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.

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)Apr 17, 2019 · Piper PA44180 · Engine (Reciprocating)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)Apr 5, 2019 · Piper PA44180 · Rudder/Tab, Attach FittingsSDR 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 HIDDEDec 16, 2016 · N721CK · Piper PA44180 · Reciprocating Engine Cylinder SectionSDR 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.Mar 11, 2016 · Piper PA44180 · Engine Air Intake SystemSDR 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.Feb 16, 2016 · N2150C · Piper PA44180 · Engine Mount SectionSDR 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 CORNERNov 5, 2015 · Piper PA44180 · Reciprocating Engine Power SectionSDR 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 IJun 29, 2015 · Piper PA44180 · Main Landing Gear Attach SectionSDR 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 THEMay 12, 2015 · N302PA · Piper PA44180 · Wing Miscellaneous StructureSDR 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 May 11, 2015 · N292PA · Piper PA44180 · Landing Gear Position and WarningSDR 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 NOApr 22, 2015 · N318PA · Piper PA44180 · Nose/Tail Landing GearSDR 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.Mar 31, 2015 · Piper PA44180 · Rudder StructureSDR 2015FA0000054Landing Gear · collapsedLANDING GEAR COLLAPSED UPON LANDING ROLLOUT. MECHANICAL FAILURE.Jan 15, 2015 · N2126X · Piper PA44180 · Main Landing GearSDR 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 WEREOct 21, 2014 · Piper PA44180 · Starter-GeneratorSDR 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. Feb 18, 2014 · N7703C · Piper PA44180 · Wing SparSDR 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. THEFeb 13, 2014 · Piper PA44180 · Landing Gear System WiringSDR 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 NENov 22, 2013 · Piper PA44180 · Hydraulic Pump (Electric/Engine), MainSDR 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 REASSep 30, 2013 · N21318 · Piper PA44180 · Nose/Tail Landing GearSDR 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 FDec 21, 2012 · Piper PA44180 · Engine StarterSDR 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 Apr 10, 2012 · N7720Y · Piper PA44180 · Power LeverSDR 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. THDec 5, 2011 · N7701A · Piper PA44180 · Wing SparSDR 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 NORMOct 21, 2011 · Piper PA44180 · Magneto/DistributorSDR 2009FA0000398Starter · malfunctionedAFTER SHUTTING DOWN THE LT ENGINE DURING A TRAINING FLIGHT, THE STARTER GEAR WOULD NOT ENGAGE DURING THE RESTART PROCEDURE.May 4, 2009 · N2112F · Piper PA44180 · Engine StarterSDR 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)Mar 18, 2009 · Piper PA44180 · Fuselage, Landing Gear Attach FittingsSDR 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 Oct 3, 2008 · Piper PA44180 · Engine Air Intake SystemSDR 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 WEREJan 22, 2008 · N2095S · Cessna T206H · Pitot/Static SystemSDR CA070823013Connector · broken(CAN) WIRE FOUND BROKEN ON DOWNLIMIT SWITCH CONNECTOR. (TC NR 20070823013)Aug 10, 2007 · Piper PA44180 · Landing Gear System WiringSDR 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 CAApr 5, 2007 · Piper PA44180 · Nose/Tail Landing Gear Attach Section
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