# Service difficulty reports: N1096W, cancelled May 24, 2012 A list on [N1096W, cancelled May 24, 2012](https://openairdocs.org/deregistered/N1096W-2012-05-24.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR XGN2007F00019](https://openairdocs.org/sdr/XGN2007F00019.md): Cylinder · cracked · Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CRACKED CYLINDER HEADS. (K) - [SDR XGN2007F00017](https://openairdocs.org/sdr/XGN2007F00017.md): Cylinder · cracked · Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CRACKED CYLINDER HEADS. (K) - [SDR XGN2007F00003](https://openairdocs.org/sdr/XGN2007F00003.md): Cylinder Head · cracked · Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CRACKED CYLINDER HEADS. (K) - [SDR XGN2007F00002](https://openairdocs.org/sdr/XGN2007F00002.md): Cylinder Head · cracked · Oct 10, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CRACKED CYLINDER HEADS. (K) - [SDR XGN2006F00002](https://openairdocs.org/sdr/XGN2006F00002.md): Cylinder · cracked · Apr 14, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CYLINDER HEAD CRACKED. (K) - [SDR XGN2006F00000](https://openairdocs.org/sdr/XGN2006F00000.md): Cylinder · cracked · Apr 14, 2006 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CYLINDER 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) - [SDR XGN2006F00075](https://openairdocs.org/sdr/XGN2006F00075.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2006F00074](https://openairdocs.org/sdr/XGN2006F00074.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2006F00073](https://openairdocs.org/sdr/XGN2006F00073.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2006F00001](https://openairdocs.org/sdr/XGN2006F00001.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2005F00017](https://openairdocs.org/sdr/XGN2005F00017.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2005F00016](https://openairdocs.org/sdr/XGN2005F00016.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2005F00015](https://openairdocs.org/sdr/XGN2005F00015.md): Cylinder · cracked · Oct 11, 2005 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > THESE 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) - [SDR XGN2003F00001](https://openairdocs.org/sdr/XGN2003F00001.md): Crankcase · cracked · Jun 16, 2003 · N1096W · Beech F33A · Reciprocating Engine Power Section > CRACK WAS DISCOVERED WHILE LOOKING FOR THE SOURCE OF AN OIL LEAK. - [SDR XGN2003F00000](https://openairdocs.org/sdr/XGN2003F00000.md): Bearing · failed · Mar 1, 2003 · N1096W · Beech F33A · AC Generator-Alternator > IN 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 ALTER - [SDR 20000913SH009](https://openairdocs.org/sdr/20000913SH009.md): Cylinder Head · departed · Aug 30, 2000 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > CYLINDER HEAD DEPARTED BARREL WHILE AIRCRAFT IN-FLIGHT. (X) - [SDR 96ZZZX5337](https://openairdocs.org/sdr/96ZZZX5337.md): Crankcase · cracked · Oct 2, 1996 · N1096W · Beech F33A · Reciprocating Engine Power Section > ON 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 IN - [SDR 95ZZZX1460](https://openairdocs.org/sdr/95ZZZX1460.md): Cylinder · guide loose · Feb 22, 1995 · N1096W · Beech F33A · Reciprocating Engine Cylinder Section > DURING 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: INCORRECT - [SDR 95ZZZX1118](https://openairdocs.org/sdr/95ZZZX1118.md): Fuel Pump · failed · Jan 19, 1995 · N1096W · Beech F33A · Fuel Control/Reciprocating Engines > ENGINE 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 - [SDR 95ZZZX576](https://openairdocs.org/sdr/95ZZZX576.md): Wheel Assy · cracked · Jan 9, 1995 · N1096W · Beech F33A · Wheel/Ski/Float > UPON 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N1096W-2012-05-24/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.