Lycoming 0-360-A1D
Service difficulty reports · 82
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 = 'O360A1D' 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 = 'O360A1D' 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 2002FA0000579Slip Joint · leakingREMOVED MUFFLER/ EXHAUST DUCT ASSEMBLY INTERNAL BAFFLES MISSING, AND NR 4 CYLINDER LOWER SLIP JOINT LEAKING.SDR AUS20020352Seat Belt · faulty(AUS) BOTH FORWARD SEAT BELTS WERE OF UNKNOWN ORIGIN WITH NOIDENTIFICATION LABLES. BELTS WERE IN EXTREMELY POOR CONDITION.BELTS DID NOT MEET THE REQUIREMENTS OF AD/RES/29. UNAPPROVEDPART. PERSONNEL/MAINTENANCE ERROR.SDR AUS20020351Strut · cracked(AUS) LH MAIN LANDING GEAR LEG ASSEMBLY CRACKED AT THE UPPER FORWARDWELD JOINT.SDR AUS20020272Link · cracked(AUS) AILERON CONTROL LINK CRACKED IN WELD JOIN.SDR AUS20020273Link · cracked(AUS) AILERON CONTROL LINK CRACKED AT WELDED JOIN.SDR UC22002F00000Control Cable · frayedFOUND RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION.SDR UC22002F00001Control Cable · wornFOUND RIGHT AND LEFT FORWARD STABILATOR CONTROL CABLES FRAYED AND WORN DURING A 100 HOUR INSPECTION. .SDR CA020116007Propeller · damaged(CAN) OWNER DISCOVERED PROP WOULD NOT CYCLE AT PRE-FLIGHT INSPECTION. AIRCRAFT WAS BROUGHT TO THE SHOP AND THE SPINNER WAS REMOVED. GREASE FITTINGS WERE REMOVED AND OIL BEGAN TO RUN OUT. PROP WAS REMOVED AND SENT FOR INSPECTION.SDR AUS20011158Magneto · faulty(AUS) MAGNETOS INTERMITTENT IN OP. INSP FOU NDFOLLOWING FAULTS ON BOTH UNITS:-1. CAPACITORS FOUND TO LEAKING ELECT.LY.2. SPUR GEAR FOUND TO BE OF NYLON TYPE WHICH HAS BEEN OBSOLETE FOR MANY YRS&REQD AS PER BENDIX MASTER MANUAL TO BE REPL. 3. DISTRIBUTOR BLOCKSDR 2001FA0000370Terminal · brokenFORWARD HORIZONTAL STABILIZER STRUT UPPER TERMINAL WAS FOUND BROKEN ON PREFLIGHT. BREAK OCCURED ON .3125 (5/16) THREADED PORTION AT UPPER END OF THREADS.SDR 20010430CW008Pivot · brokenWHILE ON CHECK RIDE, THE RIGHT MAIN LANDING GEAR FAILED TO EXTEND. THE PILOT SUCCESSFULLY MANAGED TO LOCK THE GEAR IN PLACE BY LAYING ON THE FLOOR BEHIND THE PILOTS SEATS, USING HIS HEAD TO HOLD DOOR OPEN, REACHING OUT AND PULLED GEAR INTO POSITION. LANDED SSDR 20010430CW009Pivot · crackedWHILE REPLACING THE RIGHT PIVOT, IT WAS DECIDED TO INSPECT THE LEFT PIVOT ON THIS AIRCRAFT. THE PIVOT SHOWED NO SIGNS OF CRACKING UNTIL ZYGLO TYPE DYE PENETRANT WAS USED UNDER A BLACK LIGHT. THIS REVEALED A TOTAL OF 11 CRACKS THAT RADIATED OUTWARD FROM THE SSDR 20010403CW008Valve · malfunctionedPILOTS REPORTED THAT LANDING GEAR WOULD NOT EXTEND, THEY THEN PULLED THE EMERGENCY EXTENSION VALVE AND THE GEAR LOWERED WITH THREE GREEN. UPON INSPECTION FOUND THE EMERGENCY GEAR EXTENSION VALVE TO BE, SPRAYING HYDRAULIC FLUID IN NOSE BELOW HEATER. THIS IN SDR 20010420CW003Flux Detector · malfunctionedFOUND LONGLIGHT AND STROBES PULLING HSI OFF HEADING IN EXCESS OF 10 DEGREES. NO PLACARDS INSTALLED OR REQUIRED TO NOTIFY PILOT OF THIS CONDITION.SDR 20010222CW008Housing · wornDURING ANNUAL INSPECTION , MAGNETS WERE FOUND TO BE OUT OF TIME TO THE ENGINE. EXAM OF CAM / CONTACT POINT AREA, DISCLOSED OIL AND LG AMTS OF DUST AND ALUMINUM SHAVINGS. DISASSEMBLY OF MAGNETS DISCLOSED BEARING, OUTER RACE / CUP / LOOSE IN THE HOUSING. WESDR 20001204SH013Stack · brokenTHE PIPER COMANCHE BROKE THE RT REAR EXHAUST STACK INSIDE THE CARBURETOR HEAT MUFF. THE PIPE BROKE INSIDE THE CUFF THAT IS WELDED TO THE STACK FOR THE MUFF TO ATTACH TO CAUSING THE STACK TO DROP AND ERODE ITS WAY THROUGH THE MUFF. THE HEAT BEING DIRECTED INSSDR AU001167Structure · corroded(AUS) AIRCRAFT EXTENSIVELY CORRODED IN BOTH WINGS AND FUSELAGE IN NORMALLY INACCESSIBLE AREAS. AIRCRAFT HAD NO CORROSION PROTECTION AT MANUFACTURE.SDR 20000626SH009Crankshaft · brokenAIRCRAFT INVOLVED IN AN ACCIDENT BECAUSE OF AN ENGINE FAILURE. THE ENGINE WAS DISASSEMBLED BY THE MANUFACTURER WITH THE FOLLOWING FINDINGS. THE WRONG PART NUMBER CRANKSHAFT WAS INSTALLED IN THE ENGINE. THE SLUDGE TUBES, P/N 71577, WERE NOT INSTALLED ON THESDR CA000519010Hinge · cracked(CAN) UPON STRIPING OF THE VERTICAL STABILIZER, A CRACK WAS NOTED IN THE UPPER HINGE. THIS AIRCRAFT HAS THE RUDDER BALANCE WEIGHT INSTALLATION. PIPER KIT NR 760705 INSTALLED MARCH 15, 1973. THIS AIRCRAFT WAS VANDALIZED BUT NO VISIBLE DAMAGE TO CONTROL WAS NOSDR CA000516036Structure · corroded(CAN) SEVERE CORROSION FOUND DURING ANNUAL INSPECTION. EXFOLIATION CORROSION FOUND AT LT FLAP 3 AND 4 HINGE BRACKET. INTERGRANULAR CORROSION FOUND AT LT MAIN GEAR LINK ATTACHMENT TO MAIN WING SPAR BRACKET. AT THE LT AND RT FUSELAGE TUBING ATTACHMENT TO MAIN SDR CA000706033Line · damaged(CAN) ON 1 FEB 2000 PILOT REPORTED FLUCTUATING FUEL PRESSURE GAUGE. ALSO IN THE PAST PILOTS FELT IT READ LOW AND SOMETIMES NOTICED A FUEL SMELL. FOUND: THE SHORT CURVED FUEL LINE (NOT SHOWN IN MANUAL) THAT PASSES THROUGH THE CABIN BETWEEN THE FUEL SELECTOR & SDR CA000706032Fuel Cell · leaking(CAN) LEFT FUEL CELL WAS FOUND LEAKING ON NOVEMBER 1999. LEAK WAS REPAIRED ON NOV 28, 1999. LEAK WAS THEN NOTICED AGAIN SHORTLY THEREAFTER. LEAK APPEARED TO COME FROM FORWARD WALL OF CELL. LOWERED FUEL LEVEL UNTIL FUEL SHOWED DRYING IN AREA. AT THIS LEVELSDR AU990371Hose · failed(AUS) ENGINE OIL COOLER OIL RETURN HOSE FAILED. LOSS OF ENGINE OIL. THE AIRCRAFT WAS SEVERELY DAMAGED DURING THE SUBSEQUENT FORCED LANDING.SDR CA990115004Propeller · corroded(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. EXTENSIVE WEAR AND CORROSION MADE THE PROPELLER UNREPAIRABLE. THE PROPELLER WAS RETURNED TO THE CUSTOMER.SDR 98ZZZX872Shroud Spring · failedTHE PUSHROD SHROUD TUBE SPRING RETAINER LOCATED UNDER THE VALVE COVER BROKE, AFTER ABOUT 8 HOURS OF SERVICE, ALLOWING THE SHROUD TUBE TO MOVE AND CREATE EXCESSIVE OIL LEAKAGE.SDR 97ZZZX3974Cam · fracturedPILOT REPORTED ROUGH ENGINE OPS AND HIGH EGT. INSPECTION REVEALED RIGHT MAGNETO CAMSHAFT FRACTURED AND SEPARATED BELOW CAM AT OUTER BUSHING. FRACTURED SURFACE DISPLAYED EVIDENCE OF PREVIOUS FRACTURE. SIXTY HOURS TIME SINCE NEW. AIRCRAFT TOTAL TIME: 2,202.SDR CA970910009Cylinder · oversize(CAN) PROPELLER RECEIVED FOR CORROSION INSPECTION. THE CYLINDER WAS FOUND TO BE OVERSIZE.SDR CA960604001Motor · burnt(CAN) LANDING GEAR REFUSED TO EXTEND AND LOCK. EMERGENCY EXTEND SUCCESSFUL. ELECTRICAL MOTOR BURNT OUT.SDR 96ZZZX2399Filter Screen · splitDURING ANNUAL, OIL PRESSURE SCREEN WAS REMOVED AND CHECKED FOR METAL, ETC. AFTER SCREEN WAS CLEANED IN PARTS WASHER, IT WAS NOTED THE SOLDERED SEAM OF THE INNER FINE MESH SCREEN WAS SPLIT. ON CLOSER INSPECTION, THE OUTER SCREEN SHOWED APPROXIMATELY FOUR STRASDR AU960060Bolt · broken(AUS) NO3 CYLINDER CONNECTING ROD BOLT BROKE CAUSING OTHER BOLT TO BEND AND THEN BREAK - CONNECTING ROD WAS TORN FROM PISTON - MAJOR INTERNAL DAMAGE TO ENGINE AND CRANKCASESDR 95ZZZX6052Valve · loose crimp nutDURING INSPECTION OF THERMOSTATIC BYPASS VALVE PER LYC SB518C, THE RETAINING NUT WAS FOUND LOOSE AND THE SPRING PRESSURE WAS NOTICEABLY LESS THAN OTHER VALVES PREVIOUSLY INSPECTED. ENGINE TSMOH, 320.0 HOURS.SDR 95ZZZX5759Crankcase · crackedRIGHT CRANKCASE HALF FROM PARTING SURFACE LOWER NR 3 BOLT HOLE HAS 1 EACH .25 INCH CRACK FROM BOLT HOLE TO PARTING SURFACE, AND 1 EACH 1.850 INCH CRACK FROM BOLT HOLE INTO CASE WEBBING. SUBMITTER CANNOT DETERMINE THE CAUSE OF CRACK. NOTE: THE PROPELLER GOVE
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