Lycoming LIO-360-C1E6
Service difficulty reports · 18
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 = 'LIO360C1E6' 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 = 'LIO360C1E6' 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 2020FA0000257Rod End · brokenRIGHT ENGINE THROTTLE RESPONSE INEFFECTIVE . FOUND THROTTLE ROD END FAILED .THREADED BALL POPPED OUT OF SOCKET ON ROD ENDSDR CA150204011Stud · broken(CAN) THREE BROKEN STUDS TOP CYLINDER NR 2.SDR CA090112006Stud · broken(CAN) ON ROUTINE INSP, NR 4 CYL UPPER CTR HOLD DOWN STUD WAS FOUND SNAPPED OFF. THE CYL WAS REMOVED AND A WASHER WAS FOUND IN BETWEEN CYL AND CRANKCASE. THIS CAUSED CYL TO BE ON SLIGHTLY ANGLED CAUSING STRESS ON THE HOLD DOWN STUDS CAUSING ONE TO BREAK. ENSDR CA070803012Torque Tube · broken(CAN) THE LT RUDDER CABLE TORQUE TUBE CONNECTION BROKE OFF FROM THE TUBE. RUDDER CONTROL WAS LIMITED TO THE TRIM. (TC NR 20070803012)SDR CA050810004Camshaft · worn(CAN) DURING A ROUTINE INSPECTION, THE OIL FILTER WAS CUT OPEN AND EXAMINED FOR METAL CONTAMINATION IAW MAINTENANCE INSTRUCTIONS. THE FINDINGS WERE TAKEN FOR FURTHER ANALYSIS. IT WAS DETERMINED THAT THE ENGINE WOULD NEED TO COME OFF WITHIN 50 HRS. 28.8 HRS LATSDR CA040107004Distributor Gear · broken(CAN) 8 TEETH BROKEN OFF DISTRIBUTOR GEAR ASSEMBLY. A GEAR HOLDING TOOL WAS USE FOR THE MAGNETO INSTALLATION ON ENGINE NOT RECOMMENDED IAW MFG MSB NR 528 AND MFG SB 658.SDR CA040107003Distributor Gear · broken(CAN) 20 TEETH BROKEN OFF DISTRIBUTOR GEAR ASSEMBLY AND THE DISTRIBUTOR GEAR ELECTRODE BROKEN OFF. FOLLOWING INSTRUCTIONS OF MFG SB 658 FOR CORRECT PRACTICES FOR MAGNETO INSTALLATION ON ENGINE WILL ELEMINATE THE PROBLEM.SDR CA021101002Rib · cracked(CAN) DURING A SCHEDULED 1000 HOUR INSPECTION, THE RIB HAS BEEN FOUND CRACKED IN THE FORWARD BOTTOM CORNER.SDR CA001006004Liner · sheared(CAN) UPON LANDING PILOT USED HARD BRAKING ON A SHORT RUNWAY, RESULTING THAT BRAKE LININGS ON RT SIDE SHEARED OFF CAUSING HYDRAULIC LEAK & LOSS OF PRESSURE. PILOT REACHING END OF RUNWAY MADE A SHARP LEFT TURN CAUSING COLLAPSE OF RT MAIN GEAR.SDR CA000714038Pushrod · bent(CAN) CREW EXPERIENCED ROUGH RUNNING ENGINE (RT) WHILE ON APPROACH. CREW POWERED BACK, LANDING WITHOUT FURTHER INCIDENT. UPON INVESTIGATION BY MAINTENANCE, IT WAS DISCOVERED THAT 2 NUTS HAD BACKED OFF ON THE COVER PLATE FOR THE ROCKER PIN CAUSING THE PLATE TSDR CA991116028Stud · failed(CAN) ITEM SENT FOR TRANSLATION./ STUDS FOUND BROKEN ON NR 3 CYLINDER, WITH CYLINDER BACKED OFF.SDR 98ZZZX774Crankshaft · crackedCRANKSHAFT WAS REMOVED FROM INVENTORY FOR MPI FOLLOWING ADVISORY THAT IMPROPER MACHINE WORK WAS PERFORMED BY AIR AGENCY. SHAFT WAS FOUND TO HAVE CRACKS AT THE JOURNAL RADIUS. THIS CRANKSHAFT WAS RE-WORKED BY FAA - AIR AGENCY AND IS SCRAP.SDR 98ZZZX775Crankshaft · crackedPART WAS REMOVED FOR MPI AS A PRECAUTION. THIS CRANKSHAFT WAS RE-WORKED BY AIR AGENCY AND WAS FOUND TO HAVE CRACKS IN THE JOURNAL RADII.SDR 98ZZZX923Crankshaft · crackedPART REMOVED FOR MPI, AS A PRECAUTION. THIS CRANKSHAFT WAS RE-WORKED BY AIR AGENCY AND WAS FOUND TO HAVE CRACKS IN THE JOURNAL RADII.SDR 97ZZZX1949Cylinder · crackedNR 2 CYLINDER FOUND CRACKED AT THE MOLD LINE THROUGH THE SPARKPLUG HOLE OUT ONTO THE TOP OF THE CYLINDER, THE INTAKE SIDE, RIGHT ENGINE.SDR 96ZZZX5744Piston P In · failedPISTON PIN BROKE IN 2 PIECES CAUSING A CATASTROPHIC ENGINE FAILURE. OCTOBER 8, 1996, LYCOMING ISSUED A MANDATORY SB NR 527B PERTAINING TO THIS SUBJECT. THE PISTON PIN THAT FAILED HAD THE SAME CODE MARKED ON IT (17328) THAT THE SERVICE BULLETIN STATED MUST BESDR CA961003001Bracket · torn(CAN) NOSE GEAR RETRACTED ON LANDING. AWAITING FURTHER INFO FROM FIELD.SDR 95ZZZX1159Coil · crackedDURING INSPECTION PER CUSTOMER INSTRUCTIONS, COIL CRACK WAS NOTED. REMOVED AND TESTED COIL. FOUND HIGH VOLTAGE LEAK OUT FROM CRACK. SUSPECT CAUSE MAY BE FROM MANUFACTURE DATE STAMP IN INSULATION. CRACK LOCATION ABOUT 1 INCH FROM OUTPUT TAB.
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