Lycoming O-360-E1A6D
Service difficulty reports · 27
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 = 'O360E1A6D' 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 = 'O360E1A6D' 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 CA190417001Camshaft · corroded(CAN) CAMSHAFT LW16513 AND TAPPETS LW16812 FOUND PITTED WHEN OIL CHANGE AND FILTER INSPECTION CARRIED OUT AD80-0403R2 PAR.B (TC# 20190417001)SDR CA190405011Fitting · cracked(CAN) DURING SCHEDULED 500HR INSPECTION THE END OF THE RUDDER FITTING WHICH ATTACHES THE BOTTOM OF THE RUDDER TO THE FIN AND INCLUDES THE RUDDER STOPS WAS FOUND CRACKED ON THE LEFT FLANGE NEAR THE RUDDER PIVOT. NEW PART INSTALLED. (TC# 20190405011)SDR 2016FA0000663Adapter · brokenLEFT ENGINE OIL FILTER ADAPTER CAST ASSEMBLY BROKE AT THE FITTING WHERE THE OIL CONVERTER PLATE SCREWS IN. THIS ALLOWED THE OIL FILTER ASSEMBLY TO DROP TO THE SIDE CAUSING AN ENGINE OIL LEAK. SUSPECT ADAPTER COULD HAVE BEEN CRACKED FOR SOME TIME AS IT IS HIDDESDR CA160314003Air Box · failed(CAN) INNER MOVING BAFFLE FLAP INSIDE THE CARB AIR BOX THAT CONTROLS WHICH SIDE OF THE AIRFLOW THE CARBURETOR USES WORK HARDENED AND BROKE OFF OF THE SHAFT RESULTING IN THE BROKEN PIECE COMPLETELY COVERING THE INLET TO THE CARBURETOR.SDR 2016FA0000089Mount · damagedDURING ANNUAL INSPECTION FOUND THE ENGINE MOUNT TUBING HAD CHAFE DAMAGE FROM CONTACT WITH THE THROTTLE CABLE DUE TO IMPROPER ROUTING/CLAMPING OF THE CABLE.SDR CA151106001Bearing · failed(CAN) AFTER SCHEDULED OUT OF PHASE OIL AND FILTER CHANGE GROUND RUN. NOTICED LT ENGINE PROPELLER HARD TO MOVE AND NO FORE AND AFT PLAY IN CRANKSHAFT. ENGINE REMOVED AND SENT FOR REPAIR. ENGINE SHOP REPORTED THAT BOTH HALF OF MIDDLE CRANKSHAFT BEARING CORNERSDR CA150630012Bolt · corroded(CAN) UPON DIS-ASSEMBLY OF THE RT MAIN LANDING GEAR TRUNNION, THE BOLT THAT HOLDS THE MAIN GEAR RETAINER ASSY IN PLACE IN THE TRUNNION WAS REMOVED AND FOUND EXTREMELY CORRODED. FAILURE OF THIS BOLT WOULD POSSIBLY CAUSE THE GEAR RETAINER TO FALL OUT RESULTING ISDR FQAR20150512035Angle · crackedDURING A PROGRESSIVE INSPECTION, AN ANGLE IN THE RT WING WAS FOUND CRACKED BEHIND THE LANDING GEAR SIDE BRACE FITTING. THE CRACK COULD JUST BARELY BE SEEN BEHIND THE BRACE, AND WHEN THE BRACE WAS REMOVED, DYE PENETRANT INSPECTION REVEALED IT EXTENDED FROM THESDR FQAR20150512033Downlock Switch · separatedON APPROACH, AS THE GEAR WAS LOWERED THE PILOTS NOTED THERE WAS NO DOWN-AND-LOCKED INDICATION FOR THE RT MAIN GEAR. THE PILOTS ABORTED THE APPROACH AND RAN CHECKLISTS TO GET A POSITIVE GEAR INDICATION WITH NO SUCCESS. THEY WERE ABLE TO PERFORM AN UNEVENTFUL SDR FQAR20150422029Cotter Pin · missingON PREFLIGHT, THE PILOT NOTED THAT A COTTER PIN WAS MISSING FROM THE NLG FORWARD DRAG LINK BOLT, ILLUSTRATED AS ITEM 69D, FIGURE 21. PREVIOUS FLIGHT CREWS DID NOT SEE THE COTTER PIN MISSING, AND THE NUT DID NOT LOOSEN, WHICH SUGGESTS THAT THE COTTER PIN HAD NOSDR CA150401001Attach Fitting · cracked(CAN) DURING ROUTINE INSPECTION, MECHANIC NOTICED A CRACK IN THE LOWER ATTACHMENT OF THE RUDDER TO ACFT. THE CRACKED AREA IS WHERE THE RUDDER PIVOTS AND CONTACTS THE STOPS. THE AGE OF THE BRACKET COULD NOT BE DETERMINED BUT MAY WELL BE ORIGINAL.SDR 2015FA0000054Landing Gear · collapsedLANDING GEAR COLLAPSED UPON LANDING ROLLOUT. MECHANICAL FAILURE.SDR CA141022008Bolt · missing(CAN) DURING TROUBLE SHOOTING OF THE #2 ENGINE MAINTENANCE DISCOVERED THAT A HEX BOLT WAS MISSING FROM THE #2 STARTER WHERE THE DRIVE END ASSEMBLY JOINS THE MOTOR ASSEMBLY. THE MISSING BOLT WAS REPLACED AND THE REMAINDER OF THE HEX BOLTS ON THE #2 STARTER WERESDR ECPR2014061158901Spar · corrodedCORROSION FOUND ON THE BOTTOM CAP OF THE LT WING SPAR ASSY, AT APPROXIMATLEY WING STA 36, JUST INBD OF THE 67071-00 LT LANDING GEAR ACTUATOR ATTACH BRACKET. IN ORDER TO REMOVE THE CORROSION COMPLETELY THE 67071-00 BRACKET NEEDED TO BE REMOVED FROM THE WING. SDR CA140218001Wire · broken(CAN) ACFT HAD NO LT GEAR INDICATION. A MANUAL GEAR EXTENSION WAS CARRIED OUT & THE ACFT LANDED SAFELY. THE ACFT WAS TOWED TO THE HANGER AS A PRECAUTION. UPON INVESTIGATION MAINTENANCE FOUND BROKEN WIRES ON THE LT DOWN LOCK SAFETY SWITCH, PN: 86409-02. THESDR CA131123001Pump · failed(CAN) LANDING GEAR WOULD NOT EXTEND USING ELECTRIC HYDRAULIC PUMP, EMERGENCY GEAR EXTENSION USED, GIVING 3 GREEN. ACFT LANDED SAFELY. FOUND ELECTRIC HYDRAULIC PUMP GETTING POWER FROM SELECTOR, BUT ELECTRIC MOTOR WOULD NOT TURN. REPLACED HYC5005 ASSY WITH NESDR 2013FA0000709Bolt · bentNOSE GEAR COLLAPSED ON LANDING. FOUND NOSE GEAR PIVET BOLT FOR DOWNLOCK, PN 502-341 BENT. PN 86275-03, DOWNLOCK MAY BE BENT. THIS PART INCLUDES THE HOOK. THE LEVER ON DOWNLOCK MICROSWITCH, PN 86409-02 WAS BENT WHEN GEAR RETRACTED. BELIEVE THAT WAS THE REASSDR CA130115007Starter · failed(CAN) UPON START UP OF LT ENGINE STARTER FAILED ON FIRST. STARTER FAILURE TROUBLESHOT TO DETERMINE THE CAUSE AND PROBLEM OF FAILURE. FAILURE FOUND TO BE STARTER ITS SELF. STARTER REMOVED FROM LT ENGINE AND REPLACED NEW, WITH A 149-NL STARTER , NEW STARTER FSDR ECPR201204130001Throttle Cable · detachedON CLIMBOUT, 600-700FT AGL, INSTRUCTOR PILOT (IP) REDUCED RT THROTTLE TO IDLE TO SIMULATE ENGINE FAILURE. STUDENT PILOT (SP) SIMULATED FEATHERING RT PROPELLER AND WHEN ATTEMPTING TO SET ZERO THRUST, IP DISCOVERED THAT THERE WAS NO THRUST AVAILABLE. RT ENGINE SDR ECPR2014061150605Spar · corrodedLT WING STA 56.0, UPPER OTBD QUADRANT OF AN ELECTRICAL WIRE PASSING THROUGH HOLE IN THE WING SPAR WEB WAS FOUND CORRODED. PASS THROUGH HOLE, WHICH IS IN THE LANDING GEAR WHEEL WELL AREA, HAD A CATEPILLAR GROMMET INSTALLED TO PREVENT THE WIRES FROM CHAFING. THSDR CA111116011Distributor Blk · failed(CAN) MAGNETO NOT FUNCTIONING AFTER ENGINE START. DISASSEMBLED MAG, NOTED DISTRIBUTOR BLOCK BURNED AND MELTED. MAGNETO FILLED WITH YELLOW POWDER RESIDUE. EVIDENCE OF ELECTRICAL ARCING BETWEEN COIL AND DISTRIBUTOR BLOCK. NOTED CARBON BRUSH K3215 APPEARED NORMSDR 2009FA0000398Starter · malfunctionedAFTER SHUTTING DOWN THE LT ENGINE DURING A TRAINING FLIGHT, THE STARTER GEAR WOULD NOT ENGAGE DURING THE RESTART PROCEDURE.SDR CA090921002Trunnion · cracked(CAN) FIRST 100 HR FOLLOWING IMPORTATION OF AIRCFRAFT. AIRCRAFT REBUILT FOLLOWING DAMAGE FROM TORNADO PRIOR TO IMPORT. CRACKS EVIDENT VISUALLY 100 HRS AFTER REBUILD. (TC# 20090921002)SDR CA081006004Grommet · missing(CAN) DURING A DEFECT RECTIFICATION ON OUR OTHER ACFT, IT WAS FOUND THAT THE LWR GROMMET AND BUSHING P/N 453-991 WAS MISSING ON THE LT ENGINE CARB HEAT BOX. THIS GROMMET SUPPORTS THE SHAFT IN THE CARB HEAT BOX. THIS PROMPTED THE INSP OF THIS ACFT, WHICH FOUND SDR 2008FA0000066Fitting · failedPRIOR TO COMPLIANCE WITH FAR 91.411, A STATIC SYSTEM CHECK WAS CONDUCTED. UNDER TEST SYSTEM SHOWED APPROXIMATELY 100 FPM DESCENT RATE. INSPECTION REVEALED THE 90 DEGREE PLASTIC FITTINGS (ONE ON EACH SIDE OF THE FORWARD FUSELAGE) FOR STATIC SYSTEM PLUMBING WERESDR CA070823013Connector · broken(CAN) WIRE FOUND BROKEN ON DOWNLIMIT SWITCH CONNECTOR. (TC NR 20070823013)SDR CA070425004Trunnion · cracked(CAN) DURING A PREFLIGHT INSP THE PILOT NOTICED THE NOSE GEAR TRUNNION CRACKED. THE CRACK STARTS FROM THE UPPER PART OF THE CASTING AND GOES DOWN HALFWAY AT WHICH POINT IT SPREADS INTO 3 OTHER CRACKS. THE IDENTICAL CRACK CAN BE FOUND ON THE REAR SIDE OF THE CA
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