# Service difficulty reports: N5582X A list on [N5582X](https://openairdocs.org/aircraft/N5582X.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VJ3R2015FA0000107](https://openairdocs.org/sdr/VJ3R2015FA0000107.md): Fuel Control · malfunctioned · Mar 24, 2015 · N5582X · Beech F33A · Fuel Control/Reciprocating Engines > ON THE RUNWAY, THE ENGINE QUIT WHEN THE THROTTLE WAS ADVANCED. THE ENGINE WOULD NOT MAINTAIN A MIXTURE SETTING. - [SDR 2014FA0000649](https://openairdocs.org/sdr/2014FA0000649.md): Circuit Breaker · failed · Oct 31, 2014 · N5582X · Beech F33A · Exterior Lighting > PILOT REPORTED BEACON LIGHT INOPERATIVE. TROUBLESHOT AND FOUND CIRCUIT BREAKER FAILED. REPLACED THE CIRCUIT BREAKER, OPS CHECKED GOOD. - [SDR VJ3R2013FA0000755](https://openairdocs.org/sdr/VJ3R2013FA0000755.md): Relay · failed · Dec 17, 2013 · N5582X · Beech F33A · Landing Gear Retraction/Extension System > GEAR DID NOT EXTEND WHEN SELECTED DOWN. TROUBLESHOT THE LANDING GEAR SYSTEM AND DETERMINED THAT THE DYNAMIC BRAKE RELAY WAS AT FAULT. R & R THE DYNAMIC BRAKE RELAY. - [SDR 2012FA0000095](https://openairdocs.org/sdr/2012FA0000095.md): Circuit Breaker · failed · Feb 3, 2012 · N5582X · Beech F33A · Pitot/Static Anti-Ice System > PILOT REPORTED PITOT HEAT SWITCH WOULD NOT STAY IN THE ON POSITION. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2427 FLIGHT HOURS PRIOR. RECOMMEND MFG DEVELOP A MORE DURABLE CIRCUIT BREAKER OR ACFT M - [SDR 2012FA0000015](https://openairdocs.org/sdr/2012FA0000015.md): Circuit Breaker · failed · Jan 8, 2012 · N5582X · Beech F33A · Light System Wiring > PILOT REPORTED BEACON LIGHT INOPERATIVE. ON TROUBLESHOOTING, THE TECH FOUND THE BEACON LIGHT CIRCUIT BREAKER AT FAULT. INSTALLED NEW BEACON LIGHT CIRCUIT BREAKER. OPS CHECKED OK. - [SDR 2011FA0000731](https://openairdocs.org/sdr/2011FA0000731.md): Circuit Breaker · failed · Nov 4, 2011 · N5582X · Beech F33A · Exterior Lighting > PILOT REPORTED BEACON LIGHT INTERMITTENT. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. BEACON SWITCH WAS PREVIOUSLY REPLACED 721.9 FLIGHT HOURS PRIOR. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. - [SDR 2011FA0000058](https://openairdocs.org/sdr/2011FA0000058.md): Circuit Breaker · failed · Jan 31, 2011 · N5582X · Beech F33A · Exterior Lighting > PILOT REPORTED STROBE LIGHTS STAYED ON WHEN SWITCH WAS IN THE OFF POSITION. ON TROUBLESHOOTING TECH FOUND THE CIRCUIT BREAKER/SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 1505 FLIGHT HOURS PRIOR. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME. - [SDR 2010FA0000066](https://openairdocs.org/sdr/2010FA0000066.md): Switch · shorted · Jan 18, 2010 · N5582X · Beech F33A · Exterior Lighting > PILOT REPORTED TAXI LIGHT INOPERATIVE, INVESTIGATION BY TECH, FOUND TAXI LIGHT CIRCUIT BREAKER SWITCH WAS AT FAULT. REPLACED CIRCUIT BREAKER SWITCH SYS OPS CHECKED NORMAL. THIS CIRCUIT BREAKER SWITCH WAS REPLACED 888 HOURS FLIGHT TIME PRIOR TO FAILURE IAW AD - [SDR 2006FA0000111](https://openairdocs.org/sdr/2006FA0000111.md): Relay · intermittent · Jan 19, 2006 · N5582X · Beech F33A · Landing Gear System Wiring > PILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE DOWN POSITION THE GEAR WOULDN`T EXTEND, AFTER CYCLING GEAR SELECTOR GEAR WENT DOWN, AIRCRAFT RETURNED TO BASE. ON TROUBLESHOOTING THE MECHANIC SELECTED DOWN AND IT FAILED TO EXTEND, AFTER TAPPING ON TOP OF - [SDR 2005FA0000510](https://openairdocs.org/sdr/2005FA0000510.md): Relay · intermittent · Mar 4, 2005 · N5582X · Beech F33A · Landing Gear Retraction/Extension System > PILOT SELECTED GEAR UP AND NOTHING HAPPENED. AIRCRAFT RETURNED TO BASE. UPON FURTHER TROUBLESHOOTING, FOUND RELAY WAS INTERMITTENT, PROBABLE CAUSE AT THIS TIME UNKNOWN. INSTALLED NEW AND IMPROVED RELAY IAW DATE CODE. FURTHER IMPROVEMENT ON RELAY ARE NEEDED - [SDR 2005FA0000706](https://openairdocs.org/sdr/2005FA0000706.md): Relay · intermittent · Jan 13, 2005 · N5582X · Beech F33A · Landing Gear Brake System > PILOT SELECTED GEAR UP AND NOTHING HAPPENED. STILL INDICATING (3) GREEN LIGHTS LANDING GEAR WOULD NOT RETRACT. MAINTENANCE TECH TROUBLESHOT GEAR SYSTEM AND FOUND THAT THE DYNAMIC RELAY WAS INTERMITTENT. NO RECOMMENDATION AT THIS TIME. (K) - [SDR 2003FA0000721](https://openairdocs.org/sdr/2003FA0000721.md): Relay · failed · Jun 24, 2003 · N5582X · Beech F33A · Landing Gear Retraction/Extension System > DURING 50 HOUR INSPECTION OF LANDING GEAR, GEAR FAILED TO EXTEND (2) TIMES. UPON TROUBLESHOOTING GEAR SYSTEM FOUND DYNAMIC RELAY PN SM50D7 WAS BAD. REPLACED DYNAMIC RELAY AND CYCLED GEAR SEVERAL TIMES OPERATIONAL OF GEAR CHECKED GOOD. - [SDR 2003FA0000739](https://openairdocs.org/sdr/2003FA0000739.md): Ignition Switch · intermittent · May 29, 2003 · N5582X · Beech F33A · Ignition Switching > PILOT REPORTED NO DROP IN RPM WHILE PERFORMING MAGNETO CHECK ON GROUND RUN UP. WHILE JIGLING THE KEY AROUND, THE PILOT THEN NOTICED A DROP IN RPM. MAGNETO SWITCH IS CHECKED BEFORE TAKEOFF BY PILOTS FOR PROPER OPERATION AND AT EACH 50 HOUR INSPECTION MY MAINT - [SDR VJ32003F00013](https://openairdocs.org/sdr/VJ32003F00013.md): Pump · failed · Dec 12, 2002 · N5582X · Beech F33A · Pneumatic Distribution System > DURING GROUND RUN UP OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT IDLE RPM. RAN AIRCRAFT UP AND AIR PRESSURE STILL LOW AT HIGHER RPM. - [SDR VJ32002F00050](https://openairdocs.org/sdr/VJ32002F00050.md): Flow Divider · failed · Jun 28, 2002 · N5582X · Beech F33A · Fuel Divider > AT NORMAL POWER SETTINGS THE ENGINE RAN ROUGH AT 6000 TO 7000 FEET. REMOVED FUEL FLOW MANIFOLD VALVE AND INSTALLED NEW FUEL FLOW MANIFOLD VALVE. GROUND OPERATION OF THE ENGINE CHECKED NORMAL. PART SENT IN FOR WARRANTY. - [SDR VJ32001F00011](https://openairdocs.org/sdr/VJ32001F00011.md): Distributor Blk · failed · Nov 9, 2001 · N5582X · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO. (K) - [SDR VJ32001F00010](https://openairdocs.org/sdr/VJ32001F00010.md): Distributor Blk · failed · Nov 9, 2001 · N5582X · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBUTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY INSTALLED IN MAGNETO.(K) - [SDR 2001FA0000511](https://openairdocs.org/sdr/2001FA0000511.md): Pump · leaking · Oct 29, 2001 · N5582X · Beech F33A · Engine Fuel Pump > LEAKING FUEL FROM CASE DRAIN. - [SDR 2001FA0000505](https://openairdocs.org/sdr/2001FA0000505.md): Flow Divider · defective · Oct 29, 2001 · N5582X · Beech F33A · Fuel Divider > ENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN. THE FUEL FLOW DIVIDER WOULD STICK OPEN, LETTING CONTINUOUS FUEL FLOW TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL. - [SDR VJ32001F00006](https://openairdocs.org/sdr/VJ32001F00006.md): Flow Divider · sticks · Oct 29, 2001 · N5582X · Beech F33A · Fuel Divider > ENGINE RUN ROUGH AND SOMETIME WOULD NOT SHUT DOWN. THE FUEL FLOW DIVIDER WOULD STICK OPEN LETTING FUEL TOO CONTINUAL TO THE ENGINE. THE FLOW DIVIDER WAS REMOVED AND REPLACED WITH A NEW ONE, OPERATION OF ENGINE CHECKED OUT NORMAL. - [SDR VJ32001F00001](https://openairdocs.org/sdr/VJ32001F00001.md): Pump · leaking · Oct 29, 2001 · N5582X · Beech F33A · Engine Fuel Pump > LEAKING FUEL FROM CASE DRAIN. ## 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 = 'N5582X' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N5582X/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.