# Service difficulty reports: N5587K, cancelled Nov 12, 2021 A list on [N5587K, cancelled Nov 12, 2021](https://openairdocs.org/deregistered/N5587K-2021-11-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR VJ3R2015FA0000036](https://openairdocs.org/sdr/VJ3R2015FA0000036.md): Circuit Breaker · failed · Jan 27, 2015 · N5587K · Beech F33A · Exterior Lighting > PILOT REPORTED THAT THE LANDING LIGHT CIRCUIT BREAKER SWITCH WAS NOT STAYING IN THE "ON" POSITION. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE LANDING LIGHT CIRCUIT BREAKER SWITCH FAILED. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR REC - [SDR VJ3R2015FA0000035](https://openairdocs.org/sdr/VJ3R2015FA0000035.md): Circuit Breaker · failed · Jan 27, 2015 · N5587K · Beech F33A · Exterior Lighting > PILOT REPORTED THAT THE TAXI LIGHT WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE TAXI LIGHT FAILED. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME. - [SDR VJ3R2014FA0000298](https://openairdocs.org/sdr/VJ3R2014FA0000298.md): Circuit Breaker · failed · May 2, 2014 · N5587K · Beech F33A · Light System Wiring > PILOT REPORTED THAT THE STROBE LIGHTS WERE INOPERATIVE. TROUBLESHOT AND DISCOVERED THAT THE STROBE LIGHT CIRCUIT BREAKER WAS FAULTY, REPLACED STROBE LIGHT CIRCUIT BREAKER WITH NEW AND STROBE LIGHTS OPERATED NORMALLY. - [SDR NJ3R2014042300263](https://openairdocs.org/sdr/NJ3R2014042300263.md): Circuit Breaker · failed · Apr 23, 2014 · N5587K · Beech F33A · Light System Wiring > PILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE BEACON LIGHT FAILED. THE TECH REPLACED THE CIRCUIT BREAKER SWITCH. NO CAUSE OR RECOMMENDATION AT THIS TIME. - [SDR 2012FA0000431](https://openairdocs.org/sdr/2012FA0000431.md): Circuit Breaker · failed · Jun 23, 2012 · N5587K · Beech F33A · Light System Wiring > PILOT REPORTED THAT THE LANDING LIGHT WAS NOT WORKING. DURING TROUBLESHOOTING, FOUND THAT THE LANDING LIGHT CIRCUIT BREAKER WAS TO BE AT FAULT. INSTALLED NEW LANDING LIGHT SWITCH AND OPS CHECKED GOOD. - [SDR 2012FA0000366](https://openairdocs.org/sdr/2012FA0000366.md): Circuit Breaker · failed · Jun 9, 2012 · N5587K · Beech F33A · DC Generator-Alternator > PILOT REPORTED THAT THE ALTERNATOR WAS NOT WORKING. DURING TROUBLESHOOTING, FOUND THAT THE ALTERNATOR FIELD CIRCUIT BREAKER SWITCH WAS FOUND TO BE AT FAULT. THE SWITCH WAS INSTALLED ON 07 APRIL 2009 WITH A TSN OF 3098 WITH AN ESTEMATED 12392 CYCLES. INSTALLE - [SDR 2012FA0000136](https://openairdocs.org/sdr/2012FA0000136.md): Circuit Breaker · failed · Feb 26, 2012 · N5587K · Beech F33A · Exterior Lighting > PILOT REPORTED STROBE LIGHTS INOPERATIVE. ON TOUBLESHOOTING, TECH FOUND CIRCUIT BREAKER TO BE AT FAULT. CIRCUIT BREAKER HAD BEEN REPLACED 1939 FLIGHT HOURS PRIOR AND ESTIMATED CYCLES 7756. - [SDR 2011FA0000737](https://openairdocs.org/sdr/2011FA0000737.md): Circuit Breaker · failed · Nov 9, 2011 · N5587K · Beech F33A · Light System Wiring > PILOT REPORTED NAV LIGHTS INOPERATIVE. MX FOUND CIRCUIT BREAKER TO BE AT FAULT. AD 2008-13-17 HAD BEEN COMPLETED 2489.0 FLIGHT HOURS PRIOR. - [SDR 2010FA0000288](https://openairdocs.org/sdr/2010FA0000288.md): Pump · low pressure · Apr 4, 2010 · N5587K · Beech F33A · Pneumatic Distribution System > (VJ3R)ON PHASE RUN UP MECHANIC NOTICED THE GYRO WARNING LIGHT ON. UP ON TROUBLESHOOTING THE MECHANIC DETERMINED THE VANES ON THE AIR PUMP WERE WORN AND WAS NOT PRODUCING ENOUGH PRESSURE. INSTALLED NEW PUMP, SYS WORKED NORMAL. NO PROBABLE CAUSE OR RECOMMENDAT - [SDR 2010FA0000077](https://openairdocs.org/sdr/2010FA0000077.md): Circuit Breaker · failed · Jan 27, 2010 · N5587K · Beech F33A · Light System Wiring > WHEN PILOT SELECTED LANDING LIGHT, LIGHT DID NOT WORK. TECH TROUBLESHOT AND FOUND FAULT TO BE WITH LANDING LIGHT CIRCUIT BREAKER, INTERNAL FAILURE OF CIRCUIT BREAKER. - [SDR 2010FA0000027](https://openairdocs.org/sdr/2010FA0000027.md): Circuit Breaker · failed · Dec 3, 2009 · N5587K · Beech F33A · DC Power Distribution System > DURING USE OF NAV LIGHTS, NAVIGATION LIGHT CIRCUIT BREAKER SWITCH WAS PLACED IN ON POSITION AND NAVIGATION LIGHTS DID NOT COME ON. PROBABLE CAUSE TO FAILURE WAS DUE TO INTERNAL FAILURE OF CIRCUIT BREAKER SWITCH. SEPARATE THE SWITCH FOR AN INDEPENDENT TOGGLE - [SDR 2003FA0000732](https://openairdocs.org/sdr/2003FA0000732.md): Relay · sticking · Jun 12, 2003 · N5587K · Beech F33A · Landing Gear System Wiring > RELAY FAILED TO FUNCTION ON THREE SEPARATE OCCASIONS CAUSING LANDING GEAR NOT TO EXTEND, PROBABLE CAUSE IS STICKING SOLENOID. RELAY IS SCHEDULED FOR CHANGE EVERY 900 HOURS. RECOMMEND CHANGING TO AN IMPROVED DESIGN RELAY. - [SDR 2003FA0000741](https://openairdocs.org/sdr/2003FA0000741.md): Motor · inoperative · Jun 5, 2003 · N5587K · Beech F33A · Air Distribution Fan > DURING FLIGHT, VENT BLOWER BECAME INOPERATIVE. TESTED SYSTEM ON GROUND AND FOUND VENT BLOWER ASSEMBLY MOTOR WAS BURNED OUT. SUSPECT CAUSE IS CONTINUOUS USE OF VENT BLOWER DURING FLIGHT. RECOMMEND INSTALLING AN INTERMITTENT SWITCH TO SHUT OFF VENT BLOWER WHE - [SDR 2003FA0000494](https://openairdocs.org/sdr/2003FA0000494.md): Pump · worn · May 5, 2003 · N5587K · 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 HIGHTER RPM TESTED SYSTEM AND FOUND ENGINE DRIVEN AIR PUMP NOT WORKING PROPERLY. BELIEVE DRY AIR PUMP VANES - [SDR VJ32002F00000](https://openairdocs.org/sdr/VJ32002F00000.md): Distributor · inoperative · Dec 11, 2001 · N5587K · Beech F33A · Magneto/Distributor > MAGNETO REMOVED FROM ENGINE FOR 500 HOUR INSPECTION IAW MM. REMOVED THE REAR COVER AND THE DISTRIBUTOR BLOCK FROM MAGNETO. DISTRIBTOR BLOCK ASSEMBLY SENT TO MFG FOR INSPECTION. NEW DISTRIBUTOR BLOCK ASSEMBLY. INSTALLED MAGNETO. - [SDR 20010607CW003](https://openairdocs.org/sdr/20010607CW003.md): Fuel Control · defective · May 18, 2001 · N5587K · Beech F33A · Fuel Control/Reciprocating Engines > THE PILOT REPORTED A ROUGH ENGINE IN FLIGHT AND RETURNED TO AIRPORT, A SAFE LANDING WAS MADE. MAINTENANCE GROUND RUN AIRCRAFT AND A FLUCTUATION IN FUEL FLOW WAS NOTED. THEY FOUND THAT THE MIXTURE CONTROL WAS STIFF WHEN MOVING, (POSSIBLE GALLING). - [SDR 96ZZZX62](https://openairdocs.org/sdr/96ZZZX62.md): Pump · shaft sheared · Dec 4, 1995 · N5587K · Beech F33A · Engine Fuel Pump > ENGINE DRIVEN FUEL PUMP FAILED ON CLIMB AT 400 FEET AGL. - [SDR 96ZZZX822](https://openairdocs.org/sdr/96ZZZX822.md): Vapor Separator · fod jammed pump · Dec 1, 1995 · N5587K · Beech F33A · Engine Fuel Pump > CUSTOMER REPORTED ENG DRIVEN FUEL PUMP FAILED AT 600 FEET AGL AFTER T/O. PILOT ACTIVATED ELEC PUMP AND SAFELY LANDED AIRPLANE. PUMP SENT TO THIS FACILITY FOR DISASSEMBLY AND INSP. WHEN PUMP DISASSEMBLED, 2 SMALL FLAKES OF ALUM FOUND JAMMED IN VANES OF PUMP. - [SDR 95ZZZX4184](https://openairdocs.org/sdr/95ZZZX4184.md): Relay · failed · Jun 27, 1995 · N5587K · Beech F33A · Landing Gear Retraction/Extension System > LANDING GEARBOX BOTTOMED OUT IN THE GEAR UP POSITION DUE TO FAILURE OF RELAY. EXTREME FORCE WAS REQUIRED WITH BOOT ON THE GEAR HANDLE TO BREAK LOOSE BEFORE GEAR COULD BE CRANKED DOWN. NOTE: A SOLO PILOT WOULD HAVE TO CLIMB INTO BACK SEAT TO HAVE ENOUGH FORC ## 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 = 'N5587K' AND deregistration_id = 'N5587K-2021-11-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N5587K-2021-11-12/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, except the copies of manufacturers’ service documents, which belong to their rights holders.