Lycoming IO-360-M1A
Service difficulty reports · 128
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 = 'IO360M1A' 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 = 'IO360M1A' 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 U43R2010AF0000193Heat Exchanger · brokenIAW POWER FLOW SYS "CONTINUED AIRWORTHINESS INSTRUCTIONS" (DATED 07/22/2008) PARAGRAPH 7.0 STATES "THE EXHAUST SYS MUST BE THOROUGHLY INSPECTED, ESPECIALLY WITHIN THE HEAT EXCHANGER SECTION" DURING A 100 HR INSP OF THIS AIRPLANE A CRACK WAS FOUND IN THE CHAINSDR CA100628001Fuel Tank · crackedFUEL TANK DEVELOPED A SMALL CRACK EMANATING FROM A SMALL WELD.SDR U43R2010AF0000192Starter · failedAIRPLANE HAD FLOWN 3 TIMES ON THIS DAY, ON THE 4TH FLIGHT STARTER FAILED TO START. A CLICK NOISE COULD BE HEARD WHEN TURNING KEY FROM BOTH TO START. FLIGHT WAS ABORTED.SDR U43R2010AF0000191Starter · slow(U43R) WHILE ATTEMPTING TO START THE AIRPLANE, THE STARTER TURNED THE ENGINE VERY SLOWLY. THIS WAS TO BE THE 2ND FLIGHT OF THE DAY, THE AIRPLANE HAD THE PROPER VOLTAGE SUPPLIED TO THE STARTER. R & R THE STARTER, ACFT WAS RETURNED TO SERVICE.SDR U43R2010AF0000190Valve · stripped(U43R) DURING SCHEDULED INSP, A&P MECHANIC FOUND THAT THE ALTERNATE AIR VALVE CONTROL LINE WAS LOOSE. FURTHER INSP FOUND THAT THE "EYE" BOLT HAD STRIPPED THE THREADS IN THE VALVE BODY HSG. THE BODY HSG IS MADE FROM ALUMINUM, THE "EYE" BOLT FROM STEEL. THE "SDR U43R2010AF0000189Pump · failed2ND PREFLIGHT OF THE MORNING, CREW PREFORMED A FUNCTION CHECK OF THE ELECTRIC FUEL PUMP. INTERNAL FAILURE OF THE FUEL PUMP WAS THE CAUSE.SDR U43R2010FA0000188Starter · failedSTARTER HAD WORKED FOR 2 STARTS EARLIER IN THE DAY. THE 3RD FLIGHT ATTEMPT, THE STARTER DIDN'T WORK AT ALL. CHECKED CONNECTIONS THEY WERE TIGHT. HAD PLENTY OF VOLTAGE INDICATED. PROBLEM APPEARS TO BE IN THE STARTER. ITS UNDER WARRANTY RETURNED TO THE MFG. SDR U43R2010AF0000187Pump · failed(U43R) DURRING 1ST PRE-FLIGHT OF THE DAY. CREW PERFORMED A FUNCTION CHECK OF THE FUEL PUMP, NO INDICATION OF ANY OPERATION AT ALL ON THE MFD OR ANY SOUND OF OPERATION.SDR CA100531002Starter · intermittentPERIODICALLY STARTER WOULD NOT ENGAGE ON FIRST ATTEMPT. REMOVED FOR TROUBLESHOOTING PURPOSES, ACFT HAS HAD NO STARTING ISSUES SINCE INSTALL OF NEW STARTER.SDR U43R2010AF0000186Pump · failedSUBMITTED SDR FOR THIS TYPE OF FAILURE EARLIER AND IDENTIFIED THE SERIAL NR OF THIS PUMP THAT FAILED. THE PUMP FROM THE FACTORY WAS SN 9693, WHEN IT FAILED WE INSTALLED PUMP SN 9888A. THIS PUMP DURING THE 2ND PREFLIGHT WAS FOUND TO NOT PRODUCE ENOUGH PSI (10.7SDR NX4R00001Fuel Tank · crackedDURING A ROUTINE INSP, A FUEL STAIN WAS NOTICED IN THE LT AUX TANK AREA. THE TANK WAS REMOVED AND INSPECTED. THERE WERE CRACKS FOUND AT SEVERAL OF THE WELD POINTS WHERE AN INTERNAL BAFFLE IS WELDED TO THE BOTTOM PANEL OF THE TANK. A NEW TANK (PN-D60-2814-11-00SDR U43R2010AF0000185Pump · failed3ND FLIGHT OF THE DAY, DURING PRE-FLIGHT INSPECTION. CREW DID A FUNCTION CHECK OF THE ELECTRIC FUEL PUMP, IT WAS NOT EVEN MAKING SOUNDS.SDR 2010FA0000235Blade · crackedPAINT IS CRACKING PERPENDICULAR TO BLADE. LARGE CRACKS IN PAINT HAVE EXPOSED COMPOSITE LAYER.SDR 2010FA0000236Blade · crackedPAINT IS CRACKING PERPENDICULAR TO BLADE. LARGE CRACKS IN PAINT HAVE EXPOSED COMPOSITE LAYER.SDR 2010FA0000237Paint · crackedPAINT IS CRACKING PERPENDICULAR TO BLADE. LARGE CRACKS IN PAINT HAVE EXPOSED COMPOSITE LAYER.SDR 2010FA0000240Blade · peelingPAINT IS PEELING AND CRACKING PERPENDICULAR TO BLADE, EXPOSING COMPOSITE LAYER. THIS PROP WAS RECENTLY REPAIRED WITH THE NEWEST METHOD OF BLADE PAINTING APPROVED BY MFG.SDR 2010FA0000184Housing · damagedAFTER 150 HOURS ON ACFT DURING SCHEDULED MAINTENANCE THE FIRST ONE OF THE TYPE OF PROBLEM WAS FOUND. MECHANICS ARE FINDING THE ALTERNATE AIR VALVE BODY CONTROL CABLE (PN NR DAI-9076-00-04) LOOSE OR COMPLETELY DISCONNECTED AND HANGING NEXT TO THE PRIMARY/ALTERSDR 2010FA0000157Suppressor · blisteredSMELL OF SMOKE IN COCKPIT. REPLACED TRANSIENT VOLTAGE SUPPRESSOR.SDR CA100120004Rod · worn(CAN) THE DAMPER ASSY D41-3223-20-00G WAS DISASSEMBLED TO REPLACE WORN RUBBER ELEMENTS. IT WAS DISCOVERED THAT THE LOWER END OF THE DAMPER ROD THAT HOLDS THE ASSY TOGETHER HAD BEEN SEVERELY WORN AND WAS BEYOND LIMITS. IT APPEARS THAT THE LOWER DAMPER PLATE (DSDR CA100111004Rod · worn(CAN) THE DAMPER ASSEMBLY D41-3223-20-00G WAS DISASSEMBLED TO REPLACE WORN RUBBER ELEMENTS. IT WAS DISCOVERED THAT THE LOWER END OF THE DAMPER ROD THAT HOLDS THE ASSEMBLY TOGETHER HAD BEEN SEVERELY WORN AND WAS BEYOND LIMITS. IT APPEARS THAT THE LOWER DAMPERSDR CA091102005Strut · cracked(CAN) DURING PENETRANT INSP, IAW MANDATORY SB MSB40-046/3, A SMALL CRACK WAS FOUND IN RADIUS OF PIVOT AS SHOWN IN THE MSB. MSB POINTS TO FRONT SECTION OF RADIUS IN DIAGRAM, CRACK WAS FOUND ON REAR SIDE OF RADIUS. STRUT WAS REPLACED.SDR CA090901002Drive Gear · brokenENG START ATTEMPT FAILED WITH LOUD GRINDING SOUND. UPON VISUAL INSP, STARTER DRIVE GEAR HSG FOUND BROKEN. STARTER SUPPORT EAR SNAPPED OFF AS WELL.SDR 2010FA0000152Suppressor · failedSMOKE CAME OUT FROM UNDER THE INSTRUMENT PANEL. FOUND TRANSIENT VOLTAGE SUPPRESSOR FAILED.SDR CA090612003Housing · cracked(CAN) DURING 100 HOUR INSP, REAR BRG HSG ON LT MLG ASSY WAS DETERMINED TO BE CRACKED UNDER MOUNTING BOLT AT 1 O`CLOCK POSITION WHEN SEEN FROM AFT TO THE FRONT. BOLT WAS REMOVED AND IT WAS OBSERVED THAT THE BOLT SHANK WAS BADLY CORRODED AND SOME WEAR MARKS WERSDR CA090616007Housing · cracked(CAN) DURING 100 HOUR INSP BOTH LT AND RT MLG REAR BEARING HOUSING WERE FOUND CRACKED ALONG THE HOUSING MOUNTING BOLTS. PART IDENTIFIED IN IPC AS ITEM NR 110, CHAPTER 32-10 PAGE 588 THRU 594.SDR 2008FA0000861Starter · brokenSTARTER HOUSING BROKE AT FRONT CASTING BREAKING OFF FRONT MOTOR SHAFT SUPPORT BEARING WHICH ALLOWED STARTER SHAFT TO DROP DOWN PREVENTING POSITIVE ENGAGEMENT OF STARTER TO FLY WHEEL. CONVERSATION WITH AIRCRAFT MFG NOTED THIS IS NOT AN ISOLATED INCIDENT AND THSDR 2010FA0000151Suppressor · failedAFTER HOOKING UP GROUND POWER UNIT (24 VDC), BATTERY CIRCUIT TRANSIENT VOLTAGE SUPPRESSOR BLEW SMOKE AND LOUD POPPING SOUND.SDR CA081104003Bracket · broken(CAN) DURING A ROUTINE INSP, THE ALTERNATOR MOUNTING BRACKET WAS FOUND TO BE BROKEN ACROSS THE WIDTH OF THE BRACKET ADJACENT ONE OF THE MOUNTING HOLES. (REAR MOUNTING BOLT THAT IS USED TO ATTACH THE BRACKET TO THE ENGINE).
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