Cessna 210D

Service difficulty reports · 20

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 = '210D'
  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 2022FA0000458Hydraulic Line · rupturedPILOT 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 Jul 30, 2022 · N375MK · Cessna 210D · Hydraulic System, MainSDR 2015FA0000236Rib · crackedBRACKET, 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 LIMITEMay 5, 2015 · N210W · Cessna 210D · Aileron Tab Control SystemSDR 2012FA0000796Saddle · brokenON 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 GEDec 6, 2012 · N10RV · Cessna 210D · Main Landing Gear Strut/Axle/TruckSDR 2005FA0001012Cylinder Head · crackedENGINE 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 COMPRJun 17, 2005 · N210AW · Cessna 210D · Reciprocating Engine Cylinder SectionSDR 2002FA0000437Link · failedNOSE 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 Feb 7, 2002 · N3806Y · Cessna 210D · Nose/Tail Landing GearSDR 2002FA0000331Nut · looseTHE 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 BASEFeb 7, 2002 · N375HW · Cessna 210D · Miscellaneous HardwareSDR 2001FA0000579Skin · damagedDURING 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 Nov 15, 2001 · N210KE · Cessna 210D · Horizontal Stabilizer, Plate/SkinSDR 2001FA0000578Skin · damagedDURING 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 Nov 15, 2001 · N210KE · Cessna 210D · Horizontal Stabilizer, Plate/SkinSDR 2001FA0000133Shock Mount · brokenAFTER 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 TOApr 30, 2001 · N3738Y · Cessna 210D · Instrument PanelSDR 99ZZZX4475Cylinder · failedCYLINDER 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 PORJul 8, 1999 · N446G · Cessna 210D · Reciprocating Engine Cylinder SectionSDR 20001205SH003Control Cable · brokenAIRCRAFT 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 AIRCRAFTApr 5, 1999 · N2340F · Cessna 210D · Mixture ControlSDR 99ZZZX4013Control Cable · failedMIXTURE 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 SHOWEApr 5, 1999 · N2340F · Cessna 210D · Mixture ControlSDR 98ZZZX993Ring · failedTHE 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 OFeb 21, 1998 · N3772Y · Cessna 210D · Empennage StructureSDR 98ZZZX1023Roll Pin · failedROLL 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 ANNUJan 26, 1998 · N3929Y · Cessna 210D · Landing Gear Retraction/Extension SystemSDR 97ZZZX4476Skin · crackedTOP 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 AGAOct 8, 1997 · N3785Y · Cessna 210D · Fuselage Main, Plate/SkinSDR 97ZZZX440Pump · failedPILOT REPORTED THAT ENGINE WOULD NOT RUN BELOW 1500 RPM ON START DUE TO FUEL PUMP INTERNAL FAILURE.Dec 17, 1996 · N3908Y · Cessna 210D · Engine Fuel PumpSDR 97ZZZX7Saddle · crackedINSPECTION FOUND LANDING GEAR SADDLE CRACKED AT ACTUATOR ATTACH.Dec 16, 1996 · N3815Y · Cessna 210D · Main Landing Gear Strut/Axle/TruckSDR 96ZZZX5295Saddle Assy · brokenLEFT 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.Oct 2, 1996 · N3815Y · Cessna 210D · Landing Gear Retraction/Extension SystemSDR EY2R9601615Blade · damagedSCRATCH IN THREADS OF BLADE SN K84876YSSep 1, 1996 · Cessna 210D · Propeller Blade SectionSDR 95ZZZX1122Shaft · crackedNOSE 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 LOOFeb 1, 1995 · N524BL · Cessna 210D · Landing Gear Steering System
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