N5585Y

Service difficulty reports · 16

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 = 'N5585Y' 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 2015FA0000023Lock Nut · strippedSHORTLY AFTER TAKEOFF, HAD A REDUCTION IN FUEL FLOW, LANDED WITHOUT INCIDENT. UPON INSPECTION IT WAS NOTICED THAT THE RETAINING LOCKNUT FOR THE MIXTURE CONTROL LEVER HAD BACKED OFF THE LEVER CAUSING THE LEVER TO COME OUT OF RIG AND STRIP THE SPLINES OFF THE LJan 22, 2015 · N5585Y · Beech F33A · Mixture ControlSDR VJ3R2014101300601Circuit Breaker · failedPILOT REPORTED THAT THE NAV LIGHT WAS INOPERATIVE. THE TECHNICIAN TROUBLESHOT THE SYSTEM AND DISCOVERED THE NAV LIGHT FAILED. THE TECHNICIAN REPLACED THE NAV LIGHT CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME.Oct 13, 2014 · N5585Y · Beech F33A · Light System WiringSDR 2013FA0000618Circuit Breaker · failedPILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. TROUBLESHOT SYSTEM AND DISCOVERED BEACON LIGHT CIRCUIT BREAKER FAILED. REPLACED THE CIRCUIT BREAKER.Oct 27, 2013 · N5585Y · Beech F33A · Light System WiringSDR 2013FA0000021Circuit Breaker · failedPILOT REPORTED THE TAXI LIGHT AS BEING INOPERATIVE. ON TROUBLESHOOTING, FOUND THE CIRCUIT BREAKER TO BE AT FAULT. REPLACED THE CIRCUIT BREAKER.Jan 11, 2013 · N5585Y · Beech F33A · Exterior LightingSDR VJ3R20110901001Circuit Breaker · failedPILOT REPORTED BEACON LIGHT INOP. ON TROUBLESHOOTING, TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2466 FLIGHT HOURS PRIOR. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.Sep 1, 2011 · N5585Y · Beech F33A · Exterior LightingSDR 2011FA0000426Circuit Breaker · failedPILOT REPORTED STROBES LIGHT’S INOP. ON TROUBLESHOOTING TECHNICIAN FOUND CIRCUIT BREAKER / SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2300 FLIGHT HOURS PRIOR, ESTIMATED CYCLES 9200. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.Jun 28, 2011 · N5585Y · Beech F33A · Exterior LightingSDR 2011FA0000393Pneumatic System · failedPILOT REPORTED THE GYRO WARNING LIGHT CAME ON IN FLIGHT. UP ON TROUBLESHOOTING THE MECHANIC FOUND THE SHAFT SHEARED. INSTALLED NEW PUMP, SYS WORKED NORMAL. NO PROBABLE CAUSE OR RECOMMENDATIONS AT THIS TIME.Jun 23, 2011 · N5585Y · Beech F33A · Pneumatic Distribution SystemSDR 2011FA0000243Circuit Breaker · failedPILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECH FOUND CIRCUIT BREAKER/ SWITCH TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 923 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 3692. NOTICED NEW CIRCUIT BREAKER MFG. NO PROBABLE CAUSE OR RECOMMENDATIONS AT Apr 13, 2011 · N5585Y · Beech F33A · Exterior LightingSDR 2010FA0000464Circuit Breaker · inoperativePILOT REPORTED TAXI LIGHT INOP. ON TROUBLESHOOTING TECHNICIAN FOUND CIRCUIT BREAKER / SWITCH TO BE AT FAULT. A.D. 2008-13-17 HAD BEEN COMPLETED 1180 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 4720. NOTICED NEW CIRCUIT BREAKER MANUFACTURER IS TYCO ELECTRONICS. NO May 13, 2010 · N5585Y · Beech F33A · Exterior LightingSDR 2009FA0000301Relay · intermittentPILOT REPORTED AFTER PUTTING THE GEAR SELECTOR IN THE UP POSITION, THE GEAR FAILED TO RETRACT, PILOT THEN PUT THE GEAR SELECTOR IN THE DOWN POSITION AND RETURNED TO BASE. ON TROUBLESHOOTING, THE MECHANIC CYCLED GEAR SEVERAL TIMES AND WAS UNABLE TO GET THE GEApr 5, 2009 · N5585Y · Beech F33A · Landing Gear System WiringSDR 2005FA0000705Relay · intermittentPILOT SELECTED GEARDOWN AND NOTHING HAPPENED. LANDING GEAR WOULD NOT EXTEND. FLIGHT CREW EXTENDED LANDING GEAR MANUALLY AND LANDED WITHOUT INCIDENT. MAINTENANCE TECH TROUBLESHOT GEAR SYSTEM AND FOUND THE DYNAMIC BRAKE RELAY WAS INTERMITTENT. RECOMMENDATIONJan 12, 2005 · N5585Y · Beech F33A · Landing Gear SystemSDR 2003FA0000954Transducer · failedFUEL FLOW WENT TO ZERO INDICATION IN FLT. TESTS SHOWED THAT HERTZ FLUCTUATED AND READ LOWER THAN PUBLISHED SPECIFICATIONS. SUSPECT INTERNAL FAILURE, PERHAPS IMPELLER IS STICKING. NOT RECOMMENDATIONS AT THIS TIME.Sep 10, 2003 · N5585Y · Beech F33A · Fuel Flow SensorSDR 2003FA0000742Pump · wornAVIONICS PERSONNEL FOUND INSTRUMENT AIR PRESSURE LOW ON GROUND RUN UP. ON FURTHER INVESTIGATION FOUND VANES WORN ON PUMP. RECOMMEND PUTTING DIFFERENT TYPE OF VANES IN PUMP TO LAST LONGER.Jun 9, 2003 · N5585Y · Beech F33A · Pneumatic Distribution SystemSDR VJ32002F00049Pump · failedDURING GROUND RUN UP, OUTPUT OF ENGINE DRIVEN DRY AIR PUMP FAILED TO PUT OUT PROPER PRESSURE AT 800 RPM. RAN AIRCRAFT UP TO 1600 RPM BEFORE PRESSURE READ 4.5. CHECKED PRESSURE SYSTEM FOR LEAKS AND CHECKED REGULATOR ALL CHECKED WELL.Jul 3, 2002 · N5585Y · Beech F33A · Pneumatic SystemSDR 2001FA0000566Distributor Blk · inoperativeMAGNETO 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 16, 2001 · N5585Y · Beech F33A · Magneto/DistributorSDR VJ32001F00009Brushes · wornMAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW THE MAINTENANCE MANUAL. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO AND FOUND THE CARBON BRUSH WORN. CARBON DUST WAS FOUND ON THE FLAT PART OF THE CAP. WHERE IT LOOKS LIKE A SMALL SPANov 8, 2001 · N5585Y · Beech F33A · Magneto/Distributor
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