AIRCRAFT WAS IN THE PROCESS OF LANDING WHEN A PASSENGER NOTICED THE RIGHT GER TRAILING AND NOT IN THE DOWN AND LOCK POSITION. AFTER SEVERAL ATTEMPTS TO PUT GEAR DOWN ELECTRICALLY, PILOT PUMPED THE GEAR DOWN MANUALLY INTO LOCK POSITION. UPON TROUBLE SHOOTING,
- [SDR CA011219004](https://openairdocs.org/sdr/CA011219004.md): Trunnion · cracked · Dec 5, 2001 · Cessna P210N · Nose/Tail Landing Gear
  > (CAN) NOSE LANDING GEAR LOWER TRUNNION FOUND CRACKED.
- [SDR 2003FA0000400](https://openairdocs.org/sdr/2003FA0000400.md): Bumper Block · debonded · Aug 16, 2001 · N5555S · Cessna P210N · Landing Gear Retraction/Extension System
  > LT AND RT MAIN LANDING GEAR SHELL BUMPER DEBONDS. THE BUMPER EDGES CURL OVER PREVENTING MAIN GEAR STRUT FROM MAKING FULL DOWN TRAVEL. THIS CONDITION PREVENTS MAIN GEAR STRUT FROM CONTACTING DOWNLOCKS AND PROPER DOWNLOCK SWITCH ACTUATION, THEREFORE, AN UNSAFE
- [SDR AUS20010778](https://openairdocs.org/sdr/AUS20010778.md): Clamp · broken · Jul 23, 2001 · Cessna P210N · Engine Collector/Tailpipe/Nozzle
  > (AUS) ENGINE FORWARD LH EXHAUST CLAMP BROKEN. FORWARD AIRFRAMESTRUCTURE, COWL AND NOSE TYRE TORCHED.
- [SDR 20010507CW003](https://openairdocs.org/sdr/20010507CW003.md): Alternator · malfunctioned · Apr 18, 2001 · N456BR · Cessna P210N · AC Generator-Alternator
  > AIRCRAFT UNDER IMC WHEN LOW VOLT LIGHT CAME ON AND VOLTAGE DROP TO 23.0 VOLTS. PILOT SHUT EVERYTHING OFF AND DECLARED AN EMERGENCY WITH CASCADE APPROACH. LANDED WITHOUT INCIDENT. PART WAS UNDER WARRANTY SO COULD NOT DISASSEMBLE TO FIND OUT CAUSE OF FAILURE,
- [SDR CA001229012](https://openairdocs.org/sdr/CA001229012.md): Reservoir · cracked · Dec 4, 2000 · Cessna P210N · Fuel Storage
  > (CAN) FOUND FUEL STAINING AROUND THE AFT FUEL INLET ON BOTH FUEL RESERVOIRS (FUEL ODOUR NOTICEABLE). REMOVED TANKS AND INSPECTED, FOUND VERY SMALL HAIRLINE CRACKS ON THE OUTER EDGE OF THE WELD. 16X MAGNIFYING GLASS HELPED TO IDENTIFY CRACK.
- [SDR 20001017SH033](https://openairdocs.org/sdr/20001017SH033.md): Regulator · shorted · Sep 18, 2000 · N734JV · Cessna P210N · DC Regulator
  > PILOT EXPERIENCED ELECTRICAL POWER FAILURE. NEW ALTERNATOR INSTALLED. PILOT DEPARTED EN ROUTE HOME WHEN ELECTRICAL POWER WAS LOST AGAIN 9-19-2000. MAINT REPLACED VOLTAGE REGULATOR. THIS IS THE SECOND INCIDENT. IN TWO YEARS, BOTH TIMES THE INDIVIDUAL COMPO
- [SDR 20000912SH009](https://openairdocs.org/sdr/20000912SH009.md): Crankshaft · failed · Aug 24, 2000 · N5256W · Cessna P210N · Reciprocating Engine Power Section
  > ENGINE FAILED AFTER TAKEOFF RESULTING IN FORCED LANDING. INSPECTION OF ENGINE REVEALED CRANKSHAFT FAILED BETWEEN THE NR 2 AND NR 3 JOURNALS. (X)
- [SDR 2003FA0000395](https://openairdocs.org/sdr/2003FA0000395.md): Bumper Block · debonded · Jul 14, 2000 · N5555S · Cessna P210N · Landing Gear Retraction/Extension System
  > LEFT AND RIGHT MAIN LANDING GEAR SHELL BUMPER DEBONDS, THE BUMPER EDGES CURL OVER PREVENTING MAIN GEAR STRUT FROM MAKING FULL DOWN TRAVEL. THIS CONDITION PREVENTS MAIN GEAR STRUT FROM CONTACTING DOWNLOCKS AND PROPER DOWNLOCK SWITCH ACTUATION, THEREFORE, AN U
- [SDR 20010419CW011](https://openairdocs.org/sdr/20010419CW011.md): Helicoil · dislodged · Jun 27, 2000 · N6612W · Cessna P210N · Reciprocating Engine Cylinder Section
  > PILOT REPORTED THAT AN ENGINE FAILURE OCCURRED DURING FLIGHT WITH UNEVENTFUL LANDING. PILOT INFORMED TECHS THT THE TOP SPARK PLUG HAD BECOME REMOVED FROM THE NR 1 CYLINDER. UPON ARRIVAL TO THE AIRCRAFT, FOUND TOP COWLINGS REMOVED AND THE NR 1 TOP SPARK PLUG
- [SDR 20000331SH024](https://openairdocs.org/sdr/20000331SH024.md): Blade · misoverhauled · Mar 1, 2000 · N4783K · Cessna P210N · Propeller Blade Section
  > PROPELLER VIBRATING AFTER RECENT OVERHAUL. DYNAMIC BALANCING HELPED. FOUND 7 AN 97-3 WASHERS FOR DYNAMIC BALANCE ADDED 6 MORE TO BRING BALANCE TO A 1 IPS. ALSO FOUND 6 STATIC WEIGHTS IN SAME LOCATION. REMOVED PROP FROM AIRCRAFT TO CHECK STATIC BALANCE. CO
- [SDR 20000712SH027](https://openairdocs.org/sdr/20000712SH027.md): Propeller · malfunctioned · Nov 1, 1999 · N4706A · Cessna P210N · Propeller System
  > PROPELLER IS UNCONTROLLABLE, TO LOWER PITCH, AT HIGH ALTITUDE (COLD TEMPERATURE). NEW PROPELLER FROM MANUFACTURER. INSTALLED SERVICEABLE PROPELLER. ALL SYSTEMS WORK NORMALLY. INSTALLED ANOTHER NEW PROPELLER, ALL SYSTEMS WORK NORMALLY. POSSIBLE WRONG GREAS
- [SDR 99ZZZX4160](https://openairdocs.org/sdr/99ZZZX4160.md): Relay · failed · Sep 21, 1999 · N323DC · Cessna P210N · Flight Compartment Windows
  > THIS RELAY SUPPLIES POWER TO THE WINDSHIELD HEATING PANEL AND IS CONTROLLED BY A CONTROL BOX. THE WINDSHIELD PANEL WENT OPAQUE ON AN IFR FLIGHT IN ICING CONDITIONS AND STAYED OPAQUE THROUGHOUT THE FLIGHT EVEN WHEN THE ICE HAD MELTED FROM THE REST OF THE WINDS
- [SDR 99ZZZX3610](https://openairdocs.org/sdr/99ZZZX3610.md): Gear · failed · Aug 1, 1999 · N4759K · Cessna P210N · Reciprocating Engine Power Section
  > TT: 1,443.0 HRS AIR FRAME AND ENGINE. ORIGINAL ENGINE FROM THE FACTORY, NEVER REMOVED. GEAR TOOTH FOUND DURING OIL DRAIN CHANGE, MTAL FOUND IN THE OIL FILTER. NO MOTOR OR PART FROM IN THE PREVIOUS OIL CHANGE 35 HRS PIOR. ENGINE WAS RUNNING NORMAL.
- [SDR 99ZZZX2791](https://openairdocs.org/sdr/99ZZZX2791.md): Clamp · failed · Jul 12, 1999 · N4753K · Cessna P210N · Exhaust Turbocharger
  > SHORTLY AFER NORMAL TAKEOFF ROLL AND ROTATION, PILOT NOTICED MANIFOLD PRESSURE REDUCTION TO ATMOSPHERIC. PILOT REMAINED IN THE AIRPORT PATTERN AND EXECUTED A NORMAL LANDING. INITIAL INSPECTION IDENTIFIED A BURNED LEFT FORWARD NOSE SKIN. UPON COWLING REMOVAL,
- [SDR 99ZZZX495](https://openairdocs.org/sdr/99ZZZX495.md): Bulkhead · cracked · Jan 12, 1999 · N4801P · Cessna P210N · Fuselage Main, Bulkhead
  > BULKHEAD ASSEMBLY AT STA 194.80 CRACKED/BROKEN LOWER RIGHT CORNER, THE AUTOPILOT KFC 200 PITCH SERVO AFT MOUNT, BOLTS 2 INCHES INBOARD OF CRACK.
- [SDR 99ZZZX27](https://openairdocs.org/sdr/99ZZZX27.md): Switch · failed · Dec 7, 1998 · N130RC · Cessna P210N · Electrical Power System
  > DURING PRE-FLIGHT, MAIN AVIONICS POWER SWITCH WAS FOUND INOPERATIVE. TROUBLESHOOTING REVEALED A LOOSE POSITION SWITCH. SWITCH WAS REPLACED. SUBMITTER STATED CAUSE COULD BE TENSION ON WIRING BUNDLE ATTACHED TO SWITCH.

Next page: https://openairdocs.org/model/cessna-p210n/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 = 'P210N'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-p210n/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.