Cessna T210L

Service difficulty reports · 78

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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 = 'T210L'
  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 AU980402Valve · worn(AUS) THREE ENGINE CYLINDERS REMOVED DUE TO LOW COMPRESSION. ALL EXHAUST VALVES PN 646286 AND VALVE GUIDES PN 636242 WERE FOUND TO BE WORN BEYOND LIMITS WITH 0.508MM (.020 INCH), 1.016MM (.041 INCH) AND 1.168MM (.046 INCH) CLEARANCES.Mar 24, 1998 · Cessna T210L · Reciprocating Engine Cylinder SectionSDR 98ZZZX1133Bearing · seizedDURING AN ANNUAL INSPECTION TO CHECK FLAP BEARINGS AFTER A FAILURE ON A CE-172, FOUND 10 OUT OF 12 BEARINGS WITH THE NEEDLE BEARINGS SEIZED. NO VISUAL SIGN OF WEAR. CLEANED, LUBED, REINSTALLED. SUBMITTER RECOMMENDED 1,000-HOUR INSPECTIONS REQUIRING REMOVAL.Jan 26, 1998 · N94035 · Cessna T210L · Trailing Edge FlapsSDR 98ZZZX1132Bearing · seizedDURING AN ANNUAL INSPECTION TO CHECK FLAP BEARINGS AFTER A FAILURE ON A CE-172, FOUND 10 OUT OF 12 BEARINGS WITH THE NEEDLE BEARINGS SEIZED. NO VISUAL SIGN OF WEAR. CLEANED, LUBED, REINSTALLED. SUBMITTER RECOMMENDED 1,000-HOUR INSPECTIONS REQUIRING REMOVAL.Jan 26, 1998 · N94035 · Cessna T210L · Trailing Edge FlapsSDR 98ZZZX442Downlock Shell · deformedON APPROACH, GEAR EXTENDED, LT MAIN GREEN LIGHT FAILED TO ILLUMINATE: EMERGENCY GEAR EXTENSION USED TO LOCK GEAR. DURING INSPECTION, FOUND INTERIOR OF DOWNLOCK SHELL LEFT SIDE PEELED BACK INTERFERRING WITH MAIN LEG FULL TRAVEL, THEREFORE, PREVENTING OVERCENTJan 20, 1998 · N29176 · Cessna T210L · Landing Gear Retraction/Extension SystemSDR 98ZZZX544Piston Assembly · brokenAIRCRAFT EXPERIENCED A NOSE LANDING GEAR FAILURE DURING TAXI OPERATIONS AFTER LANDING. SUBSEQUENT INSPECTION REVEALED THE FORK AND PISTON ASSEMBLY BROKE AT THE CASTING AREA LOCATED AT THE POINT WHERE BOTH FORKS ATTACH TO THE PISTON ASSEMBLY.Dec 28, 1997 · N732DK · Cessna T210L · Nose/Tail Landing Gear Strut/AxleSDR 97ZZZX4793Carry Thru Spar · corrodedINSPECTION FOUND CABIN OVERHEAD CARRY-THROUGH SPAR CORRODED WHERE FRESH AIR DUCT PASSES THROUGH. SUSPECT DISSIMILAR METAL CONTACT.Oct 1, 1997 · N121RJ · Cessna T210L · Wing SparSDR 97ZZZX4140Wheel · crackedBOTH MAIN WHEELS CRACKED. THESE ARE 3-PIECE WHEELS USED ON VARIOUS CESSNA SINGLES IN THE 1970'S. THIS SUBMITTER FEELS A MORE LIKELY CAUSE (OTHER THAN OVERTORQUING) IS STRESS CAUSED BY PULLING SMALL AMOUNTS OF ALUMINUM THROUGH THE THREADS EACH TIME THE BOLTS Aug 1, 1997 · N117P · Cessna T210L · Wheel/Ski/FloatSDR CA971027010Fuel Pump · rusted(CAN) RIGHT AUXILIARY FUEL PUMP FOUND RUSTED. ALSO LEFT AND RIGHT CHECK VALVES PART NO. FACKV-5-100-6 FOUND CLOGGED. THIS AS A RESULT OF INSTALLATION OF FLINT AUXILIARY SYSTEM STC SA2862WE, SA3266NM OR SA4300WE ACCORDING TO SUBMITTER.Jul 17, 1997 · Cessna T210L · Fuel Boost PumpSDR 97ZZZX2851Actuator · crackedDURING ANNUAL INSPECTION, FOUND A CRACK IN THE BEARING END OF THE NOSE GEAR ACTUATOR. THE CRACK ORIGINATES AT THE DOWNLOCK PIN LOCATION AND EXTENDS FORWARD LONGITUDINALLY AROUND THE CASTING. (NO PLAY WAS NOTED IN PIN WHEN C/W SEB 95-20). POTENTIAL OF NOSE GMay 26, 1997 · N732AJ · Cessna T210L · Landing Gear Retraction/Extension SystemSDR 97ZZZX2717Diode Board · failedHOOKED UP APU AND STARTER IMMEDIATELY CRANKED ENGINE. INVESTIGATION FOUND BOARD CONTAINING DIODES IN CABIN NEXT TO POWER RELAY TO HAVE BOTH DIODES INOPERATIVE. PART IS IN DIFFICULT LOCATION TO TEST INDIVIDUAL DIODES. REPLACED DIODE BOARD P/N 1570043-1 AND May 26, 1997 · N732AJ · Cessna T210L · APU Start/Ignition SystemSDR CA970506010Blade · damaged(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. LEADING EDGE OF THE PROPELLER BLADE WAS FOUND DAMAGED. REWORK AND GRINDING WAS REQUIRED TO FIX THE AIRFOIL ON ALL BLADES.Apr 29, 1997 · Cessna T210L · Propeller Blade SectionSDR 97ZZZX2120Spring · brokenTROUBLESHOOTING OF 400 RPM MAG DROP FOUND LEFT MAGNETO TIMING AT 7 DEGREES BTC. REMOVED MAG AND FOUND IMPULSE COUPLING SPRING BROKEN TWO INCHES FROM OUTER END.Apr 23, 1997 · N93377 · Cessna T210L · Magneto/DistributorSDR 97ZZZX805Actuator · bolt looseDURING ANNUAL INSPECTION, FOUND ONE ATTACHMENT BOLT ON EACH MLG ACTUATOR BACKED OUT. SUBMITTER STATES CESSNA SHOULD ADDRESS BY CHANGING P/N BOLTS HAVING BOLT HEADS DRILLED FOR SAFETY WIRE AS IN CAP INSP NR 32-30-01 WHICH IS NOT APPLICABLE TO THIS S/N AIRCRAFTJan 30, 1997 · N93285 · Cessna T210L · Landing Gear ActuatorSDR 97ZZZX966Bracket · crackedDURING A REPLACEMENT OF A TAIL TIE-DOWN RING AND AFT TAIL CONE BULKHEAD ASSY, P/N 1212130-2 AT STA 230.187, CRACKS WERE FOUND ON BOTH LT AND RT SUPPORT BRACKETS. THESE BRACKETS ARE PART OF THE HORIZONTAL STABILIZER SUPPORT ON AFT SIDE UNDER P/N 1212128-1 AND Jan 7, 1997 · N2074S · Cessna T210L · Fuselage Miscellaneous StructureSDR 97ZZZX965Bracket · crackedDURING A REPLACEMENT OF A TAIL TIE-DOWN RING AND AFT TAIL CONE BULKHEAD ASSY, P/N 1212130-2 AT STA 230.187, CRACKS WERE FOUND ON BOTH LT AND RT SUPPORT BRACKETS. THESE BRACKETS ARE PART OF THE HORIZONTAL STABILIZER SUPPORT ON AFT SIDE UNDER P/N 1212128-1 AND Jan 7, 1997 · N2074S · Cessna T210L · Fuselage Miscellaneous StructureSDR 97ZZZX504Crankshaft · brokenENGINE QUIT IN-FLIGHT AND IT WAS DISCOVERED THE CRANKSHAFT HAD BROKEN IN TWO PLACES, JUST AFT OF THE FWD THRUST BEARING. RESEARCH OF LOGS SHOWS THAT THE AIRCRAFT WAS BELLIED 891 HOURS PRIOR TO THE CRANKSHAFT BREAKAGE, AT WHICH POINT THE BELLY WAS REPAIRED, A Nov 18, 1996 · N2076S · Cessna T210L · Reciprocating Engine Power SectionSDR 96ZZZX4733Exhaust System · crackedNEW EXHAUST SYSTEM WAS INSTALLED AT ENGINE CHANGE. 274 HOURS LATER DURING 100-HOUR INSPECTION, NUMEROUS CRACKS WERE FOUND ON RIGHT SIDE OF EXHAUST, BY TURBO INLET AND FRONT RISER.Aug 29, 1996 · N613CW · Cessna T210L · Engine Collector/Tailpipe/NozzleSDR CA960826021Reinforcement · cracked(CAN) HORIZONTAL STAB REINFORCEMENT BRACKET REPLACED WITH HEAVIER REPLACEMENT PART SUPPLIED THROUGH CESSNA.Aug 8, 1996 · Cessna T210L · Horizontal Stabilizer StructureSDR 96ZZZX3558Relay · stuckGEAR POWER PACK RUNS ALL THE TIME WHEN RELAY IS IN STUCK POSITION.Jun 28, 1996 · N29176 · Cessna T210L · Hydraulic Pump (Electric/Engine), MainSDR AU960602Link · broken(AUS) PROPELLER NO1 BLADE PITCH CHANGE LINK BROKEN - FURTHER INSPECTION FOUND INCORRECT BLADE RETENTION NUT 'O' RINGS FITTED - PROPELLER IS GREASE FILLED WITH OIL FILLED PROPELLER 'O' RINGS FITTED TO UNMODIFIED GROOVES - PERSONNEL/MAINTENANCE ERROR - UNAPPROVEMay 10, 1996 · Cessna T210L · Propeller Controlling SystemSDR 96ZZZX1938Switch · inoperativePILOT REPORTED NO DOWN AND LOCK INDICATION. TROUBLESHOT SYSTEM, AND FOUND THE RT MLG DOWNLOCK SWITCH INOPERATIVE. REPLACED SWITCH, OPS CHECKED OK.Mar 21, 1996 · N51TP · Cessna T210L · Landing Gear Position and WarningSDR 96ZZZX1622Valve · spring wornTHE OIL FILTER BYPASS VALVE SPRING WAS FOUND WORN IN-HALF. THE BYPASS VALVE WAS OPEN ALLOWING OIL TO BYPASS THE FILTER.Mar 1, 1996 · N59218 · Cessna T210L · Engine Oil Temperature RegulatorSDR 96ZZZX1560Solenoid · malfunctionGEAR-UP LANDING ON ASPHALT RUNWAY. NO INJURIES. ALL LANDING GEAR DOORS OPENED, BUT GEAR FAILED TO EXTEND EITHER ELECTRICALLY OR MANUALLY. FAILURE CAUSED BY RESIDUE BUILT-UP ON SHAFT OF SOLENOID PN 9881201-1 PREVENTING OPERATION OF MANIFOLD ON POWER PACK. AFeb 4, 1996 · N381DS · Cessna T210L · Hydraulic Pump (Electric/Engine), MainSDR 96ZZZX1249Solenoid · defectiveON FEBRUARY 4, 1996, GEAR-UP LANDING WAS MADE. NO INJURIES. ALL LANDING GEAR DOORS OPENED, BUT GEAR FAILED TO EXTEND BY ELECTRIC HYDRAULIC OR MANUAL HYDRAULIC. FAILURE CAUSED BY SOLENOID RESIDUE BUILD UP ON SHAFT OF SOLENOID PREVENTED OPERATION OF MANIFOLD Feb 4, 1996 · N381DS · Cessna T210L · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZX4205Propeller · failedPILOT COMPLAINED PROPELLER WAS SLUGGISH FOR PAST YEAR. FINALLY, PROPELLER WOULD NOT RETURN TO LOW PTICH AND RUN-UP. DISASSEMBLY REVEALED WATER IN HUB, ACTUATING PINS SEVERELY CORRODED AND BINDING IN LINKS. BLADE RACES SEVERELY RUSTED. UPON INSPECTION, HUB Jul 11, 1995 · N1668X · Cessna T210L · Propeller Hub SectionSDR 95ZZZX3515Switch · failedUPON SELECTING GEAR DOWN, COULD NOT GET GREEN INDICATION FOR DOWN AND LOCKED AND PUMP CONTINUED TO RUN. UPON LANDING, GREEN LIGHT CAME ON. FOUND BAD SWITCH ON RT GEAR DOWNLOCK.Jul 1, 1995 · N15US · Cessna T210L · Landing Gear Position and WarningSDR 95ZZZX2439Control Horn · crackedELEVATOR TRIM TAB CONTROL HORN FAILED CAUSING ELEVATOR TO FLUTTER. FLUTTER WAS STOPPED BY REDUCING POWER, LOWERING LANDING GEAR AND FLAPS. APPEARS CONTROL HORN HAD BEEN CRACKED PREVIOUSLY THROUGH TWO-THIRDS OF ITS LENGTH. TRIM TAB HAD A CONSIDERABLE AMOUNT Apr 27, 1995 · N59046 · Cessna T210L · Rudder Tab Control SystemSDR 95ZZZX1427Cylinders · wornENGINE RUN SMOH WITH MOBIL AV-1 ENGINE OIL. ENG STARTED SHOWING HIGH READINGS OF IRON, CHROMIUM, ALUMINUN ON OIL ANALYSIS. CYLS REMOVED FOR INSP. ALL OIL CONTROL RINGS FND STUCK W/LEAD BUILD-UP & ALL CYL WALLS FND WORN UP TO .014 INCH. ENG REMOVED FROM ACFTFeb 1, 1995 · N210MG · Cessna T210L · Reciprocating Engine Cylinder Section
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