Lycoming O-360-C2E
Service difficulty reports · 129
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 = 'O360C2E' 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 = 'O360C2E' 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 CA050819009Control Cable · frayed(CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY.SDR CA050819010Control Cable · frayed(CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY.SDR CA050819011Control Cable · frayed(CAN) RT FLAP CABLE FRAYED AT WING ROOT PULLEY.SDR CA050819012Control Cable · frayed(CAN) LT AND RT FLAP CABLES FRAYED AT WING ROOT PULLEYS.SDR CA050812003Mount · cracked(CAN) ON THE RT WING IB MOST FLAP MOUNT THERE ARE SEVERAL SMALL CRACKS PROTRUDING OUT OF THE LOWER BOLT HOLE WHICH IS USED TO ATTACH THE BRACKET TO THE REAR SPAR OF THE WING.SDR CA050812004Mount · cracked(CAN) ON THE LT WING IB MOST FLAP MOUNT THERE ARE SEVERAL SMALL CRACKS AND ONE LARGE CRACK PROTRUDING OUT OF THE LOWER BOLT HOLE WHICH IS USED TO ATTACH THE BRACKET TO THE REAR SPAR OF THE WING.SDR CA050211001Leg Assy · delaminated(CAN) AS INSTRUCTED BY INSPECTION REPORT C-12-B80-00/NF-001, AME 118, OUT OF PHASE TASKING (MAIN LANDING GEAR SPRING): COMPLIANCE BI-ANNUAL OR 700 HOURS WHICH EVER COMES FIRST. THE GEAR LEGS WERE REMOVED AND SENT FOR NDT. AT NDT THE SUBJECT GEAR LEG WAS FOUNSDR CA041104003Leaf Spring · brokenCENTER LEAF SPRING FOUND BROKEN AT ASSY ALIGNMENT DIMPLE. ALL FLEET A/C LEAF SPRINGS WHERE REPLACED APPROX JUNE 2003. THIS IS THE 4RTH A/C SPRING ASSY FAILURE IN 3 MONTHS. SUSPECT ALL FLEET AIRCRAFT LEAF SPRINGS ARE DEFECTIVE AND SPLAYING/STRAINING TO FAILURSDR CA041013002Leaf Spring · broken(CAN) MAIN LEAF SPRING BROKEN AT TOW BRIDLE CAGING BOLT. APPROX. 4 INCHES AFT OF SPRING ASSYU BAR. THESE ARE RECENTLY PURCHASED, NEW BATCH TYPE, LEAF SPRINGS.SDR CA041013003Leaf Spring · broken(CAN) 4, MAIN LEAF SPRING, BROKEN APPROX 4 INCHES AFT OF U BAR. -5 AND -6 SPRINGS BROKEN AT AFT EDGE OF U BAR AND -6, TOP SPRING, PUSHING UP AGAINST BOTTOM OF RUDDER HORN. THESE ARE RECENTLY PURCHASED NEW BATCH TYPE LEAF SPRINGS.SDR CA041013004Leaf Spring · broken(CAN) MAIN LEAF SPRING BROKEN AT TOW BRIDLE CAGING BOLT. APPROX 4 INCHES AFT OF SPRING ASSY U BAR. THESE ARE RECENTLY PURCHASED NEW BATCH TYPE SPRINGS.SDR CA040816001Control Cable · frayed(CAN) LT AND RT CABLES FRAYED AT WING ROOT PULLEYS. CABLES REPLACED WITH GALVANIZED.SDR CA040525002Control Cable · frayedSTAINLESS STEEL CABLES, LT AND RT, FLAP CONTROL AT WING ROOT PULLEYS FRAYED.SDR CA040323003Tube · broken(CAN) AS INSTRUCTED BY THE NATIONAL DEFENSE SPECIAL INSPECTION, THE VERTICAL TUBE, ON THE LT SIDE OF THE A/C JUST ABOVE THE LANDING GEAR TUBE STRUCTURE, WAS FOUND BROKEN JUST ABOVE THE WELD.SDR CA031217001Control Cable · frayed(CAN) DURING THE COMPANIES STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE FLAP CABLE ATTACHED TO THE FLAP HANDLE WAS FOUND FRAYED AS IT STARTS TO ENTER AND TURN AROUND THE SECTOR (P/N 3-1128). THERE WAS NO INDICATION OF FRAYING UNTIL THE CABLE WAS REMOVSDR CA031203001Tube · broken(CAN) VERTICAL FRAME TUBE JUST ABOVE AND ATTACHING TO MLG TRUSS FITTING BROKEN JUST ABOVE WELD AT MLG FITTING.CRACK TRAVELS COMPLETELY AROUND AND SECOND CRACK GOES VERTICAL 2 INCHES FROM FIRST LOWER CRACK, THEN AROUND THE TUBE AGAIN APPROX 75 PERCENT.SDR CA031203002Support · cracked(CAN) FUEL TANK SUPPORT BRACKETS CRACKED AT ENDS DIRECTLY OFF OF WELDS. 5 OUT OF 6 BRACKETS CRACKED IN LT WING AND ONLY 1 FOUND CRACKED IN RT WING.SDR CA031203003Support · cracked(CAN) FUEL TANK SUPPORT BRACKETS FOUND CRACKED AT ENDS DIRECTLY OFF OF WELDS. 3 IB BRACKETS CRACKED IN RT WING NONE IN LT WING. NUMBER OF CRACKS VARY FROM 2 TO ALL 4 POINTS OF EACH BRACKET.SDR CA031201002Wire · chafed(CAN) NAV WIRE IN LT WING FOUND ATTACHED WITH MASKING TAPE TO COMPRESSION TUBE. WIRE WAS CHAFING ON TUBE AND EXPOSED WIRE CAUSING SHORT AGAINST COMPRESSION TUBE, BLOWING FUSE.SDR CA031201004Wire · chafed(CAN) NAV WIRE IN LT WING FOUND ATTACHED WITH MASKING TAPE TO 2ND AND 3RD COMPRESSION TUBES FROM OB, AND RT WING FOUND ATTACHED WITH MASKING TAPE TO 3RD (FROM OB) COMPRESSION TUBE. WIRES CHAFFING ON TUBE AND EXPOSED WIRE CAUSING SHORT AGAINST COMPRESSION TUBESDR CA031128005Mount · cracked(CAN) ON THE COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), FLAP MOUNT (LEFT WING ROOT POSITION) WAS INSPECTED AND CRACKS WERE FOUND ON THE MOUNTING FACE BOTTOM BOLT HOLE.SDR CA031128003Wire · misrouted(CAN) DURING COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), FABRIC WAS REMOVED FROM THE WINGS. ON INSPECTION OF THE WIRES, IT WAS DISCOVERED THAT THE POWER WIRES FOR THE NAV AND STROBE LIGHTS WERE INCORRECTLY ROUTED ALLOWING THE WIRES TO RUB ON A RISDR CA031006002Control Cable · frayed(CAN) RT FLAP CABLE FRAYED AT WING ROOT PULLEY AT FLAP FULL DOWN POSITION.SDR CA030825002Pedal · cracked(CAN) AME WAS DOING A QUICK VISUAL OF THE COCKPIT AREA BEFORE THE AIRCRAFT WAS TO LEAVE FOR THE DAYS FLIGHT, WHEN HE NOTICED A CRACKED ON THE FACE OF THE PEDAL. ON FURTHER INPECTION OF THE PEDAL IT WAS DISCOVERED THAT THE CRACK CONTINUED AROUND THE BACK ON INTSDR CA030814002Control Cable · frayed(CAN) STAINLESS STEEL CABLE, RT FLAP CABLE FRAYED AT PULLEY WHEN FLAPS SELECTED DOWN.SDR CA030814003Control Cable · frayed(CAN) CABLES ARE STAINLESS STEEL. LT AND RT CABLES FRAYED AT CABIN PULLEY IN NEUTRAL POSTION.SDR CA030815001Mount · corroded(CAN) DURING THE 100 HR INSPECTION, A SMALL RUST LINE WAS DETECTED ON THE UPPER LT MOUNT LOCATION AT THE WELD. FURTHER INSPECTION WITH 10 POWER MAGNIFYING GLASS DETERMINED THAT THE AREA WAS CRACKED 1/2 INCH.SDR CA030723001Cable · frayed(CAN) LT & RT CABLES FRAYED AT CABIN PULLEYS. CABLES ARE STAINLESS STEEL AND REPLACED WITH GALVANIZED.SDR CA030716002Control Cable · frayed(CAN) LT AND RT RUDDER CABLES FRAYED AT FUSELAGE PULLEYS WITH RUDDER NEUTRAL.SDR CA030722002Control Cable · frayed(CAN) CABLE FOUND FRAYED AT THE PULLEY PN 1-2395.THE AREA TENDS TO BE A HIGH WEAR BECAUSE OF THE SIZE OF PULLEY AND IS MONITORED CLOSELY AT ALL INSPECTIONS. FAILURES HAVE OCCURED IN THE PAST WITH THIS COMPANY.SDR CA030707002Control Cable · frayed(CAN)TE FLAP CABLE FRAYED AT UPPER RT PULLEY.SDR CA030616002Cable · frayed(CAN) CABLE IS FRAYED AT UPPER ALUMINUM PULLEY.SDR CA030218006Tube · cracked(CAN) AIRCRAFT HAS OVER 2,700 HOURS OF TOWING GLIDERS OFF A GRASS STRIP. DEFECT WAS FOUND DURING RECOVERING OF FUSELAGE. VERTICAL CRACK ON BOTH SIDES OF LT REAR GEAR 'U' BOLT BUSHING IN 'U' BOLT ATTACH TUBE.SDR CA021114004Control Cable · frayed(CAN) CABLE FRAYED AT WING ROOT PULLEY- STAINLESS STEEL CABLESDR CA021031005Control Cable · frayed(CAN) LT & RT RUDDER CABLES FRAYED AT PULLEYS - MINIMAL DEFLECTION AT PULLEY. - UNSURE AS TO WHY THEY ARE FRAYED. - REPLACING STAINLESS CABLES WITH GALVINIZED.SDR CA021031006Control Cable · frayed(CAN) CABLE FRAYED AT WING ROOT ALUMINUM PULLEY.- NEW CABLE FABRICATED WITH GALVINIZED. - OLD CABLE WAS STAINLESS STEEL.SDR CA021031007Control Cable · frayed(CAN) LT & RT RUDDER CABLES FRAYED AT PULLEY. MINIMAL DEFLECTION AT PULLEY. THEREFORE UNSURE AS TO WHY THEY ARE FRAYED. - REPLACING STAINLESS CABLES WITH GALVINIZED.SDR CA021007005Fuel Tank · cracked(CAN) CRACK IN LT INBOARD FUEL TANK UPPER SURFACE AT OUTBOARD END OF CENTER PREFORMED STIFFENER. - IN ALUMINUM SPAR WINGS.SDR CA020913009Spar · cracked(CAN) CRACK FOUND IN THE FUEL CELL STIFFENER SPAR ON THE WING.SDR CA020830023Structure · cracked(CAN) FUEL FITTING BOSS FOUND CRACKED AROUND WELD APPROXIMATELY 1 INCH IN LENGTH. THE CRACK IS IN THE LOWER AFT RT THREADED NIPPLE.SDR CA030825004Pedal · cracked(CAN) A/C ARRIVED FOR SUMMER OPERATION. THE AME TOOK A QUICK LOOK THROUGH THE COCKPIT AND NOTICED THE RIGHT PEDAL SYSTEM LOOSE. ON FURTHER INSPECTION, HE NOTICED THE FORWARD RIGHT PEDAL BENT AND CRACKED ON THE RIGHT MOUNT SUPPORT.SDR CA030722001Control Cable · frayed(CAN) CABLE FOUND FRAYED AT THE PULLEY PN 12395.THE AREA TENDS TO BE A HIGH WEAR BECAUSE OF THE SIZE OF PULLEY AND IS MONITORED CLOSELY AT ALL INSPECTIONS. FAILURES HAVE OCCURED IN THE PAST WITH THIS COMPANY.SDR CA020524006Cable · frayed(CAN) LT AND RT UPPER FLAP CABLES FRAYED AT WING ROOT PULLEYS WITH 2ND NOTCH OF FLAP SELECTED.SDR CA020523013Control Cable · frayed(CAN) LT UPPER FLAP CABLE FAYED AT WING ROOT PULLEY ON SECOND NOTCH OF FLAP.SDR CA020507018Control Cable · frayed(CAN) LT AND RT FLAP UPPER CABLES FRAYED AT WING ROOT PULLEYS.SDR CA020507017Control Cable · frayed(CAN) LT AND RT UPPER FLAP CABLES FRAYED AT WING ROOT PULLEY.SDR CA020121001Frame · broken(CAN) -TUBE FOUND BROKEN THROUGH NEAR WELD, AT FWD ENDOF LT LANDING GEAR FITTING.SDR CA011205001Rib · cracked(CAN) 3 RIBS RT, 2 RIBS LT WING FOUND CRACKED AT UPPER CORNER OF FLANGE WHERE RIB ATTACHES TO REAR SPAR. ALL RIBS LOCATED CLOSEST INBOARD AT WING ROOT, AND ALL RIBS CRACKED EXACTLY THE SAME.SDR CA011221004Tube · broken(CAN) TUBE FOUND BROKEN THROUGH APPROXIMATELY AT WELD TO RT FORWARD END OF LDG FITTING.SDR CA011130003Pulley · seized(CAN) LT & RT PULLEYS AT WING ROOT FOUND SEIZED AND WORN. BOTH FLAP CABLES FRAYED AT SAME LOCATION.
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