# Service difficulty reports: Cessna 210M

A list on [Cessna 210M](https://openairdocs.org/model/cessna-210m.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 94 reports

- [SDR 2014FA0000711](https://openairdocs.org/sdr/2014FA0000711.md): Line · leaking · Dec 16, 2014 · N761WU · Cessna 210M · Aircraft Fuel Distribution System
  > FUEL LINE, THAT GOES FROM THE FUEL SELECTOR TO THE FUEL BOOST PUMP WAS FOUND LEAKING PROFUSELY. HOSE LOOKED TO BE ORIGINAL EQUIPMENT.
- [SDR CCJA201306280001](https://openairdocs.org/sdr/CCJA201306280001.md): Gear · failed · Mar 12, 2013 · N6035N · Cessna 210M · Reciprocating Engine Power Section
  > DURING GROUND OPERATION, CAM SHAFT GEAR BROKE TWO TEETH. MOTOR AND DIRECTLY RELATED ACCESSORIES WERE REMOVED AND O/H. IT WAS UNDETERMINED BY THE O/H SHOP, THE CAUSE OF THE GEAR FAILURE.
- [SDR FPI2012F00008](https://openairdocs.org/sdr/FPI2012F00008.md): Cylinder Head · cracked · Jun 9, 2012 · N9489M · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING A 100 HR INSPECTION/ COMPRESSION TEST/ BUBBLE LEAK CHECK FOUND NR 2 CYCLE POSITION HEAD CRACKED INTO THE COMBUSTION CHAMBER - CYLINDER ASSY.
- [SDR FPI2012F00009](https://openairdocs.org/sdr/FPI2012F00009.md): Cylinder Head · cracked · May 9, 2012 · N9489M · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING A 100 HR INSPECTION/ COMPRESSION TEST/ BUBBLE LEAK CHECK, FOUND NR 4 CYLINDER POSITION HEAD CRACKED INTO THE COMBUSTION CHAMBER- REPLACED CYLINDER ASSY.
- [SDR FPI2012F00006](https://openairdocs.org/sdr/FPI2012F00006.md): Cylinder Head · cracked · May 3, 2012 · N9073M · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING A 100 HR INSPECTION, COMPRESSION TEST AND SOAP BUBBLE TEST FOR CRACKS FOUND THE NR 6 CYLINDER HEAD CRACKED INTO THE COMBUSTION CHAMBER LEAKING COMPRESSED AIR.
- [SDR FPI2011F00008](https://openairdocs.org/sdr/FPI2011F00008.md): Impulse Coupling · failed · Oct 13, 2011 · N8427M · Cessna 210M · Magneto/Distributor
  > DURING INVESTIGATIONOF REPORTED MAGNETO FAIL, REMOVED LT & RT MAGS AND FOUND LT MAGNETO IMPULSE COUPLING DRIVE PADS AND CAGE WERE BROKEN. DISASSEMBLED LT MAG AND FOUND ROTOR GEAR STRIPPED AND THE BREAKER END ROLLER BEARING HAD FAILED AND COME APART AND JAMED
- [SDR FPI2011F00009](https://openairdocs.org/sdr/FPI2011F00009.md): Cylinder · cracked · Oct 12, 2011 · N778VK · Cessna 210M · Reciprocating Engine Cylinder Section
  > CURING A 100 HR INSPECTION, FOUND NR1 CYLINDER CRACKED FROM FUEL NOZZLE TO SPARK PLUG PORT. REPLACED CYLINDER ASSY.
- [SDR 2011FA0000543](https://openairdocs.org/sdr/2011FA0000543.md): Alternator · failed · Aug 11, 2011 · N732VU · Cessna 210M · DC Generator-Alternator
  > ALTERNATOR COOLING FAN CAME APART IN FLIGHT AFTER TAKEOFF. PART OF COOLING FAN PUNCHED A HOLE IN INDUCTION AIR BOX DOWN STREAM OF AIR FILTER AND THE ALTERNATOR BELT CAME LOOSE IN THE ENGINE COMPARTMENT. LOSS OF ENGINE POWER FROM ENGINE FOD DAMAGE RESULTED IN
- [SDR FPI2011F00007](https://openairdocs.org/sdr/FPI2011F00007.md): Cylinder · cracked · Jul 20, 2011 · N9073M · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING A 100 HR INSPECTION, COMPRESSION TEST USING SOAPY WATER, BUBBLES CAME FROM CYLINDER HEAD COOLING FINS ABOVE EXHAUST PORT. NO VISUAL CRACKS NOTED.
- [SDR FPI2011F00006](https://openairdocs.org/sdr/FPI2011F00006.md): Cylinder · cracked · Jul 20, 2011 · N9073M · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING 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.
- [SDR FPI2011F00005](https://openairdocs.org/sdr/FPI2011F00005.md): Cylinder · cracked · Jul 20, 2011 · N9073M · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING 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.
- [SDR FPI2011F00000](https://openairdocs.org/sdr/FPI2011F00000.md): Gasket · failed · Apr 11, 2011 · N732YA · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING A SCHEDULED INSPECTION OF ENGINE, FOUND 5 OUT OF 5 INDUCTION GASKETS LEAKING. AFTER REMOVING INTAKE TUBES, OBSERVED THAT THE GASKETS WERE CRACKED AND TORN DURING INSTALLATION AT ASSEMBLY AT MFG AND WAS POSSIBILY CAUSE OF HIGH CHT READINGS.
- [SDR CA110208018](https://openairdocs.org/sdr/CA110208018.md): Torque Tube · corroded · Feb 4, 2011 · Cessna 210M · Rudder Control System
  > (CAN) DURING ANNUAL INSPECTION, PILOT`S LT RUDDER PEDAL ARM PART NUMBER FOUND LOOSE ON TORQUE TUBE. THE BOLT SECURING ARM TO TORQUE TUBE FOUND TO BE EXTREMELY CORRODED. INTERNAL INSPECTION OF MOUNTING ARM AND TORQUE TUBE STUB-END REVEALED SEVERE CORROSION IN
- [SDR 2010FA0001200](https://openairdocs.org/sdr/2010FA0001200.md): Camshaft · worn · Nov 17, 2010 · N994RA · Cessna 210M · Reciprocating Engine Power Section
  > METAL PARTICLES FOUND DURING OIL CHANGE. FURTHER INVESTIGATION FOUND CAMSHAFT LOBES WORN PAST LIMITS AND LIFTER BODIES MISSING SOME METAL. AD 2009-24-52 PREVIOUSLY COMPLIED WITH AND LIFTER 675915 HAD BEEN REPLACED PRIOR TP PRIOR "0" TIME O/H PERFORMED 468.2
- [SDR 2010FA0001157](https://openairdocs.org/sdr/2010FA0001157.md): Cylinder Head · cracked · Oct 21, 2010 · N6035N · Cessna 210M · Reciprocating Engine Cylinder Section
  > DURING AN ANNUAL/100HR INSP FOUND 4 OUT OF THE 6 CYLINDER HEADS CRACKED, THEY ARE ECI CYLINDERS WITH PN TIST71.4, SN'S 38519-08, 38542-17, 38947-18, 38947-30.
- [SDR 2010FA0001155](https://openairdocs.org/sdr/2010FA0001155.md): Nut · missing · Sep 20, 2010 · N5YBLG · Cessna 210M · DC Generator-Alternator
  > THIS ALTERNATOR, O/H WAS INSTALLED. TEST RUN-UP SHOWED NORMAL OPERATION. CHARGING SYS PROBLEMS WERE ENCOUNTERED AGAIN ON THE NEXT FLIGHT. UPON LANDING IT WAS DISCOVERED THAT THE HEX NUT ON THE ROTOR SHAFT WAS MISSING, INDICATING IMPROPER TORQUE AT UNIT O/H.
- [SDR 2010FA0001229](https://openairdocs.org/sdr/2010FA0001229.md): Attach Bracket · cracked · Sep 7, 2010 · N994RA · Cessna 210M · Horizontal Stabilizer, Attach Fittings
  > DURING ROUTINE ANNUAL INSP, THE RT FWD HORIZ STABILIZER ATTACH BRACKET WAS FOUND CRACKED. SB87-2 CALLS FOR KIT 210-118 TO BE INSTALLED. THE NEW FITTINGS PN 21320191 ARE BEEFED UP AND THE BULKHEAD IS ALSO. DUE TO THE CRITICAL NATURE OF THIS ATTACH FITTING, I
- [SDR 2010FA0000096](https://openairdocs.org/sdr/2010FA0000096.md): Torque Tube · cracked · Jan 11, 2010 · N732LW · Cessna 210M · Rudder Control System
  > UPON LANDING, PILOT LT RUDDER TORQUE TUBE CRACKED AT PEDDLE ATTACH POINT BELOW WELD. NO EVIDENCE OF FATIGUE OR STRESS CRACKS. NOTED CLEAN FRESH BREAK.
- [SDR FPI2008F00000](https://openairdocs.org/sdr/FPI2008F00000.md): Cable · broken · Aug 21, 2008 · N778VK · Cessna 210M · Standard Practices/Structures
  > MFG SERVICE KIT PN SK210174, CABLE ASSY BROKE AT THREADED END AFTER THE STOP NUT SEVEN WEEKS AFTER INSTALLATION APPEARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K)
- [SDR FPI2008F00001](https://openairdocs.org/sdr/FPI2008F00001.md): Cable · broken · Aug 14, 2008 · N8427M · Cessna 210M · Landing Gear Retraction/Extension System
  > MFG SERVICE KIT, PN SK210-174 CABLE ASSEMBLY BROKE AT THREADED END AFTER THE STOP NUT FIVE WEEKS AFTER INSTALLATION APPEARS THREAD WALL IS TOO THIN LEADING TO FATIGUE. (K)
- [SDR 2008FA0000349](https://openairdocs.org/sdr/2008FA0000349.md): Torque Link · cracked · May 2, 2008 · N70HG · Cessna 210M · Nose/Tail Landing Gear
  > OUR REPAIR STATION HAS REPLACED SEVERAL OF THESE SAME UPPER TORQUE LINKS DUE TO FINDING THEM BENT AT INSPECTION (APPROX 5 TOTAL) THIS IS THE FIRST ONE FOUND CRACKED. PROBABLE CASUE IS WHAT I BELIEVE IS LANDING IMPACT WITH MORE THAN RECOMMENDED STRUT ESTENSION
- [SDR 2006FA0000760](https://openairdocs.org/sdr/2006FA0000760.md): Snap Ring · failed · Aug 2, 2006 · N965B · Cessna 210M · Propeller Blade Section
  > 2 SNAP RINGS FAILED ON PROPELLAR BLADES. (K)
- [SDR N6265B](https://openairdocs.org/sdr/N6265B.md): Bulkhead · cracked · May 24, 2006 · N6265B · Cessna 210M · Fuselage Main, Bulkhead
  > WHILE UNDERGOING AN ANNUAL INSPECTION, FOUND THE FIREWALL TO BE CRACKED ON THE LT & RT SIDE WHERE THE P/N 1250255-7 EXHAUST HANGAR BRACKETS ATTACH. THE CRACKS WERE EXTENDING OUT FROM UNDER THE HANGAR BRACKETS AND EXTENDED IN MULTIPLE DIRECTIONS. ADDITIONAL INS
- [SDR 2006FA0000672](https://openairdocs.org/sdr/2006FA0000672.md): Diode · inoperative · Jan 4, 2006 · Cessna 210M · Landing Gear Position and Warning
  > DURING LANDING, FORGOT TO EXTEND THE LANDING GEAR AND GEAR UP LANDING WAS CARRIED OUT. ACCIDENT INVESTIGATION INCLUDED A SATISFACTORY OPS CHECK OF LANDING GEAR RETRACTION/EXTENSION SYSTEM, BUT WARNING HORN FAILED TO OPERATE. AFTER DISASSEMBLING THE WARNING U
- [SDR S3692](https://openairdocs.org/sdr/S3692.md): Wheel · separated · Aug 25, 2005 · N761K · Cessna 210M · Wheel/Ski/Float
  > TWO BOLTS IN RT MAIN WHEEL INNER FLANGE, BROKE ON LANDING, CAUSING WHEEL INNER FLANGE AND BRAKE DISC TO PARTIALLY SEPARATE FROM WHEEL HUB AND RUB INTO MAIN GEAR AXLE FITTING. MOUNTING BOLT HOLES IN BRAKE DISC SHOW SOME ELONGATION, POSSIBLY DUE TO LOOSE BOLTS
- [SDR 2005FA0000969](https://openairdocs.org/sdr/2005FA0000969.md): Impulse Coupling · worn · Jun 28, 2005 · N6175N · Cessna 210M · Magneto/Distributor
  > MAGS REMOVED FOR TROUBLESHOOTING OF ENGINE HIGH ALTITUDE OPERATION PROBLEM. DURING PREINSTALLATION INSPECTION OF COUPLINGS. ONE WAS FOUND WORN BEYOND LIMITS. (K)
- [SDR CCJ2005F00000](https://openairdocs.org/sdr/CCJ2005F00000.md): Bracket · broken · Apr 13, 2005 · N6035N · Cessna 210M · Main Landing Gear
  > THERE WAS NO (GEAR DOWN) INDICATION WHEN THE LANDING GEAR WAS EXTENDED. PILOT DECLARED EMERGENCY AND DIVERTED TO AN AIRPORT WITH A LONGER RUNWAY. LANDING WAS NORMAL AND UNEVENTFUL. UPON EXAMINATION IT WAS FOUND THAT THE BRACKET HOLDING THE NOSE GEAR (DOWN)
- [SDR AUS20040361](https://openairdocs.org/sdr/AUS20040361.md): Hose · loose · May 1, 2004 · Cessna 210M · Engine Fuel Distribution
  > (AUS) ENGINE FUEL HOSE LEAKING AT CONNECTION TO CHECK VALVE. FUEL LEAKING INTO ENGINE BAY. HOSE HAD NOT BEEN TIGHTENED DURING MAINTENANCE. PERSONNEL/MAINTENANCE ERROR.
- [SDR 2004FA0000316](https://openairdocs.org/sdr/2004FA0000316.md): Wire · shorted · Apr 8, 2004 · N761SP · Cessna 210M · DC Generator-Alternator
  > THE 3 WIRES COMING FROM THE STATOR ARE SHORTED OUT ON THE CASE. THIS IS 4TH ALTERNATOR OVERHAUL BY FACILITY WITH THE SAME FAILURE, ALL 4 ALTERNATORS HAD LESS THAN 390 HOURS SINCE OVERHAUL. THERE NEED TO BE MORE INSULATION ON THE 3 WIRES.
- [SDR AUS20040077](https://openairdocs.org/sdr/AUS20040077.md): Wire Harness · burned · Feb 5, 2004 · Cessna 210M · Electrical Power System Wiring
  > (AUS) WIRING LOOM CHAFED AND BURNED BY ELEVATOR COUNTERWEIGHT.
- [SDR 2004FA0000202](https://openairdocs.org/sdr/2004FA0000202.md): Wire · broken · Feb 3, 2004 · N732PY · Cessna 210M · Electrical Power System Wiring
  > AIRCRAFT LANDED WITH NO ELECTRICAL POWER. REPAIRED DAMAGED ALTERNATOR PRIMARY WIRE AND RESOLDERED CAPACITOR WIRE. TOP CHARGED BATTERY. OPS CHECKED GOOD IAW MFG C210 AMM AND AC43-1B/2A CHAPTER 11-7.
- [SDR AUS20040062](https://openairdocs.org/sdr/AUS20040062.md): Hose · failed · Jan 16, 2004 · Cessna 210M · Hydraulic System, Main
  > (AUS) NOSE LANDING GEAR DOOR ACTUATOR HOSE FAILED. LOSS OF HYDRAULIC FLUID.
- [SDR 2004FA0000319](https://openairdocs.org/sdr/2004FA0000319.md): Fuel Line · corroded · Dec 4, 2003 · N761AN · Cessna 210M · Aircraft Fuel Distribution System
  > FRONT FUEL LINE FROM LT WING TANK WAS IN CONTACT WITH FRESH AIR DUCT IN THE WING, AERO DUCT PN CEET 1.5 INCH. THIS CAUSED CORROSION ON THE ALUMINUM FUEL LINE. PROBLEM WAS FOUND WHEN FUEL STARTED LEAKING OUT OF THE WING. REPLACED FUEL LINE AND FRESH AIR DUCT
- [SDR XVQ2003F00000](https://openairdocs.org/sdr/XVQ2003F00000.md): Bearing · failed · Nov 20, 2003 · N823AR · Cessna 210M · Nose/Tail Landing Gear Strut/Axle
  > AIRCRAFT WAS FORCED TO MAKE A GEAR UP LANDING, DAMAGING PROP AND ENGINE. THE CAUSE WAS FOUND TO BE THE FAILURE OF A BEARING/WHEEL ASSEMBLY THAT ACTUATES THE NOSE GEAR DOORS CLOSING MECHANISM. THE BEARING FAILED ALLOWING THE WHEEL PORTION TO SHIFT OUTBOARD EX
- [SDR AUS20031032](https://openairdocs.org/sdr/AUS20031032.md): Hub · cracked · Sep 15, 2003 · Cessna 210M · Propeller Hub Section
  > (AUS) PROPELLER HUB CRACKED IN AREA OF FOURTH THREAD AT THE 2 O'CLOCK POSITION. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).
- [SDR CXU2003F00000](https://openairdocs.org/sdr/CXU2003F00000.md): Accumulator · failed · Mar 27, 2003 · N965B · Cessna 210M · Landing Gear Door Retract Section
  > END PLUG IN HYDRAULIC ACCUULATOR DEPARTED RELEASING HYDRAULIC FLUID AND PRESSURE. AIRCRAFT TACH READS 3679.2.
- [SDR AUS20030262](https://openairdocs.org/sdr/AUS20030262.md): Downlock Switch · sticking · Feb 24, 2003 · Cessna 210M · Landing Gear Position and Warning
  > (AUS) RT MAIN LANDING GEAR DOWNLOCK SWITCH STUCK. RT LANDING GEAR COLLAPSED ON LANDING.
- [SDR AUS20030009](https://openairdocs.org/sdr/AUS20030009.md): Tube · corroded · Jan 3, 2003 · Cessna 210M · Landing Gear Retraction/Extension System
  > (AUS) LANDING GEAR ACCUMULATOR LINE CONTAINED A SMALL CORROSION PINHOLE. LOSS OF HYDRAULIC FLUID.
- [SDR FPI2003F00000](https://openairdocs.org/sdr/FPI2003F00000.md): Line · chafed · Dec 16, 2002 · N7660E · Cessna 210M · Hydraulic System, Main
  > LANDING GEAR DOWN LINE CHAFED THRU BY AILERON RUDDER INTERCONNECT CABLE. WHEN SELECTING DOWN, ALL FLUID WAS PUMPED OUT OF SYSTEM. NOSE GEAR CAME DOWN AND LOCKED, MAIN GEAR DID NOT.
- [SDR AUS20021162](https://openairdocs.org/sdr/AUS20021162.md): Switch · faulty · Oct 15, 2002 · Cessna 210M · Landing Gear Position and Warning
  > (AUS) LT MAIN LANDING GEAR DOWN SWITCH INTERMITTENT IN OPERATION.
- [SDR AUS20020340](https://openairdocs.org/sdr/AUS20020340.md): Bracket · cracked · Mar 29, 2002 · Cessna 210M · Fuselage, Stabilizer Attach Fittings
  > (AUS) LH REAR HORIZONTAL STABILISER ATTACHMENT BRACKET CRACKED.
- [SDR AUS20020345](https://openairdocs.org/sdr/AUS20020345.md): Fitting · faulty · Mar 3, 2002 · Cessna 210M · Wing, Fuselage Attach Fittings
  > (AUS) LH WING ATTACHMENT FITTING CONTAINED A SUBSURFACE DEFECT IN THE AREA ADJACENT TO BUT NOT INTO THE MAIN WING ATTACHMENT BOLT HOLE. FOUND DURING EDDY CURRENT INSPECTION.
- [SDR 20000808SH015](https://openairdocs.org/sdr/20000808SH015.md): Mount · missing · Jul 27, 2000 · N7660E · Cessna 210M · Engine Mount Section
  > PART MANUFACTURED DEFECT. MISSING REINFORCEMENT WASHER ON UPPER HALF. (X)
- [SDR 20000626SH011](https://openairdocs.org/sdr/20000626SH011.md): Alternator · loose · Jun 26, 2000 · N761PS · Cessna 210M · Alternator-Generator Drive
  > FOUND GROUND STUD TO BE LOOSE ON BACK OF ALTERNATOR. (X)
- [SDR AU000024](https://openairdocs.org/sdr/AU000024.md): Contactor · faulty · Jan 14, 2000 · Cessna 210M · Magneto/Distributor
  > (AUS) MAGNETO CONTACT SET FAULTY.
- [SDR 99ZZZX4139](https://openairdocs.org/sdr/99ZZZX4139.md): Spark Plug · mismanufactured · Sep 30, 1999 · N761PS · Cessna 210M · Spark Plug/Igniter
  > UPON INSPECTION OF PLUGS, FOUND PLUGS, 4 EACH, TO TEST WEAK AND NOT APPROPRIATE FOR INSTALLATION ON AIRCRAFT. NOTE: BY DOM AIR CARRIERS, ONE OF THE FOUR SPARK PLUGS HAD A RED DISCOLORATION AT BASE OF ELECTRODE AND CERAMIC. LOT NR 4G99.
- [SDR 99ZZZX4138](https://openairdocs.org/sdr/99ZZZX4138.md): Spark Plug · mismanufactured · Sep 29, 1999 · N9163M · Cessna 210M · Spark Plug/Igniter
  > INSTALLED NEW PLUGS IN ENGINE. PERFORMED RUN-UP. OPS OK. FOUR HOURS LATER, ENGINE HAD A 600 RPM DROP. REMOVED SPARK PLUGS, FOUND A PIECE OF WIRE AROUND CENTER ELECTRODE OF 3 PLUGS AND 4 OTHER PLUGS NOT FIRING VERY HOT ON PLUG TESTER. OPENED ANOTHER SET OF
- [SDR 99ZZZX4137](https://openairdocs.org/sdr/99ZZZX4137.md): Spark Plug · mismanufactured · Sep 29, 1999 · N9163M · Cessna 210M · Spark Plug/Igniter
  > SPARK PLUGS WERE REPLACED BECAUSE OF WEAR. UPON INSPECTION OF NEW PLUGS, FOUND WIRE WRAPPED AROUND CENTER ELECTRODE ON TWO OF THE NEW PLUGS (WHICH GROUNDED IT OUT) AND ANOTHER SIX WOULD NOT TEST GOOD IAW CHAMPION TEST PROCEDURES. OBTAINED ANOTHER NEW SET OF
- [SDR AU990682](https://openairdocs.org/sdr/AU990682.md): Bearing · failed · Jun 16, 1999 · Cessna 210M · Reciprocating Engine Power Section
  > (AUS) CRANKSHAFT BEARING FAILED. THE BEARING FELL OUT OF THE SUMP PLUG HOLE DURING ENGINE OIL DRAIN. LIMITED INFORMATION PROVIDED.
- [SDR 99ZZZX2724](https://openairdocs.org/sdr/99ZZZX2724.md): Bracket · cracked · Jun 1, 1999 · N1781M · Cessna 210M · Rudder, Spar/Rib
  > THE BRACKET IS THE RUDDER BOTTOM ATTACH POINT. INTERGRANULAR CORROSION EXTENDING THROUGH THE RIVETS AND SPLITTING THE SEAM. PICTURES PROVIDED.

Next page: https://openairdocs.org/model/cessna-210m/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 = '210M'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/cessna-210m/reports

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