Continental TSIO-360 series
Service difficulty reports · 77
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 engine_model_key = 'TSIO360' 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.
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 engine_model_key = 'TSIO360' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FFK2004F00001Battery · unserviceableDURING AIRCRAFT STARTUP PILOT HAD HARD TIME STARTING THE ENGINES. AFTER TRYING FOR A FEW MINUTES WITH NO SUCCESS, PILOT WENT TO GET THE GROUND POWER UNIT, UPON RETURNING THE AIRCRAFT BATTERY HAD CAUGHT FIRE MELTING SOME FIBERGLASS AROUND THE BATTERY BOX AND TSDR AKG2003F00002Actuator · wornTHE THREADS IN THE ACTUATOR NUT ARE WORN AND ALLOWING THE NUT TO MOVE ON THE JACK SCREW AND BECOME JAMMED WHEN IT CONTACTS THE STOP ON EITHER END OF TRAVEL NOSE UP OR NOSE DOWN. PART LOCATION IS BETWEEN THE PILOT AND COPILOT SEATS UNDER THE FLOOR PANEL.SDR 2003FA0001113Clamp · brokenFRONT ENGINE TURBO EXHAUST STACK RETAINER CLAMP (TURBINE OUTLET LIP) BAND CLAMP PN S19212 STRAP PORTION FRACTURED AND EXHAUST STACK FELL OFF AIRCRAFT ON TAKEOFF. CLAMP MAY HAVE BEEN CRACKED, AND IT HAD NOT BEEN DETECTED BEFORE FAILURE OCCURRED. CLOSER VISUALSDR 00067669Hub · corrodedCORRISION ON PROPELLER HUB.SDR LZ2R996KWire · separatedENGINE MISSING ON ONE MAGNETO; PULLED MAG AND FOUND WIRE SEPERATED FROM CAPACITOR.SDR R2J2003F00003Skin · crackedDURING ANNUAL INSPECTION, INSPECTOR FOUND 2 EA .750 INCH CRACKS AT WS 124.6B RIVET. FURTHER INSPECTION FOUND 3 CRACKS IN PN 3743301 RIB AT SOME WS CRACKS EXCEEDED 1 INCH IN LENGTH, ALSO AT THE RIVET HOLES CRACKS REPAIRED IAW APPROVED DATA. CAUSE OF CRACKING,SDR R2J2003F00000Structure · damagedDURING ANNUAL INSPECTION, FOUND RUDDER LOOSE AT ATTACHMENT. FITTING BOLT HOLES FOUND ELONGATED. AIRCRAFT ALREADY UPGRADED WITH MFG RUDDER FITTING KIT 7.64-100 (BIGGER BOLTS). THERE IS STILL A PROBLEM IN THIS AREA. SECOND AIRCRAFT FOUND WITH THIS PROBLEM. SDR R2J2003F00001Distributor Gear · arcedWHILE COMPLETEING RECOMMENDED 500 HOURS INTERNAL MAGNETO INSPECTION ON MAGNETO. 569 HOURS SINCE NEW; INSPECTOR FOUND DISTRIBUTOR GEAR ELECTRODE DAMAGED DUE TO ARCING AND OVERHEATING. MAGNETO WAS OPERATING NORMALLY, WAS SOON TO MISFIRE IF ELECTRODE BROKE FRSDR 2002FA0001143Distributor Blk · burnedDURING MAGNETO PERFORMANCE, CHECK PRIOR TO FLIGHT, PILOT NOTED ENGINE WANTED TO QUIT RUNNING WITH RIGHT MAGNETO SELECTED TO OFF. EXTERNAL INSPECTION OF MAGNETO LEFT CHECKED GOOD. REMOVED LEFT MAGNETO AND INSPECTED INTERNALLY. INSPECTION REVEALED .5000 INCH SSDR 2002FA0001209Universal Joint · inoperativeDURING INVESTIGATION OF AUTO PILOT PITCH OSOLATIONS. FOUND UNIVERSAL JOINT AT PITCH TRIM JACK SCREW SQUARE DRIVE ISSING ONE OF THE FOUR STAKED IN ROLL PINS.SDR 10991Control Cable · damagedCABLE STIFF, THIS CABLE RUNS THROUGH THE FIRE WALL AND WITHIN THE TURBO REGION. HEAT GENERATED FROM TURBO ASSEMBLY AFFECTS INSIDE LINNING. RECOMMEND A FIRE JACKET OR ALTERNATE MEANS TO SHIELD CABLE ASSEMBLY FROM HEAT.SDR 2002FA0000798Relay · burnedHAVE FOUND 2-3 RELAYS WITHIN PAST MONTH WITH BURNED CONNECTION TO MFG. THE MAIN BUSS CONNECTIONS OVER TIME HAVE TURNED BLACK AND HAVE ULTIMATELY FAILED.SDR VDN2002F00000Housing · crackedDURING ANNUAL INSPECTION, THE TURBOCHARGER HOUSING PART NUMBER COULD NOT BE DETERMINED. THE TURBO HOUSING WAS REMOVED TO CHECK APPLICABILITY WITH AD. IT WAS DETERMINED THAT THIS TURBO HOUSING DOES NOT HAVE TO BE INSPECTED PER PARAGRAPH (J) OF AD DUE TO PART SDR GMZ2002F00000Hose · failedNOSE GEAR WILL NOT EXTEND. NEW HOSES FABRICATED 8 HOURS BEFORE, MALFUNCTIONED. RETEST HOSE, REMOVED AND CHECKED FOR RESTRICTIONS. RESTRICTION EVIDENT. REMOVED ORIFICE AND FILTER AT FIREWALL. FOUND RUBBER TRAPPED ORIFICE (UPSTREAM) AND RUBBER AND METAL PARSDR 2002FA0000307Windshield · departedAT APPROXIMATELY 17,000 FEET CO-PILOTS WINDSHIELD DEPARTED AIRCRAFT, RECOMMEND LARASCOPE INSPECTION OF WINDSHIELD HOLES. TOTAL TIME ON PART 6,234.9.SDR EEJ2002F00001Channel · inoperativeON TAKE OFF WHEN THE PILOT RETRACTED THE GEAR. HE HEAD A STRANGE NOISE FROM THE NOISE GEAR AREA. WHEN HE PUT THE GEAR HANDLE DOWN. THE NOSE GEAR EXTEND ABOUT 45 DEGREES. UPON INSPECTION AFTER LANDING THE TILLER BALL (95387-00) HAD COME OUT OF THE STEERING SDR T9Z2002F00000Boot · crackedREMOVED HORIZONTAL DEICE BOOT DUE TO CONDITION. DURING CLEANUP AND INSPECTION CRACKS WERE FOUND IN LEADING EDGE AT RIVET LOCATIONS AT RIBS. DEFECTS APPEAR TO BE CAUSED FROM IMPROPERLY DIMPLED HOLES. THERE ARE NO INSPECTION PANELS FOR LEADING EDGE, SO VISUALSDR 2001FA0000659Torque Tube · damagedWHILE INSPECTING RUDDER ON ANNUAL INSPECTION THE INSPECTOR FOUND LOOSENESS AT THE RUDDER TORQUE TUBE ATTACH BOLTS. TEARDOWN INSPECTION SHOWED BOLT HOLES OVERSIZE AND ELONGATED. NEW PARTS INSTALLED BECAUSE (AN 174) BOLTS WERE LARGEST SIZE BOLTS PERMITTED. MFSDR 2001FA0000550Switch · stuckDURING TRIM ADJUSTMENT, PILOT EXPERIENCED AN UNCOMMANDED NOSE DOWN ATTITUDE. GROUND INVESTIGATION REVEALED THAT THE ELEVATOR TRIM SWITCH HAD STUCK IN THE NOSE DOWN POSITION.SDR WD42002F00000Line · wornAIRCRAFT TOOK OFF AND LANDING GEAR FAILED TO RETRACT FULLY. OPERATOR CYCLED GEAR DOWN AND THE RIGHT MAIN GEAR DOWN LOCK LIGHT FAILED TO ILLUMINATED. THE AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. EVALUATION OF THE SYSTEM REVEALED A LEAK IN THE USDR 20010319CW002Fuel Line · leakingWHILE INVESTIGATING FUEL SMELL INSIDE AIRCRAFT, FOUND FUEL CROSSFEED LINE BELOW FLOOR LEAKING. LINE ATTACHES DIRECTLY TO MAIN FUEL TANK AND RUNS UNDER FLOOR TO OTHER FUEL SOV. LINE FAILED DUE TO CORROSION DUE TO WATER NOT BEING SUMPED FROM FUEL DRAIN POINTS.SDR 20010403CW006Contactor · damagedBATTERY MASTER CONTACTOR INTERMITTANT. REMOVED AND INSPECTED CONTACTOR. FOUND BOTTOM COVER FULL OF WATER AND CONTACTS RUSTED. INSTALLED NEW CONTACTOR, OPERATIONAL CHECK SATISFACTORY. INSPECTED AFT BAGGAGE DOOR SEAL AND SURROUNDING SKIN SEAMS FOR SOURCE OF WSDR ECA2003F00000Rib · crackedRIB HAD SMALL CRACK JUST ABOVE FORWARD SCREW HOLE THAT HOLDS BALANCE WEIGHT CAUSE MAYBE OVER TORQUE OF HARDWARE.SDR 20001101SH031Controller · stuckTHE CONTROLLER PISTON STICK IN. A SPLIT IN POWER SETTING IN-FLIGHT AND ON THE GROUND. CONTROLLER REPLACED. (X)SDR 20000811SH012Pump · damagedPILOT REPORTED WHEN ELECTRIC FUEL WAS TURNED ON, THE ELECTRIC FUEL PUMP AND ALTERNATOR FIELD CIRCUIT BREAKERS TRIPPED. INSPECTED FUEL PUMP AND FOUND LEAD-IN WIRE TO ELECTRIC PUMP HAD PULLED OUT OF HOUSING AND WAS SHORTING TO GROUND. (X)SDR 98ZZZX3425Induction Tube · crackedFOUND CLYINDERS NR 3 (PN 649263) AND NR 4 (PN 649264) INDUCTION TUBES CRACKED UNDER THE INDUCTION TUBE FLANGES (PN 646933).SDR 97ZZZX4207Fitting · brokenFITTING BROKE IN THREADS WHERE THEY SCREW INTO THROTTLE CONTROL. ENGINE QUIT IN FLIGHT. CONTINUED FLIGHT ON OTHER ENGINE TO BNA. PILOT SAW FUEL COMING FROM COWLING AFTER ENGINE QUIT. REMOVED AND REPLACED BROKEN FITTINGS. LEAK AND OPS CHECK OK. FITTING AP
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