N1096W, cancelled May 24, 2012

Service difficulty reports · 20

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N1096W' AND deregistration_id = 'N1096W-2012-05-24'
  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 XGN2007F00019Cylinder · crackedCRACKED CYLINDER HEADS. (K)Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2007F00017Cylinder · crackedCRACKED CYLINDER HEADS. (K)Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2007F00003Cylinder Head · crackedCRACKED CYLINDER HEADS. (K)Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2007F00002Cylinder Head · crackedCRACKED CYLINDER HEADS. (K)Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2006F00002Cylinder · crackedCYLINDER HEAD CRACKED. (K)Apr 14, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2006F00000Cylinder · crackedCYLINDER HEAD CRACK BETWEEN THE EXHAUST VALVE SEAT AND THE BOTTOM SPARK PLUG HOLE. DUE TO THE CYLINDER HEAD FAILURES, WE ARE DOING COMPRESSION CHECKS AT 25 HR INTERVALS. (K)Apr 14, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2006F00075Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NUMBER OF CRACKED CYLINDER HEADS, WE DO A COMPRESSION CHECK EVERY 50 HRS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2006F00074Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NUMBER OF CRACKED CYLINDER HEADS. WE DO A COMPRESSION CHECK EVERY 50 HRS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2006F00073Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS, COMPRESSION CHECK EVERY 50 HRS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2006F00001Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NUMBER OF CRACKED CYLINDER HEADS, WE DO A COMPRESSION CHECK EVERY 50 HRS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2005F00017Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS, A COMPRESSION CHECK IS DONE EVERY 50 HOURS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2005F00016Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS. DO A COMPRESSION CHECK EVERY 50 HOURS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2005F00015Cylinder · crackedTHESE CYLINDERS SHOWED TO BE CRACKED IN THE EXHAUST SIDE OF THE HEAD. THE LEAKS SHOWED UP WHEN DOING THE COMPRESSION CHECK. DUE TO THE NR OF CRACKED CYLINDER HEADS, COMPRESSION CHECK DOEN EVERY 50 HOURS. (K)Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR XGN2003F00001Crankcase · crackedCRACK WAS DISCOVERED WHILE LOOKING FOR THE SOURCE OF AN OIL LEAK.Jun 16, 2003 · N1096W · Beech F33A · Reciprocating Engine Power SectionSDR XGN2003F00000Bearing · failedIN FLIGHT, AIRCRAFT LANDED WITHOUT INCIDENT. THE ALTERNATOR DRIVE END BEARING FAILED CAUSING THE ALTERNATOR ROTOR ASSEMBLY WITH THE DRIVEN GEAR TO EXTEND INTO THE ALTERNATOR DRIVE GEAR. THE MISALIGNMENT OF THESE TWO GEARS CAUSED THE ATTACH BOLTS ON THE ALTERMar 1, 2003 · N1096W · Beech F33A · AC Generator-AlternatorSDR 20000913SH009Cylinder Head · departedCYLINDER HEAD DEPARTED BARREL WHILE AIRCRAFT IN-FLIGHT. (X)Aug 30, 2000 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR 96ZZZX5337Crankcase · crackedON 10-2-96 MAINTENANCE WAS NOTIFIED OF AN OIL LEAK ON THE ENGINE. UPON FURTHER INVESTIGATION, A CRACK WAS NOTED ABOVE THE TOP FORWARD CYLINDER HOLD DOWN STUD OF THE NR 5 CYLINDER. SUSPECT CAUSE OVERTORQUEING OR TORQUEING SEQUENCE. SUBMIMTTER STATED CLOSE INOct 2, 1996 · N1096W · Beech F33A · Reciprocating Engine Power SectionSDR 95ZZZX1460Cylinder · guide looseDURING A ROUTE INPSECTION, NR 1 CYLINDER DISPLAYED LOW COMPRESSION. FURTHER INVESTIGATION, AFTER REMOVAL OF CYLINDER, REVEALED A LOOSE VALVE GUIDE IN THE CYLINDER HEAD. THIS ENGINE HAD BEEN OVERHAULED 70.0 HOURS PREVIOUS TO THE INSPECTION. CAUSE: INCORRECTFeb 22, 1995 · N1096W · Beech F33A · Reciprocating Engine Cylinder SectionSDR 95ZZZX1118Fuel Pump · failedENGINE LOST POWER WHEN REDUCED FOR DESCENT. EFFORTS TO RESTART ENGINE FAILED. AIRCRAFT MADE AN UNEVENTFUL OFF AIRPORT LANDING. AFTER AIRCRAFT SAT, ENGINE WAS ABLE TO BE RESTARTED. PUMP WAS REMOVED AND SENT OUT FOR CHECK. MULTIPLE DISCREPANCIES WERE FOUND Jan 19, 1995 · N1096W · Beech F33A · Fuel Control/Reciprocating EnginesSDR 95ZZZX576Wheel Assy · crackedUPON INFLATION OF NOSE WHEEL AND TIRE ASSEMBLY, A 6 INCH PIECE OF THE WHEEL LIP FAILED. TIRE AND TUBE WERE DESTROYED, FAILED SECTION OF WHEEL WAS FOUND 50 FEET AWAY. NO PERSONNEL WERE INJURED. SUSPECT CAUSE, FATIGUE-CASTING FLAW.Jan 9, 1995 · N1096W · Beech F33A · Wheel/Ski/Float
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