Lycoming IO-360-C1C

Service difficulty reports · 82

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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 = 'IO360C1C'
  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 2022FA0000178None · crackedWHILE PERFORMING A FUSELAGE SKIN REPAIR. THE RH WING WAS REMOVED. AN EDDY CURRENT INSPECTION WAS PERFORMED ON THE WING SPAR ATTACH FITTINGS, UPPER AND LOWER. FOUND A CRACK APPROX. 3 INCHES LONG ON THE UPPER SPAR FACE, ORIGINATING FROM THE OUTBOARD, FORWARD, SEMar 31, 2022 · N872WL · Piper PA28R200 · Wing Main, Frame StructureSDR 2020FA0000264Wire · chafedNOSE LANDING GEAR FAILURE ON ENGINE STARTUP. OWNER TOWED AIRCRAFT FROM HANGAR FOR A VFR FLIGHT. PREFLIGHT INSPECTION PERFORMED WITH NO ISSUES. PRESTART CHECKLIST PERFORMED. OWNER STATED THAT HE STARTED AIRCRAFT, AND WHEN BRINGING THE ENGINE MIXTURE UP FROMMay 28, 2020 · N7KL · Piper PA28R200 · Landing Gear System WiringSDR 2020FA0000152Guide · crackedTHIS MALFUNCTION LEAD TO A NOSE GEAR UP LANDING. THE NLG APPEARS TO HAVE RETRACTED IN AN OFF-CENTER POSITION. INSPECTION POST INCIDENT REVEALED A CRACKED ALIGNMENT GUIDE, WHICH IS FIXED TO THE TOP OF THE NLG STRUT. THIS PART IS RESPONSIBLE FOR ENSURING THE Jun 16, 2018 · N16566 · Piper PA28R200 · Nose/Tail Landing GearSDR 2018FA0000112Ammeter · arcedSTUDENT PILOT AND INSTRUCTOR REPORTED RADIOS QUIT AFTER A LOUD BUZZING SOUND WAS HEARD THROUGH THE HEADSETS FOR A FEW SECONDS. RADIOS STARTED FUNCTIONING NORMALLY A FEW SECONDS AFTER. BETWEEN 15 - 20 MINUTES LATER SMOKE STARTED COMING FROM BEHIND THE PANEL, OMar 20, 2018 · N56353 · Piper PA28R200 · DC Indicating SystemSDR 2017FA0000262Stud · missingDURING ROUTINE 50-HOUR SERVICE, DISCOVERED THE NR 2 CYLINDER HOLD DOWN STUDS WERE MISSING AND ONE WAS BACKING OUT. THERE WAS NO REPORTED ISSUE, EVEN FROM THE MECHANIC WHO GROUND RAN THE ENGINE.Jun 28, 2017 · N75278 · Reciprocating Engine Cylinder SectionSDR NKVR2016030901Mount · crackedENGINE WAS REMOVED FOR O/H, THE ENGINE MOUNT WAS INSPECTED AND REJECTED DUE TO CRACKS.Mar 7, 2016 · N56720 · Piper PA28R200 · Engine Mount SectionSDR 5HAS2015102700504Radio · failedCOM 2 RADIO FREQUENCY KNOBS FOR COM/NAV HAD PLAY INSIDE THE RADIO. THE PLAY ALLOWED THE KNOB TO FREE SPIN. THE OPERATOR COULD NOT SELECT PROPER FREQUENCY.Oct 26, 2015 · N1430X · Piper PA28R200 · VHF Communications SystemSDR 2015FA0000517Exhaust Stack · separatedEXHAUST STACK SEPARATED AT THE WELD OF THE ENGINE EXHAUST MANIFOLD MOUNT, NR 1 CYLINDER.Oct 20, 2015 · N9301N · Piper PA28R200 · Engine Collector/Tailpipe/NozzleSDR 2015FA0000453Joint · separatedTHE THROTTLE CONNECTION TO THE CARBURETOR IS CONNECTED BY A JOINT ASSEMBLY, BALL, SPRING TYPE, THE JOINT ASSY SEPARATED FROM THE "BALL" WHICH IN TURN DISCONNECTED THE THROTTLE FROM THE CARBURETOR, CREATING NO CONTROL OF THE THROTTLE ACTION.Sep 15, 2015 · N95HF · Piper PA28R200 · Fuel Control/Reciprocating EnginesSDR 2015FA0000288Stud · brokenCYLINDER BASE STUDS BROKE ON NR 3 CYLINDER. APPEARS TO HAVE STARTED FROM THE BOTTOM RIGHT PART NUMBER 76220-P01 THRU STUD BROKE AT THE CYLINDER BASE AND .500 NUT. THE REST OF THE STUDS BROKE DUE TO INCREASED LOAD FROM THE BROKEN 76220 STUD.Jun 25, 2015 · N4861T · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR 2015FA0000092Cylinder · separatedIN-FLIGHT . ENGINE BEGAN TO RUN VERY ROUGH. ACFT RETURNED TO AIRPORT, ENGINE WAS SHUTDOWN ON RUNWAY. INSPECTION OF ENGINE FOUND NR 1 CYLINDER SEPARATING FROM CASE, CYLINDER HOLD DOWN NUTS SHEARED OFF, ALL EXCEPT AFT LOWER HOLD DOWN NUT, AND STUD WAS BENT.Feb 28, 2015 · N8734E · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR 2015FA0000038Fitting · looseAIRCRAFT LOST OIL PRESSURE DURING DECENT WHICH CAUSED AN ENGINE FAILURE. THE PROP GOVENOR OIL SUPPLY LINE FITTING WAS LOOSE ALLOWING HIGH PRESSURE OIL TO ESCAPE. THIS CAUSED OIL STARVATION AND CONNECTING ROD FAILURE. THIS CAUSED ENGINE FAILURE AND AN EMERGEJan 28, 2015 · N1147X · Piper PA28R200 · Propeller GovernorSDR 2013FA0000423Throttle · disconnectedLACK OF THROTTLE CONTROL ON APPROACH TO AIRPORT.Jul 27, 2013 · N5083S · Piper PA28R200 · Power LeverSDR 2011FA0000650Trunnion · crackedTHIS ACFT HAS HAD 2 NOSE GEAR TRUNNION ASSY CRACKED AT THE BOTTOM OF THE TRUNNION. THE CRACKS ACCRUE AT THE PART THAT THE SHIMMY DAMPNER ATTACHES TO THE TRUNNION AND TUBE ASSY.Sep 28, 2011 · N3892T · Piper PA28R180 · Nose/Tail Landing GearSDR 2010FA0000950Air Filter · debondedFOUND AIRFILTER ELEMENT TO HAVE SEPARATED AT GLUED SEAM, LEADING TO INJESTION OF UNFILTERED AIR FOR AN UNKNOWN LENGTH OF TIME.Sep 7, 2010 · N55460 · Piper PA28R200 · Engine Air Intake SystemSDR 2009FA0000816Retainer · disconnectedLT NOSE GEAR DOOR WOULD NOT OPEN TO LET THE NOSE GEAR COME DOWN. AFTER LANDING WITH THE NOSE GEAR UP, FOUND THAT THE LINKAGE CAME OFF IN FLIGHT AND JAMMED THE DOOR CLOSED. AFTER REMOVING AN INSP COVER, WAS ABLE TO FREE THE LINKAGE AND DROP THE NOSE GEAR WHILOct 8, 2009 · N2084D · Amtr VELOCITY · Landing Gear Door Retract SectionSDR 2009FA0000361Mount · corrodedENGINE MOUNT SHOWED PIN HOLES ON LOWER OUTER TUBE. REMOVED PAINT AND FOUND CORROSION. REPAIRED 13 TUBES. (K)May 1, 2009 · N5042T · Piper PA28R200 · Engine Mount SectionSDR 2009FA0000052Line · fracturedOIL LINE FRACTURED (1) INCH FROM FITTING IN FRONT OF CRANKCASE CAUSING LOSS OF OIL AND OIL PRESSURE. AS A RESULT OF MALFUNCTION, GOVERNOR HAD TO BE OVERHAULED, PROP FLUSHED AND RESEALED; ENGINE HAD TO BE REMOVED FROM SERVICE. (K)Jan 27, 2009 · N404SE · Piper PA28R200 · Reciprocating Engine Oil SystemSDR 2008FA0000559Drive Shaft · brokenDISTRIBUTOR (POINT CAM SHAFT BROKE FLUSH WITH UPPER MAG GEAR INNER RACE CAUSING TOTAL MAG FAILURE. PART WAS RETURNED TO OWNER. (K)Aug 10, 2008 · N2952R · Piper PA28R200 · Magneto/DistributorSDR 2007FA0001057Booster · shortedPILOT REPORTED ROUGH ENGINE; IGNITION SYSTEM TROUBLESHOOT FOUND START MAGNETO STARTER BOOSTER INTERNALLY SHORTED, GROUNDING MAGNETO P-LEAD CAUSING MAGNETO FAILURE. REMEDIED BY REMOVING START FROM AIRCRAFT AND MAGNETO OPERATING NORMALLY. (K)Nov 27, 2007 · N1473T · Piper PA28R200 · Magneto/DistributorSDR CA070327006Distributor Blk · unserviceable(CAN) DISTURBER BLOCK CENTER BUSHING WAS LOOSE IN THE PLASTIC MOLDING. (TC NR 20070327006)Mar 23, 2007 · Piper PA28R200 · Magneto/DistributorSDR CA070308001Float · worn(CAN) HOLE IN FLOAT WAS EXTREMELY WORN AND FLOAT FELL OFF. (TC NR 20070308001)Mar 2, 2007 · Piper PA28R200 · Fuel Quantity SensorSDR 2006FA0001010Rod End · brokenROD END BROKE AT POINT OF ATTACHMENT ON SERVO ARM. APPEARS BOLT MAY HAVE BEEN OVER TORQUED AT SOME POINT WHICH CAUSED A STRESS CRACK AND FAILURE OF BOLT AT POINT OF ATTACHMENT. TORQUE BOLT AT TIME OF INSTALLATION. (K)Sep 13, 2006 · N55068 · Piper PA28R200 · Standard Practices/StructuresSDR CA060612004Powerpack · failedHYDRAULIC POWER PACK BRUSHES FAILED, PART REPLACED.Jun 9, 2006 · Piper PA28R200 · Hydraulic System, MainSDR 2006FA0000495Oil Filter · leakingPILOT REPORTED OIL SPOTS ON HANGAR FLOOR. ENGINE WAS WASHED AND GROUND RUN FOR LEAK CHECK. INSPECTED ENGINE AFTER ENGINE RUN AND FOUND OIL ON BOTTOM SIDE OF OIL FILTER. FURTHER INSPECTION OF THE OIL LEAK REVEALED THAT THE OIL WAS LEAKING FROM THE HEX NUT ONMay 9, 2006 · N1663H · Piper PA28R201 · Reciprocating Engine Oil SystemSDR 2006FA0000431Pressure Switch · corrodedLANDING GEAR FAILED TO RETRACT IN FLIGHT. PLACING THE AC ON JACKS, THE LANDING GEAR FAILED TO COMPLETELY RETRACT. BY PLACING A JUMPER WIRE BYPASSING THE HYDRAULIC PRESSURE SWITCH THE LANDING GEAR WORKED NORMALLY. AFTER REMOVING THE PRESSURE SWITCH, CORROSIOApr 18, 2006 · N4967T · Piper PA28R200 · Landing Gear Position and WarningSDR CA051230004Spar · crackedWING MAIN SPAR EXTRUSION CRACKED AT MAIN LANDING GEAR SIDESTAY SUPPORT BRACKETS, LT AND RT SIDES. CRACKS RUN SPANWISE IN FILLET RADIUS AND IN WEB. TWO CRACKS VISIBLE IN EACH SIDE, LONGEST CRACK IS ABOUT 1.25" LONG. CRACKS EXTEND THROUGH FULL THICKNESS OF THDec 30, 2005 · Piper PA28R200 · Wing SparSDR AU510001451Screw · broken(AUS) ENGINE COWL SUPPORT BRACKET ATTACHMENT SCREW BROKEN ALLOWING SUPPORT BRACKET TO INTERFERE WITH THE NOSE LANDING GEAR DOWN MICROSWITCH STRIKER PLATE.(OTHER CAUSE: MATERIAL ) (CASA# 510001451)Dec 12, 2005 · Piper PA28RT201 · Engine Cowling SystemSDR CA051117007Distributor Gear · broken(CAN) MAGNETO FAILED SHORTLY AFTER TBO. (80 HOURS), DAMAGING THE DISTRIBUTOR GEAR.Nov 16, 2005 · Piper PA28R200 · Magneto/DistributorSDR CA051104015Stud · broken(CAN) 7 OF THE 8 STUDS ON NR 2 CYL BROKE ALLOWING THE CYL TO SHIFT CAUSING A VIBRATION. 5 MIN AFTER TAKEOFF THE PILOT NOTED A VIBRATION AND RETURNED FOR A NORMAL LANDING. INSPECTION OF THE LOG BOOK IT WAS NOTED THAT NR2 CYL HAD BEEN REMOVED 375 HRS PRIOR BY TOct 27, 2005 · Piper PA28R200 · Reciprocating Engine Power SectionSDR CA050829004Crankcase · cracked(CAN) ON INSPECTION, CHECKING FOR OIL LEAK, A CRACK IN THE CRANKCASE WAS FOUND. FRONT LT SIDE FORWARD OF NR 2 CYLINDER.Aug 23, 2005 · Piper PA28R200 · Reciprocating Engine Power SectionSDR 2005FA0000861Drive Gear · failedBENDIX DRIVE GEAR COMES APART DAMAGING RING GEAR SUPPLIER. (NOT MFG) STATED THIS WAS A COMMON PROBLEM. SECOND INSTANCE FOR THIS AIRCRAFT. (K)Jun 10, 2005 · N4583T · Piper PA28R200 · Engine StarterSDR 2005FA0000862Drive Gear · damagedBENDIX DRIVE GEAR COMES APART DAMAGING RING GEAR SUPPLIER (NOT MFG) STATED THIS WAS A COMMON PROBLEM. (K)Jun 10, 2005 · N55003 · Piper PA28R200 · Engine StarterSDR ZB0R200500002Starter · brokenON START, PILOT HEARD GRINDING NOISE. ABORTED START PROCEDURE AND PERFORMED VISUAL INSP OF VISIBLE STARTER COMPONENTS. FOUND STARTER BENDIX SEVERELY DAMAGED. MAINT INSPECTION REVEALED DAMAGE TO STARTER RING GEAR. BOTH COMPONENTS (GEAR AND STARTER) REPLACED. NOApr 25, 2005 · N15143 · Piper PA28R200 · Engine StarterSDR 2005FA0000579Rib · crackedDURING A 100HR. INSPECTION, A SMALL CRACK WAS FOUND IN THE RT. NOSE RIB PN-62021-005 AND -004. A MORE THOROUGH INSPECTION REVEALED THAT AN ADDITIONAL CRACK, MUCH LARGER (ABOUT 4 INCES LONG), WAS FOUND ON THE RIB PN-78475-009 AND -008. THESE RIBS ARE INCLUDED IMar 20, 2005 · N705ER · Piper PA28R201 · Wing, Rib/BulkheadSDR 2005FA0000202Spool · misinstalledGOVERNOR SENT FOR REPAIR DUE TO RPM CONTROL ISSUES AND A HISTORY OF LEAKING. DURING DISASSEMBLY, THE PILOT SPOOL SHAFT THREADS WERE FOUND DAMAGED. IT WAS DISCOVERED THAT AT THE PREVIOUS ASSY OF THIS PART, A FINE THREADED B3808-4 NUT WAS USED IN PLACE OF THE Jan 27, 2005 · N55696 · Piper PA28R200 · Propeller GovernorSDR 2005FA0000167Stud · failed(4) EA DECK STUDS ON NR 2 CYLINDER, FAILED.Oct 26, 2004 · N33129 · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR 2004FA0000761Stud · failedNR 2 CYLINDER STUD, 8 O CLOCK POSITION, FAILED.Aug 11, 2004 · N4509X · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR 2004FA0000747Sump · corrodedOWNER HAD OIL LEAK, UPON INSPECTION, FOUND OIL DRIPPING FROM OIL SUMP FWD OF RT INTAKE PORT. REMOVED OIL SUMP, FOUND AREA APPROX. 2.5 INCHES IN DIA. PITTED AND CORRODED. ONE AREA HAD PITTED THROUGH AND LEAKED. ENTIRE AREA WAS CLOSE TO PITTING THROUGH. IAWJun 28, 2004 · N2850T · Piper PA28R200 · Reciprocating Engine Oil SystemSDR AUS20040202Spar · corroded(AUS) WING SPAR CORRODED. FOUND FOLLOWING REMOVAL OF FUEL TANK FOR STRUCTURAL DEFECT REPAIR. CORROSION WAS SEVERE ENOUGH TO HAVE COMPROMISED STRUCTURAL INTEGRITY.Mar 16, 2004 · Piper PA28R200 · Wing SparSDR CA040130008Trunnion · cracked(CAN) CRACK EMANATING FROM TOP OF WEB JUST RT OF CENTER STRUT HOUSING. NO REPORT OF HARD LANDING OR ABUSE.Jan 27, 2004 · Piper PA28R200 · Nose/Tail Landing GearSDR GZQ2004F00002Case Half · crackedA CRACK WAS FOUND ON THE LT CASE HALF TOP FORWARD SECTION.Jan 1, 2004 · N41585 · Piper PA28R200 · Engine (Reciprocating)SDR AUS20030459Bushing · failed(AUS) NR 4 CYLINDER CONNECTING ROD FAILED. ENGINE SEVERELY DAMAGED. METAL CONTAMINATION OF OIL SYSTEM. INVESTIGATION FOUND CONNECTING ROD LITTLE END BUSH FAILED. ALL OTHER LITTLE END BUSHES EXHIBITED SIGNS OF CRACKING AND UNUSUAL WEAR PATTERNS.Apr 22, 2003 · Piper PA28R200 · Reciprocating Engine Power SectionSDR 2003FA0000380Rib · crackedTHE LT AND RT FORWARD TRUNNION FITTING ASSEMBLIES WERE REMOVED TO COMPLY WITH MFG (FORWARD SIDEBRACE STUD). WHILE THE FITTINGS WERE REMOVED IT WAS NOTICED THAT THE LEFT AND RIGHT WING RIBS MFG (PN 7847504 AND 05) WERE CRACKED AT THE FORWARD OUTBOARD FLANGE OFeb 17, 2003 · N56018 · Piper PA28R200 · Wing, Rib/BulkheadSDR 2002FA0001220Bolt · brokenNR 3 CYLINDER CONNECTING ROD BOLT BROKE. ENGINE WAS DESTROYED. PROBABLE CAUSE, POSSIBLE OVER-TORQUED.Aug 9, 2002 · N32481 · Piper PA28R200 · Reciprocating Engine Cylinder SectionSDR AUS20020667Brushes · loose(AUS) LANDING GEAR MOTOR BRUSHES ADRIFT IN BRUSH HOLDER. MOTOR FAILED.May 3, 2002 · Piper PA28R200 · Landing Gear ActuatorSDR CA020227011Frame · cracked(CAN) BOTH LT AND RT UPPER FORWARD WELD JOINTS FAILED ON SEAT FRAME ASSEMBLY. THE SEAT ASSEMBLY IS VERY DIFFICULT TO INSPECT IN THIS AREA AS IT IS COVERED WITH UPHOLSTERY.Feb 22, 2002 · Piper PA28R200 · Flight Compartment EquipmentSDR CA020227013Frame · cracked(CAN) BOTH LT AND RT UPPER FORWARD WELD JOINTS FAILED ON SEAT FRAME ASSEMBLY.THE SEAT ASSEMBLY IS VERY DIFFICULT TO INSPECT IN THIS AREA AS IT IS COVERED WITH UPHOLSTERY.Feb 22, 2002 · Piper PA28R200 · Passenger Compartment EquipmentSDR CA030107010Trunnion · cracked(CAN) DURING ANNUAL INSPECTION, NOSE GEAR TRUNION FOUND CRACKED AROUND UPPER RT ATTACHMENT.Jan 20, 2002 · Piper PA28R200 · Nose/Tail Landing GearSDR 2001FA0000193Crankcase · crackedAT INSPECTION AN AREA OF OIL IS NOTICED BEHIND PROP- IT APPEARS TO LOOK LIKE THE SPLIT CASE SEAM IS LEAKING. CLEAN AREA AND USE NDT DEVELOPER. RUN-UP PLANE AND CRACK APPEARS. THERE ARE SEVERAL STYLES OF CASE FOR THIS ENGINE. BUT ON A CERTAIN STYLE SEEMS TOJul 30, 2001 · N9235G · Piper PA28R201 · Reciprocating Engine Power Section
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