Eci O360A1A

Service difficulty reports · 103

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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 = 'O360A1A'
  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 2023FA0000625Cylinder · separatedCYL €¢3 DEVELOPED/, CRACK IN THE CYLINDER HEAD BETWEEN COOLING FINS IIPPROXIMATEL Y 1 625 INCHED ABOVE LOWEST FINE AT HE/ID/ 81\RREL ATTACHMENT. IOCIITED IN LOWER CORNEER EDGE OF CLINDER HEAD ON INTAKE VALVE SIDE. PILOT NOFLCED CYL HEAD !HIP RISINC, TO APPRJun 19, 2023 · N2838L · Cessna 172H · Reciprocating Engine Cylinder SectionSDR 2018FA0000176Exhaust Stack · blockedA COMPLETE EXHAUST SYSTEM REPAIR AND OVERHAUL. REINSTALLED ON AIRCRAFT. PERFORMED A RUN-UP OF ENGINE AND EXPERIENCED INCREASED VIBRATION LEVELS AND LOW EGT READINGS ON THE NR 3 CYLINDER. AN AUDIBLE, METALLIC-SOUNDING PING COULD BE HEARD IN THE CABIN AND FROM Jun 13, 2018 · N5832P · Piper PA24180 · Engine Collector/Tailpipe/NozzleSDR 2018FA0000122Turnbuckle · separatedAIRCRAFT LOST AILERON CONTROL IN FLIGHT, DECLARED EMERGENCY AND LANDED. AFTER SHUTDOWN THE SEPARATED CABLE FOR LEFT AILERON FROM TURNBUCKLE SWEDGED FITTING UNDER RIGHT SIDE OF COCKPIT PANEL WAS DISCOVERED. AIRCRAFT GROUNDED.Mar 31, 2018 · N5910R · Cessna 172G · Aileron Control SystemSDR 2017FA0000047Spark Plug · departedDURING CRUISE , THE NR 3 CYLINDER, LOWER SPARK PLUG, DEPARTED THE ENGINE, CAUSING A SUBSTANTIAL LOSS OF POWER. THE SUSPECT SPARK PLUG WAS RECOVERED, AND WAS FOUND TO HAVE THE HELICOIL FROM THE CYLINDER STILL FIRMLY ATTACHED.Feb 7, 2017 · N6260Z · Piper PA25 · Spark Plug/IgniterSDR 2015FA0000305B-Nut · looseENGINE FIRE DURING START UP. FIRE EXTINGUISHED ON GROUND. INSPECTED ENGINE COMPARTMENT AFTER FIRE AND FOUND THAT FLEXIBLE FUEL LINE FROM FUEL PUMP TO CARBURETOR HAD COME LOOSE AT THE B-NUT ON ENGINE DRIVEN FUEL PUMP AND WAS LEAKING FUEL.Jun 30, 2015 · N6194J · Piper PA28181 · Engine Fuel DistributionSDR 2012FA0000698Exhaust Stack · erodedTHE PILOT MADE AN INTENTIONAL GEAR-UP LDG AFTER SEVERAL UNSUCCESSFUL ATTEMPTS TO FULLY EXTEND THE LANDING GEAR. FOLLOW-UP INSPECTION OF THE ACFT REVEALED THAT A SECTION OF THE LEFT-FRONT EXHAUST STACK ASSY HAD FAILED AND SEPARATED FROM THE ENGINE EXHAUST SYS,Sep 23, 2012 · N7059P · Piper PA24 · Engine Collector/Tailpipe/NozzleSDR CA120711007Crankshaft · failed(CAN) CUSTOMER BROUGHT ENGINE TO US AFTER 40HRS SINCE MAJOR O/H. THE CUSTOMER WAS SOLD A CRANKSHAFT AND CONNECTING RODS, FROM AN ENGINE SHOP. THE ENGINE WAS DECLARED TO BE AN O/H AND INSTALLED HIS ENGINE. AT 38.1 HRS SINCE O/H THE CUSTOMERS ENGINE STOPPED DUJun 22, 2012 · Reciprocating Engine Power SectionSDR CA120104011Step · cracked(CAN) RIGHT PASSENGER STEP CRACKED BETWEEN ARM AND PLATE ON THE LOWER SURFACE ADJACENT TO THE WELD. CRACK LENGTH APPROXIMATELY 1 INCH. TOTAL TIME ON PART 202 HOURS.Dec 30, 2011 · Amtr RV6A · Fuselage Main, StructureSDR CA110919002Cable · shorted(CAN) THE CABLE THAT RUNS FROM THE ELT REMOTE SWITCH TO THE ELT HAD A SHORT IN IT. THIS WAS CAUSING THE ELT TO ACTIVATE IN FLIGHT AND OR ON THE GROUND.Sep 6, 2011 · Piper PA28151 · Equipment/Furnishings WiringSDR 2010FA0000386Carburetor · defectivePARTIAL LOSS OF POWER ON DEPARTURE AT 1,000` AGL. AFTER RETURNING TO LAND, ENGINE ROUGHNESS INCREASED. DURING TAXI IN, MAX ATTAINABLE RPM WAS 900. MECHANIC TROUBLESHOT AND DETERMINED THE PROBLEM TO BE FUEL STARVATION. FUEL SUPLY TO THE CARBURETOR WAS NORMApr 16, 2010 · N68RS · Amtr RV7A · Fuel Control/Reciprocating EnginesSDR CA090706007B-Nut · loose(CAN) IN FLIGHT, PILOT NOTICED THE OIL PRESSURE GAUGE FLUCTUATING. PILOT TURNED AROUND AND RETURNED TO DEPARTURE. WHILE RETURNING, OIL PRESSURE DROPPED TO 0 AND OIL TEMP CLIMBED TO RED LINE. PILOT SHUTDOWN ENG AND GLIDED BACK TO AIRPORT. ON TROUBLESHOOTING, Jul 5, 2009 · Cessna 172M · Reciprocating Engine Oil SystemSDR 2008FA0000535Downlock · wornLANDING GEAR LEVER BECAME DISENGAGED FROM THE DOWN LOCK LATCHING ASSY ON THE PILOT`S LOWER CENTER INSTRUMENT PANEL. AC WAS ON THE GROUND DURING LANDING ROLLOUT. THIS ALLOWED GEAR TO COLLAPSE. SB M20-88B, 5/10/94. (K)Jul 30, 2008 · N74542 · Mooney M20B · Landing Gear SelectorSDR 2008FA0000547Downlock · wornLANDING GEAR LEVER BECAME DISENGAGED FROM THE DOWNLOCK LATCHING ASSY ON THE PILOT`S LOWER CENTER INSTRUMENT PANEL. AC WAS ON THE GROUND DURING LANDING ROLLOUT. THIS ALLOWED GEAR TO COLLAPSE, SB M20-88B, 5-10-94. (K)Jun 28, 2008 · N74542 · Mooney M20B · Landing Gear Position and WarningSDR 2008FA0000105Fitting · brokenPILOT STATED THAT HE PERFORMED AN OFF AIRPORT LANDING ALONG A BEACH WHILE HUNTING. UPON LANDING, THE UPPER RT MLG CABANE FITTING BROKE. THE LANDING GEAR SAFETY CABLES PREVENTED A TOTAL GEAR COLLAPSE. (K)Dec 4, 2007 · N723C · Piper PA18 · Main Landing Gear Strut/Axle/TruckSDR 2007FA0001084Nose Rib · crackedIN-FLIGHT, PILOT LOWERED FLAPS AND AIRCRAFT STARTED TO ROLL TO THE RT. PILOT NOTICED RT FLAP WAS RETRACTED, HE THEN RETRACTED FLAP HANDLE. AIRCRAFT LANDED SAFELY, WITHOUT INCIDENT. UPON INSPECTION, FOUND RT FLAP ROD ATTACH BRACKET BROKEN AND FLAP NOSE RIB NNov 9, 2007 · N9349Y · Beech B95 · Trailing Edge FlapsSDR 2007FA0001010Pipe · failedLEADING EDGE EXHAUST SYSTEM INSTALLED BY STC SA02200AK FAILED AT THE SAIL PIPE TO MUFFLER WELD. SYSTEM HAS 36 HOURS SINCE NEW. (K)Nov 1, 2007 · N7066B · Piper PA18150 · Engine Collector/Tailpipe/NozzleSDR CA070419005Bracket · cracked(CAN) DURING THE ANNUAL INSPECTION, BOTH RUDDER HINGE BRACKETS WERE FOUND TO BE CRACKED. RUDDER WAS REMOVED AND REINSTALLED AFTER REPAIRS. PN 0531018-1 AND 0531018-2 WERE REPLACED WITH NEW IAW THE MM. (TC NR 20070419005)Apr 12, 2007 · Cessna 172D · Rudder StructureSDR CA070110003Torque Link · cracked(CAN) PRIOR TO INSTALLATION ON AIRCRAFT, NOSE GEAR SHOCK STRUT ASSEMBLY WAS THOROUGHLY INSPECTED. SEVERAL CRACKS WERE FOUND ON UPPER TORQUE LINK. NEW MFG PART WAS INSTALLED. (TC NR 20070110003)Dec 20, 2006 · Cessna 172D · Nose/Tail Landing Gear Strut/AxleSDR 2006FA0000260Oil Cooler · splitDURING ROUTINE RUN-UP FOLLOWING AN OIL CHANGE, AN IMMEDIATE EXPULSION OF SEVERAL QUARTS OF OIL OCCURRED IN SECONDS. (K)Mar 6, 2006 · N5496H · Cessna 172M · Engine Oil CoolerSDR AU510001642Piston Ring · delaminated(AUS) ENGINE CYLINDERS (4OFF) HAD TOP PISTON RINGS DELAMINATING. PLASMA FACE SECTION COMING AWAY FROM BASE MATERIAL. ALL 4 CYLINDERS ALSO HAD EXCESSIVELY WORN EXHAUST VALVE GUIDES AND 2 EXHAUST VALVES REQUIRED REPLACEMENT. (CASA NR 510001642)Dec 12, 2005 · Socata TB10TOBAGO · Reciprocating Engine Power SectionSDR AU510001679Piston Ring · delaminatedTOP COMPRESSION RINGS ON ALL PISTONS DELAMINATING.Dec 12, 2005 · Socata TB10TOBAGO · Reciprocating Engine Power SectionSDR AU510001711Piston Ring · deterioratedNR 2 CYLINDER PISTON TOP COMPRESSION RING PLASMA COATING DELAMINATING. TOP RINGS ON ALL OTHER PISTONS SHOWING SIGNS OF DELAMINATION BEGINNING TO OCCUR.Dec 12, 2005 · Socata TB10TOBAGO · Reciprocating Engine Power SectionSDR AU510001823Hinge · corrodedFOUND TOP RUDDER HINGE CORRODED.Dec 12, 2005 · Socata TB10TOBAGO · Rudder StructureSDR AU510001824Mount · crackedENGINE MOUNT CRACKED. FOUND DURING INSPECTION IAW AD/TB10/8 AND TBSB NO 16/1.Dec 12, 2005 · Socata TB10TOBAGO · Engine Mount SectionSDR AU510001825Hinge · corrodedRT STABILATOR HINGE CORRODED, AD/SB DESC: CASA SCHEDULE 5.Dec 12, 2005 · Socata TB10TOBAGO · Elevator StructureSDR 2005FA0001597Engine · malfunctionedFORCED LANDING, DUE TO ENG FAIL DURING TAKEOFF. DAMAGE TO AC INCLUDED LT MLG WAS BROKEN, LT WING TIP SKIN DENTED, LWR ENG COWLING DAMAGED. DAMAGE TO AC WAS CONSIDERED TO BE MINOR. INSP OF AC REVEALED LT FUEL TANK WAS FULL OF FUEL; FUEL QTY IN RT FUEL TANK CDec 10, 2005 · N20EA · Amtr RV8 · Engine (Reciprocating)SDR CA050121005Fitting · cracked(CAN) DURING ANNUAL INSP, IT WAS NOTICED THAT AC DID NOT COMPLY WITH REQUIREMENTS OF AD98-10-12 WITH REF TO SB78 HORIZONTAL STABILIZER INSP AND REWORK. AD98-10-12 WAS SIGNED OUT IN THE TECH RECORDS ON SEPT 1,1998 AT 1683.22 TT. REMOVAL OF FITTINGS REVEALED P/NNov 25, 2004 · Conaer LA4 · Horizontal Stabilizer StructureSDR 2004FA0000782Cap · cloggedPILOT EXPERIENCED FUEL INTERRUPTION TO ENGINE WHILE ENROUTE. SWITCHED FUEL TANKS AND ENGINE QUIT. MADE EMERGENCY LANDING. REMOVED AC FROM FIELD TO LOCAL AIRPORT (N75). DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FUEL WITH FUEL CAPS ON THAT DRAININGSep 23, 2004 · N8214Y · Piper PA28181 · Fuel StorageSDR 2004FA0000783Cap · cloggedPILOT EXPERIENCED FUEL INTERRUPTION TO ENGINE WHILE ENROUTE. SWITCHED FUEL TANKS AND ENGINE QUIT. MADE EMERGENCY LANDING. NO INJURIES OR DAMAGE TO AIRCRAFT. REMOVED AC FROM FIELD TO LOCAL AIRPORT (N75). DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FSep 23, 2004 · N8214Y · Cessna 172 · Fuel StorageSDR 2004FA0000744Cap · cloggedPILOT EXPERIENCED FUEL INTERUPTION. MADE EMERGENCY LANDING IN SOYBEAN FIELD. NO INJURIES OR DAMAGE TO AC. REMOVED AC FROM FIELD TO LOCAL AIRPORT. DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FUEL WITH FUEL CAPS ON THAT DRAINING FUEL WAS SLOW. REMOVSep 23, 2004 · N8214X · Cessna 172 · Fuel StorageSDR 2004FA0000689Shaft · failedTAIL ROTOR DRIVE FROM 90 GEARBOX TO TAIL ROTOR GEARBOX FAIL AT ATTACHING POINT IN TAIL ROTOR GEARBOX. BY THE DISCOLORATION OF THE BREAK IT APPEARS THAT IT HAD PARTIALLY CRACKED PRIOR TO TOTAL FAILURE. THIS CAUSED LOST OF DIRECTIONAL CONTROL OF AIRCRAFT. THEJun 23, 2004 · N9023Z · Hynes B2B · Tail Rotor GearboxSDR CA040507001Actuator · failedCAPT REPORTED THE PITCH CONTROL STICKING ( HARD POINT FEELING ) AFTER AP DISCONNECTION. CPT HAD TO PULL THE CONTROL COLUMN TO RECOVER THE FLIGHT CONTROL. PITCH SERVO ACTUATOR WAS REPLACED.Mar 29, 2004 · Cndair CL6002B19 · Autopilot Main ServoSDR AUS20040142Bearing · failed(AUS) MAGNETO DRIVE SHAFT OUTER BEARING COMPLETELY DESTROYED. BEARING HAD BEEN RUNNING DRY FOR SOME TIME. SUSPECT MAGNETO ASSEMBLED WITHOUT GREASE IN THE BEARING. PERSONNEL/MAINTENANCE ERROR.Mar 2, 2004 · Socata TB10TOBAGO · Magneto/DistributorSDR AUS20030967Spar · corroded(AUS) LT UPPER AFT REAR SPAR WEB CONTAINED LIGHT EXFOLIATION CORROSIONIN AREA ADJACENT TO MAIN LANDING GEAR. FOUND DURING INVESTIGATION FOLLOWING CORROSION IN RT WING SPAR. SEE MDR 03/0900.Sep 17, 2003 · Socata TB10TOBAGO · Wing SparSDR AUS20030900Spar · corroded(AUS) RT WING MAIN SPAR AFT LOWER WEB CONTAINED EXFOLIATION CORROSION. CORROSION WAS MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR LEG.Sep 8, 2003 · Socata TB10TOBAGO · Wing SparSDR AUS20030901Spar · corroded(AUS) LT AND RT WING MAIN SPAR AFT LOWER WEBS CONTAINED EXFOLIATION CORROSION. CORROSION MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR.Sep 8, 2003 · Socata TB10TOBAGO · Wing SparSDR AUS20030844Spar · corroded(AUS) LT AND RT WING MAIN SPARS CONTAINED SEVERE EXFOLIATION CORROSION.Aug 19, 2003 · Socata TB10TOBAGO · Wing SparSDR AUS20030835Spar · corroded(AUS) RT WING MAIN SPAR UPPER CAP CONTAINED CORROSION ON THE AFT FACE. RT WING LEADING EDGE INTERCOSTAL CONTAINED CORROSION ON THE LOWER FLANGE. FOLLOWING REMOVAL OF WINGS FOR REPAIR FURTHER CORROSION WAS FOUND ON THE TOP SURFACE OF THE LT AND RT MAIN SPAR UPPJul 24, 2003 · Socata TB10TOBAGO · Wing SparSDR CA030729011Screw · loose(CAN) SCREWS HOLDING FLOAT BOWL TO CARBURETOR HOUSING. ALL SCREWS LOCKED BUT ALL LOOSE IN HOUSING CAUSING CHAFING BETWEEN BOWL, GASKET HOUSING WITH A 1/16 INCHES GAP AND ALL AROUND. DISCOVERED ON ANNUAL INSPECTION.Jul 14, 2003 · Piper PA24180 · Fuel Control/Reciprocating EnginesSDR AUS20030833Bracket · corroded(AUS) RUDDER LOWER HINGE SUPPORT BRACKET CONTAINED EXFOLIATION CORROSION. FOUND DURING INSPECTION IAW AD TB10 31.May 25, 2003 · Socata TB10TOBAGO · Rudder StructureSDR AUS20030832Fitting · corroded(AUS) REAR SEAT BELT OUTBOARD FITTINGS CONTAINED EXFOLIATION CORROSION.May 23, 2003 · Socata TB10TOBAGO · Flight Compartment EquipmentSDR CA031021005Spar · broken(CAN) DISCOVERED A BREAK IN THE STABILIZER SPAR DURING AN ANNUAL INSPECTION.May 16, 2003 · Cessna 175 · Horizontal Stabilizer, Spar/RibSDR 2003FA0000685Fork · crackedPITCH CHANGE FORK WAS CRACKED, POSSIBLY DUE TO EXCESSIVE ENGINE VIBRATION. PROPELLER HAD 200 HOURS SINCE LAST OVERHAUL. CUSTOMER WAS ADVISED TO HAVE PROPELLER, DYNAMICALLY BALANCED TO AVOID ANY FURTHER DAMAGE TO PROPELLER ASSEMBLY.May 5, 2003 · Mooney M20C · Propeller Controlling SystemSDR 2003FA0000156Governor · malfunctionedPROPELLER WOULD CYCLE NORMALLY DURING RUN UP. AFTER TAKE OFF THE PROP WOULD BECOME UNCONTROLLABLE. RMP ONLY CONTROLLABLE BY THROTTLE, NOT PROPELLER CONTROL. REMOVAL AND DISASSEMBLY OF PROP GOVERNOR REVEALED THAT ALLEN SCREW HAD BACKED OUT OF REAR OF UNIT AND WFeb 17, 2003 · N468JL · Amtr RV8 · Propeller GovernorSDR 2003FA0000175Indicator · inoperativeALTIMETER PURCHASED NEW. MAY 5, 2001 MANUFACTURE DATE. FAILED TO PASS FRICTION PORTION OF PITOT/STATIC/XPDR. BIANNUAL CHECK. MFG CONTACTED AND IS UNAWARE OF ANY PROBLEMS WITH THIS MODEL BUT TECHNICIAN DOING STATIC TEST NOTES SEVERAL LIKE IT HAVE FAILED SAMJan 24, 2003 · N751MB · Amtr RV8A · Altimeter, Barometric/EncoderSDR AUS20021187Pipe · fractured(AUS) PROPELLER GOVERNOR EXTERNAL OIL PIPE FAILED AT CONNECTION TO THEGOVERNOR.Oct 16, 2002 · Socata TB10TOBAGO · Propeller Controlling SystemSDR CA020916005Wire Rope · broken(CAN) ON TAKEOFF RUN, AT APPROXIMATELY 2 FT OFF THE WATER, A/C SETTLED BACK DOWN DUE TO UNSTABLE AIR. A NOISE WAS HEARD AND THE A/C BECAME VERY UNSTABLE. ABORTED TAKEOFF. AS THE A/C SLOWED DOWN & THE LIFT DISSIPATED, THE LT WING SUDDENLY DIPPED DOWN AND CAug 2, 2002 · Cessna 172D · Wheel/Ski/FloatSDR CA020610003Line · worn(CAN) - FUEL LINE FROM UNION TO FIREWALL (STRAINER) FOUND RUBBING ON CO-PILOT STEERING TORQUE TUBE AND STEERING ARM. FUEL LINE HAD A SMALL PIN HOLE AND A SMALL AMOUNT OF FUEL WAS LEAKING. - NEW LINE WAS MANUFACTURED AND ROUTED AWAY FROM STEERING ARM.May 31, 2002 · Cessna 172K · Aircraft Fuel Distribution SystemSDR AUS20020429Frame · cracked(AUS) FUSELAGE FRAME NR 9 CRACKED AT BOTH TOP CORNERS.Apr 26, 2002 · Socata TB10TOBAGO · Fuselage Main, FrameSDR CA020205002Cylinder · failed(CAN) A/C C-2 SKIMMERS, BOTH UTILIZE COLONIAL STYLE MAIN UNDER CARRIAGE OLEOS. ONE OLEO PER A/C CAME APART.THE MAIN GEAR OLEOS ARE CRACKING AT LOWER END CAP TO CYLINDER (CASING) ATTACH BOLTS. WHEN THIS OCCURS, BEFORE LONG END CAP DISLODGES FROM OLEO CAUSING GEJan 28, 2002 · Conaer C2 · Main Landing Gear Strut/Axle/Truck
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