Cessna T210M

Service difficulty reports · 110

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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 = 'T210M'
  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 AUS20010557Transponder · faulty(AUS) TRANSPONDER GIVING FALSE ALTITUDE READINGS.May 18, 2001 · Cessna T210M · ATC Transponder SystemSDR 20010430CW004Engine · lack of lubeOWNER DISCOVERED A GREAT LOSS OF ENGINE OIL, FOLLOWING A COLD WEATHER FLIGHT. TEMPERATURE WAS 40 DEGREES C/F. AIR/OIL SEPARATOR INSTALLED PRIOR TO RECENT CYLINDER REPLACEMENT.Apr 30, 2001 · N732UH · Cessna T210M · Reciprocating Engine Oil SystemSDR CA010131018Rib · cracked(CAN) DURING A 50 HOUR INSPECTION OF THE HORIZONTAL STAB, THE 4 RIBS WERE FOUND TO BE LOOSE & CRACKED. THIS IS DONE BY SQUEEZING THE NOSE RIBS (WITH A MODERATE AMOUNT OF PRESSURE) AND LISTEN FOR CLICKING SOUNDS & FEELING OF LOOSE RIVETS. THEREFORE, THE LOWER SJan 10, 2001 · Cessna T210M · Horizontal Stabilizer, Spar/RibSDR 20010302AP001Bulkhead · crackedFOUND RIGHT WING INBOARD FLAP BELLCRANK BULKHEAD STA.54.75 CRACKED. CRACK WAS LOCATED LEFT LOWER CORNER OF BULKHEAD (LOOKING FWD) AND APPROX. 1.5 INCHES LONG. AIRCRAFT HAS ROBERTSON STOL KIT INSTALLED. SUSPECT HIGHER CABLE TENSIONS BECAUSE OF STOL KIT CONTRIBJan 3, 2001 · Cessna T210M · Wing, Rib/BulkheadSDR 20000516SH015Stud · brokenBOTH FORWARD AND AFT STUDS BROKEN HALF WAY OUT THROUGH .4375 INCH - 20 INCH THREADS. (X)Apr 27, 2000 · N730P · Cessna T210M · Reciprocating Engine Power SectionSDR 99ZZZX3853Alternator · failedDURING VFR FLIGHT, ALTERNATOR FAILED AFTER LANDING GEAR RETRACTION. ALTERNATOR FAILED 5 MINUTES AFTER LANDING GEAR RETRACTION DURING CLIMB TO ALTITUDE. AMMETER AND VOLTMETER INDICATIONS PRIOR TO FAILURE WERE NORMAL. ALTERNATOR DID NOT COME ON-LINE AFTER COMSep 9, 1999 · N888Q · Cessna T210M · DC Generator-AlternatorSDR 99ZZZX2954Hose · separatedHOSE CLOSE TO GEAR DOOR DOUBLE-ACTING HYDRAULIC ACTUATOR SEPARATED AT SOCKET DURING LANDING GEAR LOWERING CYCLE. HOSE WAS FIVE YEARS OLD.Jul 24, 1999 · N732YK · Cessna T210M · Landing Gear Door ActuatorSDR 99ZZZX1885Lifter · spalledDURING 100-HOUR INSPECTION, FOUR CYLINDERS SHOWED LOW COMPRESSION. UPON REMOVAL OF CYLINDERS, NOTED THE NR 5 CYLINDER EXHAUST CAM FOLLOWER WAS SPALLED BAD. INSPECTION OF CAM LOBE DID NOT APPEAR NEARLY AS BAD AS CAM FOLLOWER. CAMSHAFT AND CAM FOLLOWERS WERE Apr 5, 1999 · N761VH · Cessna T210M · Reciprocating Engine Power SectionSDR 99ZZZX1443Support · looseDURING ANNUAL INSPECTION, ALL 4 NAS565-33 BOLTS LT AND RT SIDE WERE FOUND LOOSE ALLOWING THE MLR SADDLE AND SHIMS TO MOVE.Mar 12, 1999 · N761KC · Cessna T210M · Landing Gear Retraction/Extension SystemSDR 99ZZZX575Spar · crackedDURING AN ANNUAL INSPECTION A CRACK APPROXIMATELY 1 INCH LONG WAS DETECTED ON THE LEFT HORIZONTAL STABILIZER AFT SPAR LOWER RADIUS.Jan 18, 1999 · N7067Z · Cessna T210M · Horizontal Stabilizer, Spar/RibSDR 98ZZZX4791Lifter · failedSPALLED LIFTER WAS FOUND AFTER NR 1 CYLINDER WAS REMOVED DUE TO LOW COMPRESSION. SUSPECT MANUFACTURING DEFECT OR OIL FILM FAILURE. ENGINE WAS USING AEROSHELL 15W-50.Dec 8, 1998 · N761AS · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 99ZZZX2382Accumulator · failedAFTER LANDING, GEAR WAS CYCLED DOWN AND RIGHT AFTER A GREEN LIGHT CAME ON, A LOUD BANG WAS HEARD FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. A SAFE LANDING WAS MADE. DISCOVERED THE MLG DOOR ACCUMULATOR HAD FAILED AT THE SNAP RING. A HOLE WAS PUT IN THE RIGHT SKNov 21, 1998 · N761KC · Cessna T210M · Landing Gear Door Retract SectionSDR CA981006011Blade · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. INSPECTION FOUND ALL THREE BLADES HAD BEEN FIELD MODIFIED BELOW MINIMUM WIDTH.Aug 28, 1998 · Cessna T210M · Propeller Blade SectionSDR 98ZZZX3317Ducting · deterioratedIN THE FLOOR OF THE AIRCRAFT, A FRESH AIR DUCT WAS TOUCHING A BRAKE LINE. IT CAUSED DISSIMILAR METAL CORROSION TO FORM ON THE BRAKE LINE WHICH THEN LEAKED.Aug 20, 1998 · N732VH · Cessna T210M · Air Distribution SystemSDR 98ZZZX2809Battery Box · corrodedDURING ANNUAL INSPECTION, RIVETS IN BOTTOM OF BOX WERE FOUND CORRODED AND MISSING UNDER PLASTIC LINER ALLOWING ACID INTO COCKPIT. MORE FREQUENT INSPECTION RECOMMENDED.Jul 29, 1998 · N761VZ · Cessna T210M · Battery Box StructureSDR 98ZZZX3068Alternator · failedALTERNATOR FAILED OUT OF THE SHIPPING BOX. (ELECTROSYSTEMS OVH UNIT).Jul 20, 1998 · N7398M · Cessna T210M · DC Generator-AlternatorSDR 98ZZZX2359Plunger · wornFUEL STRAINER DRAIN PLUNGER NIPPLE LEAKING FASTER THAN BEFORE. SUBMITTER SUGGESTED CHANGING FUEL OR RUBBER ON PLUNGER.Jun 19, 1998 · N6977B · Cessna T210M · Aircraft Fuel Filter/StrainerSDR 98ZZZX889Turbocharger · failedONE BENT BLADE AND ONE BLADE SEPARATED AT HALF ITS LENGTH. PART FAILED ON FINAL APPROACH TO LANDING. COMPRESSOR SHAFT AND TURBINE SHAFT BENT. NO KNOWN REASON FOR COMPRESSOR BLADE TO HAVE SEPARATED, OR FOR SHAFT TO HAVE BENT, NO EVIDENCE OF FOREIGN OBJECTS BFeb 12, 1998 · N6687B · Cessna T210M · Exhaust TurbochargerSDR AU980392Structure · misinstalled(AUS) HORIZONTAL STABILIZER SPAR CAP CRACKED IN AREA OF THE LOWER REAR MOUNT BOLT HOLES. CRACK LENGTHS 12.7MM (0.5 INCH). INVESTIGATION FOUND NEW PN 1232624-1 REINFORCEMENTS (SE 84-17) HAD BEEN FITTED IN AMERICA (29JUL84), BUT HAD BEEN INSTALLED UPSIDE DOWN Feb 1, 1998 · Cessna T210M · Horizontal Stabilizer, Spar/RibSDR 98ZZZX318Rib · crackedDURING ANNUAL INSPECTION, A CLICKING NOISE WAS HEARD WHILE PRESSING THE LEADING EDGE OF THE HORIZONTAL STABILIZER AT THE RIBS. WITH FURTHER INSPECTION, SEVERAL RIBS FOUND CRACKED ON BOTH LT AND RT SIDES OF THE STABILIZER. ALSO, FOUND ON THIS ACFT, RIB PN 123Jan 7, 1998 · N732XE · Cessna T210M · Horizontal Stabilizer, Plate/SkinSDR 99ZZZX113Line · chafedPILOT REPORTED ERRATIC FUEL FLOW INDICATION. DURING GROUND ENG RUN-UP FOR T/S, A LOUD POP WAS HEARD, LARGE SPARK SHOT FROM BEHIND COPILOT'S INSTRUMENT PANEL, AND THE 3-AMP STEREO CB OPENED. INVEST REVEALED THE 28-VOLT POWER LEAD FOR THE STEREO (INSTALLED SEVNov 18, 1997 · N761VE · Cessna T210M · Aircraft Fuel Distribution SystemSDR 97ZZZX4763Turbocharger · looseAT ANNUAL INSPECTION, NOTED THE CENTER SECTION WAS LOOSE AT THE BOLTS THAT HOLD THE CENTER SECTION TO THE HOT SIDE OF THIS UNIT. THIS HAS BEEN LEAKING AS THERE WAS EVIDENCE OF EXHAUST IN THIS AREA. IT IS ASSUMED THESE BOLTS WERE LEFT LOOSE DURING INSTALLATIOOct 16, 1997 · N761KC · Cessna T210M · Exhaust TurbochargerSDR 97ZZZX4049Bracket · cracked100 HOUR INSPECTION FOUND A BROKEN SCREW P/N AN 509-416R13 IN THE HORIZONTAL STABILIZER MOUNT AND MOUNT BRACKET P/N 1212128-1 CRACKED IN THREE PLACES.Aug 18, 1997 · N6241B · Cessna T210M · Horizontal Stabilizer, Attach FittingsSDR 97ZZZX4048Screw · broken100 HOUR INSPECTION FOUND A BROKEN SCREW P/N AN 509-416R13 IN THE HORIZONTAL STABILIZER MOUNT AND MOUNT BRACKET P/N 1212128-1 CRACKED IN THREE PLACES.Aug 18, 1997 · N6241B · Cessna T210M · Horizontal Stabilizer, Attach FittingsSDR 97ZZZX3334Piston · erodedSHORTLY AFTER TAKEOFF, PILOT LOST ENGINE POWER AND CRASH LANDED SHORT OF RUNWAY. POST-ACCIDENT INVESTIGATION REVEALED CYL NR 1 SHOWED SIGNS OF EXCESSIVE HEAT. UPON REMOVAL OF CYL ASSY, THE PISTON WAS FOUND SEVERELY ERODED AROUND MUCH OF THE UPPER PERIMETER. Jul 2, 1997 · N761FM · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 97ZZZX2919Pin · shearedSEE FIGURE 126A OF PART MANUAL 1970 TO 1980 CESSNA 210. PIN PN 1280209-1 IS PRESSED INTO BEARING END PN 1280600-5 AND LOCKED IN PLACE WITH A ROLL PIN. THIS PIN IS USED FOR NOSE GEAR DOWNLOCK. PINS WERE BEING REPLACED AS PART OF REPAIR TO REMOVE PLAY IN NLG.Apr 23, 1997 · N6798M · Cessna T210M · Landing Gear Retraction/Extension SystemSDR 97ZZZX1869Bolt · failedBOLT ATTACHING ALTERNATOR ADJUSTING BRACKET TO ENGINE FAILED. THIS ALLOWED THE ALTERNATOR TO MOVE UNTIL ELECTRICAL TERMINAL CONTACTED A GROUND CAUSING A DIRECT SHORT. THE BOLT WAS A NON-STANDARD BOLT OF UNKNOWN ORIGIN. UNAPPROVED PART.Apr 4, 1997 · N6687B · Cessna T210M · Alternator-Generator DriveSDR 97ZZZX975Valve · wornDURING 100 HOUR INSPECTION, FOUND NR 1 CYLINDER READING 20/80 DURING COMPRESSION CHECK, ALSO, ALL OTHER CYLINDERS IN LOW SIXTIES. TOTAL TIME 824.8 HOURS SINCE TCM. ZERO TIME REBUILD.Feb 20, 1997 · N6457B · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 96ZZZX6008Connect Rod · failedENGINE OPERATED 233 HOURS OVER MFG RECOMMENDED OVERHAUL TIME OF 1400 HRS. REF SB NR M91-8, 10JULY91. CONNECTING ROD FAILED IN NORMAL CRUISE AT 8,000 FEET ALTITUDE. ENGINE HAD A 100 HR INSPECTION WITHIN PREVIOUS 25 HRS OF OPERATION. COMPRESSION REPORTED 72/Nov 11, 1996 · N732LR · Cessna T210M · Reciprocating Engine Power SectionSDR EY2R9601219Bearing · corrodedRETAIN BEARING CORRODED.Nov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601218Cylinder · corrodedCYLINDER CORRODED.Nov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601217Piston · corrodedPISTON CORRODED.Nov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601216Retainer · corrodedCORROSION FOUND ON SPLIT RETAINER.Nov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601215Actuator Pin · corrodedACT PIN ASSEMBLY FOUND CORRODED.Nov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601214Piston Link Pin · corrodedCORROSION FOUND ON PISTON LINK PIN.Nov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601213Propeller · corrodedPROPELLER ASSY IS CORRODEDNov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601212Spring · corrodedCORROSION FOUND ON PITCH RETURN SPRINGNov 1, 1996 · Cessna T210M · Propeller AssemblySDR EY2R9601211Blade · corrodedBLADE, SN 125242, FOUND CORRODED.Nov 1, 1996 · Cessna T210M · Propeller Blade SectionSDR EY2R9601210Blade · corrodedBLADE, SN 125221, FOUND CORRODED.Nov 1, 1996 · Cessna T210M · Propeller Blade SectionSDR EY2R9601209Blade · corrodedBLADE, SN 124558, FOUND CORRODED.Nov 1, 1996 · Cessna T210M · Propeller Blade SectionSDR 96ZZZX5492Alternator · failedFAILURE DURING IFR CONDITIONS. OPS CHECK AFTER LANDING SHOWED NORMAL VOLTAGE AND CHARGING RATE. SECOND FAILURE IN IFR AND A/C LANDED. OPS CHECK SHOWED ERRATIC VOLTAGE AND HIGH CHARGE RATE. A/C FERRIED IFR TO REPAIR FACILITY 10 MINUTES AWAY WITH ALT ON LINEOct 17, 1996 · N6161N · Cessna T210M · DC Generator-AlternatorSDR 96ZZZX4735Regulator · failedREGULATOR FIELD LINE WENT TO FULL VOLTAGE CONDITION CAUSING OVERVOLTAGE PROTECTION TO DISABLE SYSTEM. REPLACED VOLTAGE REGULATOR TO SOLVE PROBLEM.Aug 31, 1996 · N732TG · Cessna T210M · DC RegulatorSDR 96ZZZX4958Crankshaft · flange failedPROPELLER AND CRANKSHAFT PROPELLER FLANGE SEPARATED FROM ENGINE.Jul 5, 1996 · N7398M · Cessna T210M · Reciprocating Engine Power SectionSDR 96ZZZX3446Line · brokenON APPROACH TO LAND, PILOT HAD A LANDING GEAR UNSAFE LIGHT INDICATION. PILOT NOTED THERE WAS NO GREEN LIGHT ILLUMINATED TO INDICATE THE LANDING GEAR WAS IN SAFE DOWN AND LOCK CONDITION. ALSO, AN INTERMITTENT FLICKERING LIGHT FOR THE LANDING GEAR 'UP' POSITIOJun 4, 1996 · N7398M · Cessna T210M · Landing Gear Retraction/Extension SystemSDR 96ZZZX3327Line · rupturedHYDRAULIC LINE FAILED IN SERVICE CAUSING HYDRAULIC FLUID LEAK. LANDING GEAR COULD NOT BE HAND PUMPED DOWN. SUBMITTER RECOMMENDS CLOSE INSPECTION OF ALL HYDRAULIC LINES DURING ROUTINE INSPECTIONS.Jun 3, 1996 · N7398M · Cessna T210M · Hydraulic System, MainSDR 96ZZZX3213Line · rupturedSUBJECT HYDRAULIC LINE FAILED IN SERVICE CAUSING HYDRAULIC FLUID LEAK. LANDING GEAR COULD NOT BE HAND PUMPED DOWN. SUBMITTER RECOMMENDS CLOSE INSPECTION OF ALL HYDRAULIC LINES DURING ROUTINE INSPECTIONS.Jun 3, 1996 · N7398M · Cessna T210M · Hydraulic System, MainSDR 96ZZZX2412Engine · defectivePRE-PURCHASE INSPECTION OF AIRCRAFT REVEALED ENGINE COMPRESSION WELL BELOW ACCEPTABLE LIMITS, SEAT RAILS WERE WORN BEYOND LIMITS. ESTABLISHED BY AIRWORTHINESS DIRECTIVE. ELEVATOR TRIM TAB WITH HOLES CORRODED THROUGH THE TAB SKIN. AIRCRAFT WAS ANNUALLED THE Mar 20, 1996 · N761TF · Cessna T210M · Reciprocating Engine Cylinder SectionSDR 96ZZZX1047Hose · chafedWASTEGATE OIL RETURN HOSE CHAFED THROUGH AT FORWARD RIGHT ENGINE MOUNT. SUBMITTER STATES CORRECTIVE ACTION - CLAMP HOSE OFF FOR PROPER CLEARANCE.Feb 23, 1996 · N666SW · Cessna T210M · Reciprocating Engine Oil SystemSDR 96ZZZX1268Cable Assy · bound yokeUPON PREPARATION FOR TAKEOFF, PILOT CHECKED CONTROLS AND YOKE LOCKED UP ON NEAR TO A FULL FORWARD POSITION. ROLL WAS OK. UPON INSPECTION, YOKE ELECTRICAL RIBBON ASSY FOUND BOUND IN 2 OF THE 4 YOKE TUBE ROLLERS. PHYSICAL FORCE COULD NOT DISLODGE. ROLLERS REFeb 12, 1996 · N6276B · Cessna T210M · Control Column SectionSDR 96ZZZX799Cylinder · excess wearFOUND CYLINDER EXCESS WEAR. THE NORMAL LIFE OF THIS CYLINDER IS AT 1,500 HOURS TBO. THIS CYLINDER LASTED 1,043 HOURS. PREMATURE WEAR FAILURE SEEMS TO BE AN UNFORTUNATE TREND FOR CERMICHROME CYLINDERS. SUBMITTER RECOMMENDS NORMAL OPERATIONS WATCHING ENGINE Jan 23, 1996 · N7398M · Cessna T210M · Reciprocating Engine Cylinder Section
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