N5582X

Service difficulty reports · 21

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 = 'N5582X' AND registry_match = 'registration'
  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 VJ3R2015FA0000107Fuel Control · malfunctionedON THE RUNWAY, THE ENGINE QUIT WHEN THE THROTTLE WAS ADVANCED. THE ENGINE WOULD NOT MAINTAIN A MIXTURE SETTING.Mar 24, 2015 · N5582X · Beech F33A · Fuel Control/Reciprocating EnginesSDR 2014FA0000649Circuit Breaker · failedPILOT REPORTED BEACON LIGHT INOPERATIVE. TROUBLESHOT AND FOUND CIRCUIT BREAKER FAILED. REPLACED THE CIRCUIT BREAKER, OPS CHECKED GOOD.Oct 31, 2014 · N5582X · Beech F33A · Exterior LightingSDR VJ3R2013FA0000755Relay · failedGEAR 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.Dec 17, 2013 · N5582X · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2012FA0000095Circuit Breaker · failedPILOT 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 MFeb 3, 2012 · N5582X · Beech F33A · Pitot/Static Anti-Ice SystemSDR 2012FA0000015Circuit Breaker · failedPILOT 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.Jan 8, 2012 · N5582X · Beech F33A · Light System WiringSDR 2011FA0000731Circuit Breaker · failedPILOT 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.Nov 4, 2011 · N5582X · Beech F33A · Exterior LightingSDR 2011FA0000058Circuit Breaker · failedPILOT 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.Jan 31, 2011 · N5582X · Beech F33A · Exterior LightingSDR 2010FA0000066Switch · shortedPILOT 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 Jan 18, 2010 · N5582X · Beech F33A · Exterior LightingSDR 2006FA0000111Relay · intermittentPILOT 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 OFJan 19, 2006 · N5582X · Beech F33A · Landing Gear System WiringSDR 2005FA0000510Relay · intermittentPILOT 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 NEEDEDMar 4, 2005 · N5582X · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2005FA0000706Relay · intermittentPILOT 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)Jan 13, 2005 · N5582X · Beech F33A · Landing Gear Brake SystemSDR 2003FA0000721Relay · failedDURING 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.Jun 24, 2003 · N5582X · Beech F33A · Landing Gear Retraction/Extension SystemSDR 2003FA0000739Ignition Switch · intermittentPILOT 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 MAINTMay 29, 2003 · N5582X · Beech F33A · Ignition SwitchingSDR VJ32003F00013Pump · failedDURING 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.Dec 12, 2002 · N5582X · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00050Flow Divider · failedAT 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.Jun 28, 2002 · N5582X · Beech F33A · Fuel DividerSDR VJ32001F00011Distributor Blk · failedMAGNETO 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)Nov 9, 2001 · N5582X · Beech F33A · Magneto/DistributorSDR VJ32001F00010Distributor Blk · failedMAGNETO 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)Nov 9, 2001 · N5582X · Beech F33A · Magneto/DistributorSDR 2001FA0000511Pump · leakingLEAKING FUEL FROM CASE DRAIN.Oct 29, 2001 · N5582X · Beech F33A · Engine Fuel PumpSDR 2001FA0000505Flow Divider · defectiveENGINE 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.Oct 29, 2001 · N5582X · Beech F33A · Fuel DividerSDR VJ32001F00006Flow Divider · sticksENGINE 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.Oct 29, 2001 · N5582X · Beech F33A · Fuel DividerSDR VJ32001F00001Pump · leakingLEAKING FUEL FROM CASE DRAIN.Oct 29, 2001 · N5582X · Beech F33A · Engine Fuel Pump
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