Lycoming IO-360-A1A

Service difficulty reports · 315

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 = 'IO360A1A'
  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 AU960930Block · failed(AUS) DURING INVESTIGATION OF A WRINKLE IN THE FABRIC COVERING ON THE TOP WING (INBOARD) TRAILING EDGE, THE DRAG/ANTI-DRAG WIRE REAR ATTACHMENT BLOCK AT REAR SPAR WAS FOUND BROKEN WHICH IN TURN CAUSED THE TRAILING EDGE TO CENTRE HOOP ATTACHMENT BLOCK TO FAILMay 14, 1996 · Amtr CHRISEAGLE2 · Wing Miscellaneous StructureSDR 96ZZZX1705Engine · seizedAIRCRAFT WAS IN LEVEL FLIGHT AT 13,500 FEET, HAD COMPLETE ENGINE FAILURE AND SEIZED WITH NO PRIOR WARNING. DECLARED EMERGENCY. GLIDED 17.2 NM BACK TO AIRPORT, LANDED WITHOUT FURTHER INCIDENT. NO DAMAGE TO AIRCRAFT AND NO INJURIES. ENGINE SCHEDULED TO BE REMar 15, 1996 · N1940Y · Mooney M20E · Engine (Reciprocating)SDR AU960526Wing · corroded(AUS) WING CENTRE SECTION SEVERELY CORRODED - THE FOLLOWING ITEMS NEEDED REPAIR: 1.PNO 210022-091 - WING RIB INBOARD FUSELAGE ATTACHMENT - LH 2. PNO 210022-901 - WING RIB INBOARD FUSELAGE ATTACHMENT - RH 3.PNO 210029-4 - WING RIB INBOARD UNDERCARRIAGE BAY 4Mar 13, 1996 · Mooney M20E · Wing Main, Frame StructureSDR AU960239Hub · corroded(AUS) PROPELLER HUB SEVERELY CORRODED INTERNALLY IN HUB CAVITY AND AROUND ATTACHMENT BOLT FILLETSFeb 28, 1996 · Mooney M20E · Propeller Hub SectionSDR AU960561Rivet · sheared(AUS) HORIZONTAL STABILISER RH ATTACHMENT BRACKET RIVETS (8OFF) SHEAREDJan 31, 1996 · Mooney M20F · Fuselage Main, Attach FittingsSDR AU960059Control Column · broken(AUS) AFT CONTROL COLUMN BROKE IN AREA IN LINE WITH FORE AND AFT GUSSETWELD AND PRESS TO TALK (PTT) WIRING HOLE AT BOTTOM OF STICKJan 18, 1996 · Child S2APITTS · Control Column SectionSDR 96ZZZX390Magneto Tab · bentOPENED MAGNETO TO TROUBLESHOOT TIMING PROBLEM. FOUND COIL TAB BENT AT DOWNWARD ANGLE SUFFICIENT TO CAUSE STEEL BARREL OF CARBON BRUSH HOLDER TO BE ROTATING ON COIL TAB, DAMAGING IT SUBSTANTIALLY. THE SLICK MANUAL CALLS FOR FLUSH TO .0312 INCH FROM THE PARTINDec 29, 1995 · Mooney M20E · Magneto/DistributorSDR 95ZZZX2377Capacitor · shortingINVESTIGATION FOR AN INTERMITTENT DEAD MAG FOUND SPRING STRAP TOUCHING HOUSING AS P-LEAD IS PUSHED INTO COVER.Apr 27, 1995 · Magneto/DistributorSDR 95ZZZX2423Through-Bolt · failedSUBJECT NR 1 CYLINDER UPPER THROUGH-BOLT FOUND BROKEN DURING PRE-FLIGHT. DETECTED AS THE MAJOR REMAINING PORTION AND HOLD-DOWN NUT FOUND BACKED OUT OF POSITION AND LODGED AGAINST CYL FINS. INST NEW BOLT, SPACER, AND NUT. TORQUED PER LYCOMING S.I. 10293. BOLApr 25, 1995 · N7112V · Mooney M20F · Reciprocating Engine Cylinder SectionSDR 95ZZZX6141Through-Bolt · brokenSUBJECT NR 1 CYLINDER UPPER THROUGH-BOLT FOUND BROKEN DURING PREFLIGHT. DETECTED AS THE MAJOR REMAINING PORTION AND HOLD-DOWN NUT FOUND BACKED OUT OF POSITION AND LODGED AGAINST CYL FINS. INSTALLED NEW BOLT, SPACER, AND NUT. TORQUED PER LYC SERVICE LETTER 1Apr 25, 1995 · N7112V · Mooney M20F · Reciprocating Engine Power SectionSDR 95ZZZX2427Intake Pipe · crackedREPLACED PARTS RECEIVED BACK FROM OVERHAUL AGENCY FOLLOWING PROP STRIKE DISASSEMBLY INSPECTIONS INCLUDED A PN SL-10204J PISTON AND SUBJECT NR 3 CYL. INTAKE PIPE. PISTON EXHIBITED EARLY STAGES OF TYPICAL DETONATION DAMAGE ON THE HEAD, ADJACENT TO ITS O.D. AT TApr 24, 1995 · N7112V · Mooney M20F · Reciprocating Engine Cylinder SectionSDR 95ZZZX2428Oil Line · chafedINSPECTION FOLLOWING ENGINE REMOVAL REVEALED EXTREME CHAFING/WEAR DAMAGE TO PROP GOVERNOR EXTERNAL OIL LINE AT GOV. END APPROX 5 INCHES AWAY FROM B-NUT ATTACH. DAMAGED AREA APPROX .25 INCH BY .50 INCH & WEAR WAS NEARLY THROUGH TUBE WALL THICKNESS. OIL LOSS WApr 24, 1995 · N7112V · Mooney M20F · Reciprocating Engine Oil SystemSDR 95ZZZX6142Pipe · crackedREPLACED PARTS RECEIVED BACK FROM OVERHAUL AGENCY FOLLOWING PROP STRIKE DISASSEMBLY INSPECTIONS, INCLUDED A PN SL-1024J PISTON AND SUBJECT NR 3 CYL INTAKE PIPE. PISTON EXHIBITED EARLY STAGES OF TYPICAL DETONATION DAMAGE ON THE HEAD, ADJACENT TO ITS O.D., AT TApr 24, 1995 · N7112V · Mooney M20F · Reciprocating Engine Cylinder SectionSDR 95ZZZX6143Oil Line · chafedINSPECTION FOLLOWING ENGINE REMOVAL REVEALED EXTREME CHAFING/WEAR DAMAGE TO PROP GOVERNOR EXTERNAL OIL LINE AT GOV END APPROX 5 INCHES AWAY FROM B-NUT ATTACH. DAMAGED AREA APPROX .25 INCH BY .50 INCH & WEAR WAS NEARLY THROUGH TUBE WALL THICKNESS. OIL LOSS WAApr 24, 1995 · N7112V · Mooney M20F · Reciprocating Engine Oil SystemSDR 95ZZZX1309Dist Block · loose bushingON DISASSEMBLING THE MAG FOR INSPECTION, THE CENTER BRONZE BUSHING IN THE DISTRIBUTOR BLOCK WAS FOUND LOOSE IN THE PLASTIC MATERIAL OF THE BLOCK. THIS IS THE SECOND ELECTRO SYSTEMS DISTRIBUTOR BLOCK FOUND IN THIS CONDITION IN LAST MONTH, THE OTHER BLOCK WAS PFeb 16, 1995 · N3205F · Mooney M20F · Magneto/Distributor
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