# Service difficulty reports: Cessna 210D A list on [Cessna 210D](https://openairdocs.org/model/cessna-210d.md). Newest first. General aviation reporting is voluntary. - [SDR 2022FA0000458](https://openairdocs.org/sdr/2022FA0000458.md): Hydraulic Line · ruptured · Jul 30, 2022 · N375MK · Cessna 210D · Hydraulic System, Main > PILOT STATED THAT DURING CRUISE FLIGHT HE SUDDENLY FELT WARM LIQUID ON HIS ANKLE THAT WAS LATER IDENTIFIED AS HYDRAULIC FLUID. ATTEMPT WAS MADE TO LOWER THE GEAR WITHOUT SUCCESS. AIRCRAFT ENDED UP LANDING GEAR UP ON THE RUNWAY. INSPECTION OF GEAR SYSTEM AFTER - [SDR 2015FA0000236](https://openairdocs.org/sdr/2015FA0000236.md): Rib · cracked · May 5, 2015 · N210W · Cessna 210D · Aileron Tab Control System > BRACKET, PN 123139-1, ELEVATOR TRIM TAB JACK SCREW SUPPORT, SEPARATED FROM RIB AT BS 23.375 RT SIDE HORIZONTAL STABILIZER, CAUSING COMPLETE LOSS OF TRIM CONTROL AND PERIODIC JAMMING OF ELEVATOR AS JACKSCREW WAS CATCHING ON REAR SPAR OPENING. DAMAGE WAS LIMITE - [SDR 2012FA0000796](https://openairdocs.org/sdr/2012FA0000796.md): Saddle · broken · Dec 6, 2012 · N10RV · Cessna 210D · Main Landing Gear Strut/Axle/Truck > ON TAKEOFF, PILOT SELECTED TO RETRACT LANDING GEAR, BUT DID NOT GET A GEAR-UP CONFIRMATION LIGHT. PILOT OBSERVED BY MIRRORS THAT THE LT MLG WAS ONLY HALFWAY RETRACTED. PILOT CYCLED LANDING GEAR SELECTOR SEVERAL TIMES WITH MOVEMENT FROM NOSE AND RT LANDING GE - [SDR 2005FA0001012](https://openairdocs.org/sdr/2005FA0001012.md): Cylinder Head · cracked · Jun 17, 2005 · N210AW · Cessna 210D · Reciprocating Engine Cylinder Section > ENGINE WITH 450.0 TIS AND CYLINDER NR 2 WITH THE SAME TIS, BUT 31.0 HOURS SINCE REMOVAL/REPAIR/REINSTALLATION. DURING CRUISE FLIGHT, ENG BECAME VERY ROUGH WITH LOSS OF POWER. NORMAL LANDING WAS MADE. UPON INSP OF ENG, FOUND NR 2 CYL (COLD). PERFORMED COMPR - [SDR 2002FA0000437](https://openairdocs.org/sdr/2002FA0000437.md): Link · failed · Feb 7, 2002 · N3806Y · Cessna 210D · Nose/Tail Landing Gear > NOSE GEAR FAILED TO EXTEND FOR LANDING, DAMAGING ENGINE, PROPELLER, GEAR DOORS AND NOSE TIRE. AFTER JACKING AIRCRAFT IT WAS DISCOVERED THAT ROLLER ON MECHANICAL LINKAGE FOR NOSE GEAR DOORS HAD MOVED ON MECHANICAL LINKAGE FOR NOSE GEAR DOORS HAD MOVED FORWARD - [SDR 2002FA0000331](https://openairdocs.org/sdr/2002FA0000331.md): Nut · loose · Feb 7, 2002 · N375HW · Cessna 210D · Miscellaneous Hardware > THE ELT ANTENNA WAS FOUND TO BE LOOSE ON VISUAL INSPECTION. REMOVED ELT ANTENNA ASSEMBLY, FOR PROGRESSIVE INSPECTION. FOUND SHIELD LOCKING NUT SECURING METAL RADIATING ROD TO ANTENNA BASE ASSEMBLY WAS LOOSE. WHEN RADIATING ROD WAS REMOVED FROM ANTENNA BASE - [SDR 2001FA0000579](https://openairdocs.org/sdr/2001FA0000579.md): Skin · damaged · Nov 15, 2001 · N210KE · Cessna 210D · Horizontal Stabilizer, Plate/Skin > DURING AN ANNUAL INSPECTION THE RIGHT INBOARD SKIN HAD EXCESSIVE OIL CANNING WHEN FLEXED. WHEN FAIRING, PN 12124265 AND PN 12124266 (RIGHT AND LEFT) WERE REMOVED, THE RIGHT UPPER SKIN SURFACE UNDER FAIRING WAS CHAFFED THROUGH 4 INCHES IN LENGTH THE LEFT SKIN - [SDR 2001FA0000578](https://openairdocs.org/sdr/2001FA0000578.md): Skin · damaged · Nov 15, 2001 · N210KE · Cessna 210D · Horizontal Stabilizer, Plate/Skin > DURING AN ANNUAL INSPECTION THE RIGHT INBOARD SKIN HAD EXCESSIVE OIL CANNING WHEN FLEXED. WHEN FAIRING, PN 12124265 AND 12124266 (RIGHT AND LEFT) WERE REMOVED, THE RIGHT UPPER SKIN SURFACE UNDER FAIRING WAS CHAFFED THROUGH 4 INCHES IN LENGTH THE LEFT SKIN IN - [SDR 2001FA0000133](https://openairdocs.org/sdr/2001FA0000133.md): Shock Mount · broken · Apr 30, 2001 · N3738Y · Cessna 210D · Instrument Panel > AFTER FLYING THROUGH TURBULANCE THE PILOT COULD NOT LEVEL OFF ATER A DECENT DUE TO LIMITED ELVEATOR CONTROL. A NOSE FIRST LANDING WAS ACCOMPLISHED WITH THE AIRCRAFT/ENGINE RECEVING SUBSTANTIAL DAMAGE. INITIAL OBSERVATIONS REVEALED THE ELVEATORS ONLY GOING TO - [SDR 99ZZZX4475](https://openairdocs.org/sdr/99ZZZX4475.md): Cylinder · failed · Jul 8, 1999 · N446G · Cessna 210D · Reciprocating Engine Cylinder Section > CYLINDER HEAD SEPARATED DURING FLIGHT. ACFT MADE PRECAUTIONARY LANDING. POST-INCIDENT INSP REVEALED NR 3 CYL HEAD SEPARATED BETWEEN ITS COOLING FINS. HEAD CRACKED, SEPARATED AT THREADS THAT SECURE CYL HEAD TO BARREL. EVIDENCE OF A 3 INCH CRACK NEAR EXH POR - [SDR 20001205SH003](https://openairdocs.org/sdr/20001205SH003.md): Control Cable · broken · Apr 5, 1999 · N2340F · Cessna 210D · Mixture Control > AIRCRAFT LOST POWER AND COLLIDED WITH GROUND OBSTRUCTIONS FOLLOWING A FORCED LANDING OFF-FIELD. SUBSEQUENT INVESTIGATION REVEALED A BROKEN MIXTURE CABLE. AD-85-03-01 IS A ONE-TIME AD WHICH APPLIES TO THIS AIRCRAFT. THE AD INCORPORATED SE69-16. THE AIRCRAFT - [SDR 99ZZZX4013](https://openairdocs.org/sdr/99ZZZX4013.md): Control Cable · failed · Apr 5, 1999 · N2340F · Cessna 210D · Mixture Control > MIXTURE CABLE BROKE IN-FLIGHT CAUSING FORCED OFF-FIELD LANDING AND SUBSEQUENT INJURIES TO PILOT AND PASSENGER, AND DESTRUCTION OF THE AIRCRAFT. MIXTURE CABLE HAD BEEN REPLACED LESS THAN ONE YEAR PRIOR AND 99 FLIGHT HOURS HAD BEEN ACCUMULATED. THE CABLE SHOWE - [SDR 98ZZZX993](https://openairdocs.org/sdr/98ZZZX993.md): Ring · failed · Feb 21, 1998 · N3772Y · Cessna 210D · Empennage Structure > THE TAIL TIE-DOWN RING BROKE WHEN THE OWNER ATTEMPTED A MINOR RE-ALIGNMENT. REMOVAL OF THE FAILED PARTS REVEALED AN UNAPPROAVED PART HAD BEEN INSTALLED BY SOMEONE IN THE PAST. THIS RING BOLT CAN BE FOUND IN MOST ANY HARDWARE STORE. IT HAD BEEN WIRE FORMED O - [SDR 98ZZZX1023](https://openairdocs.org/sdr/98ZZZX1023.md): Roll Pin · failed · Jan 26, 1998 · N3929Y · Cessna 210D · Landing Gear Retraction/Extension System > ROLL PIN BACKED OUT OF GEAR CONTROL VALVE AT GEAR UP SELECTION, NO FURTHER GEAR SELECTION WAS POSSIBLE AT THIS TIME. CESSNA PARTS SHEET SHOWS AFFECTED PIN (ITEM NR 27). SUBMITTER RECOMMENDS GEAR POWER PACK SELECTOR ROLL PINS BE SAFETIED AND CHECKED EACH ANNU - [SDR 97ZZZX4476](https://openairdocs.org/sdr/97ZZZX4476.md): Skin · cracked · Oct 8, 1997 · N3785Y · Cessna 210D · Fuselage Main, Plate/Skin > TOP CABIN SKIN TORN (OIL CANNED) FROM AERODYNAMIC FORCES ACTING ON THE COMM 1 ANTENNA. THE ANTENNA WAS IMPROPERLY MOUNTED. IT WAS MOUNTED DIRECTLY TO THE CABIN SKIN WITHOUT THE USE OF A DOUBLER. SUBMITTER STATED TO PREVENT THIS OCCURRENCE FROM HAPPENING AGA - [SDR 97ZZZX440](https://openairdocs.org/sdr/97ZZZX440.md): Pump · failed · Dec 17, 1996 · N3908Y · Cessna 210D · Engine Fuel Pump > PILOT REPORTED THAT ENGINE WOULD NOT RUN BELOW 1500 RPM ON START DUE TO FUEL PUMP INTERNAL FAILURE. - [SDR 97ZZZX7](https://openairdocs.org/sdr/97ZZZX7.md): Saddle · cracked · Dec 16, 1996 · N3815Y · Cessna 210D · Main Landing Gear Strut/Axle/Truck > INSPECTION FOUND LANDING GEAR SADDLE CRACKED AT ACTUATOR ATTACH. - [SDR 96ZZZX5295](https://openairdocs.org/sdr/96ZZZX5295.md): Saddle Assy · broken · Oct 2, 1996 · N3815Y · Cessna 210D · Landing Gear Retraction/Extension System > LEFT LANDING GEAR WOULD NOT EXTEND OR RETRACT AFTER TAKEOFF. AN EMERGENCY LANDING WAS MADE WITH THE GEAR IN THE UP POSITION. MINOR DAMAGE TO BELLY OF AIRCRAFT AND BENT PROPELLER BLADES. FOUND BROKEN GEAR SADDLE THAT ATTACHES TO GEAR ACTUATOR. - [SDR EY2R9601615](https://openairdocs.org/sdr/EY2R9601615.md): Blade · damaged · Sep 1, 1996 · Cessna 210D · Propeller Blade Section > SCRATCH IN THREADS OF BLADE SN K84876YS - [SDR 95ZZZX1122](https://openairdocs.org/sdr/95ZZZX1122.md): Shaft · cracked · Feb 1, 1995 · N524BL · Cessna 210D · Landing Gear Steering System > NOSE GEAR STEERING SHAFT ASSY CRACKED 75 PERCENT AROUND AT HOLE FOR SHIMMEY DAMPENER ARM ROLL PIN. CRACK NOT VISIBLE UNTIL PART WAS COMPLETELY REMOVED. ONLY EVIDENCE OF PROBLEM WAS LOOSE ROLL PIN. SUBMITTER RECOMMENDS REGULAR INSPECTION OF ROLL PINS FOR LOO ## 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 = '210D' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/cessna-210d/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.