Lycoming IO-360-C1E6
Service difficulty reports · 67
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 = 'IO360C1E6' 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 = 'IO360C1E6' 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 AU990360Swivel · worn(AUS) THROTTLE CONTROL CABLE SWIVEL WORN AND SEPARATED FROM THE BALL JOINT.SDR CA990202011Lifter · worn(CAN) DURING INSPECTION, METAL WAS DETECTED IN BOTH ENGINE OIL FILTERS. THE METAL WAS SENT TO LYCOMING FOR ANALYSIS. IT WAS DETERMINED THE METAL CAME FROM THE HYDRAULIC LIFTER HOUSING. THE TWO ENGINES WERE TAKEN OUT OF SERVICE AND SENT FOR REPAIR.SDR CA981216003Joint · failed(CAN) NO RESPONSE WHEN PILOT THROTTLE BACK ON LEFT ENGINE. THE BALL HAD COME OUT OF THE JOINT ASSEMBLY AT THE THROTTLE BODY. RIGHT ENGINE THROTTLE BALL JOINT HAD BEEN REPLACED 13.1 HOURS PREVIOUS. SUMBITTER NOTES THAT THEY ARE FOLLOWING PIPER SL 747 (WEAR CSDR AU981138Motor · failed(AUS) LANDING GEAR MOTOR COMMUTATOR SEGMENT HAD OPEN CIRCUIT.SDR AU971620Mount · cracked(AUS) NOSE LANDING GEAR MOUNT TUBE TO CENTERING CHANNEL WELD FAILED.SDR CA970702024Trunnion · broken(CAN) APPROXIMATELY 1.5 INCH SECTION OF THE TRUNNION LUG ON THE RIGHT HAND SIDE BROKE OFF. THIS ALLOWED THE NOSE GEAR TO TRACK OUT OF POSITION BY APPROXIMATELY 15 DEGREES.SDR CA970603027Spring · loose(CAN) NLG LIGHT WOULD NOT COME ON TO INDICATE DOWN AND LOCKED. FLY-BY INDICATED NLG IN LANDING POSITION. AIRCRAFT LANDED AND NOSE GEAR COLLAPSED SHORTLY AFTER TOUCHDOWN. MOST FLUID LOST DUE TO PERFORATED PRESSURE LINE P/N 95153-43 AFTER GEAR SELECTED UP. ESDR AU970254Bulkhead · corroded(AUS) FUSELAGE REAR BULKHEAD CORRODED IN AREA OF STABILATOR ATTACHMENT BRACKETS - RIVETS POPPED AT FRAME OF FORWARD FIN ATTACHMENT AREA- FOLLOWING REMOVAL OF TOP AFT FUSELAGE SKIN AND SKIN ON FIN AND STABILISER. WIDE SPREAD SURFACE CORROSION WAS FOUND WHERE SDR CA961028001Gear Assembly · broken teeth(CAN) DURING A MAGNETO INSEPCTION FOR ENGINE TIMING CHECK, MAINTENANCE FOUND TWO MISSING TEETH ON THE DISTRIBUTOR GEAR. NO REPORTS OF ENGINE RUNNING IRREGULAR. THE MAGNETO WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR AU960564Side Brace · cracked(AUS) LH AND RH MAIN LANDING GEAR SIDE BRACE STUDS CRACKED IN RADIUS - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/PA34/46SDR AU960452Stud · cracked(AUS) MAIN LANDING GEAR SIDE BRACE STUD CRACKED - FOUND DURING MAGNETIC PARTICLE INSPECTION (MPI) IAW AD/PA34/46SDR 96ZZZX5287Pump · port blockedAN AUSTRALIAN BASED PA-34 PILOT REPORTED ENGINE FAILURE DUE TO FUEL STARVATION. CAUSE WAS A RUBBER WASHER BLOCKING THE FUEL OUTLET PORT OF A NEW TEXTRON FUEL PUMP. TEXTRON SB 525 ADDRESSES THE PROBLEM. NO AIRWORTHINESS DIRECTIVE HAS BEEN ISSUED TO DATE. SUSDR AU960087Pump Valve · blocked(AUS) LH ENGINE DRIVEN FUEL PUMP OUTLET VALVE BLOCKED BY FOREIGN OBJECT- ROUND RUBBER WASHER 19MM (0.74IN) IN DIAMETER WITH A 6MM (0.236IN) HOLE WHICH SEPARATED FROM THE DIAPHRAGM ASSEMBLY - INVESTIGATION FOUND NO DAMAGE TO THE RUBBER WASHER AND IT IS SUSPECTESDR CA960222009Breather · blocked(CAN) AFTER TAKEOFF, THE PILOT NOTICED THE OIL PRESSURE DROPPING ON THE RIGHT ENGINE. AS IT APPROACHED THE CAUTION ARC ON THE GAUGE, HE ELECTED TO SHUT DOWN ENGINE AND RETURN TO AIRPORT.HE THEN NOTICED LEFT ENGINE PRESSURE DROPPING AND DECLARED AN EMERGENCY. ESDR CA960306004Breather · blocked(CAN) DURING CRUISE, PILOT NOTICED ROUGHNESS IN THE RIGHT ENGINE AND HE REDUCED POWER. THE PILOT ELECTED TO SHUT THE ENGINE DOWN AND RETURN TO ORIGIN, AS HE DID WITHOUT FURTHER INCIDENT. INSPECTION REVEALED THAT THE ENGINE BREATHER ICE CONTROL APERTURE HAD FROSDR 95ZZZX6393Connect Rod · failedDURING LEVEL FLIGHT WITHOUT INDICATION OF POSSIBLE PROBLEM, THE ENGINE FAILED. PROBLEM WAS DETERMINED TO BE A BROKEN CONNECTING ROD BOLT. ENGINE CASE WAS DESTROYED. AIRCRAFT WAS NOT DAMAGED.SDR 95ZZZX2733Coil · burnedENGINE FAILED TO START. PROBLEM TRACED TO A BURNED THROUGH IGNITION COIL ON THE LT MAGNETO. COIL WAS BURNED THROUGH AT THE FRONT OF COIL (WHERE PN IS PRINTED) AND WAS ARCING TO THE MAGNETO CASE. MAGNETO IS ONLY 2 YEARS OLD AND ONLY HAS 250 HOURS TIME IN SER
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