# N5587K: 1989 Beech F33A, registration cancelled 2021-11-12 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 12, 2021 - Exported to: Brazil - Status when cancelled: Valid registration - Airframe: [Beech F33A](https://openairdocs.org/model/beech-f33a) (registry code 1151425) - Engine: [Continental IO-520 series](https://openairdocs.org/engine/continental-io-520-series) (registry code 17032) - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS E5CE](https://openairdocs.org/tcds/E5CE) (OpenAirDocs) - Serial number: CE-1392 - Year built: 1989 - Type of aircraft: Fixed wing single engine - Engine type: Reciprocating - Airworthiness: Standard, utility - Airworthiness date: October 9, 1989 - Certificate issued: July 14, 2021 - Last registry action: July 14, 2021 - Mode S code: A7207A - Owner when cancelled: [High Performance Aircraft Inc](https://openairdocs.org/faa-owner/HIGH%20PERFORMANCE%20AIRCRAFT%20INC) - Location: [El Cajon, CA](https://openairdocs.org/faa-place/CA/El%20Cajon) - Owner type: Corporation - Owner's area on the map: 32.7956° N, 116.9698° W: Placed by OpenAirDocs at the center of ZIP code 92020, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N5587K - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=5587K - Page: https://openairdocs.org/deregistered/N5587K-2021-11-12 From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Beech F33A: https://openairdocs.org/model/beech-f33a.md ## Service difficulty reports (19) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR VJ3R2015FA0000036](https://openairdocs.org/sdr/VJ3R2015FA0000036), Jan 27, 2015: CIRCUIT BREAKER. FAILED. 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 LI - [SDR VJ3R2015FA0000035](https://openairdocs.org/sdr/VJ3R2015FA0000035), Jan 27, 2015: CIRCUIT BREAKER. FAILED. 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 - [SDR VJ3R2014FA0000298](https://openairdocs.org/sdr/VJ3R2014FA0000298), May 2, 2014: CIRCUIT BREAKER. FAILED. PILOT REPORTED THAT THE STROBE LIGHTS WERE INOPERATIVE. TROUBLESHOT AND DISCOVERED THAT THE STROBE LIGHT CIRCUIT BREAKER WAS FAULTY, REPLACED STROBE LIGHT CIRCU - [SDR NJ3R2014042300263](https://openairdocs.org/sdr/NJ3R2014042300263), Apr 23, 2014: CIRCUIT BREAKER. FAILED. PILOT REPORTED THAT THE BEACON LIGHT WAS INOPERATIVE. THE TECH TROUBLESHOT THE SYSTEM AND DISCOVERED THE BEACON LIGHT FAILED. THE TECH REPLACED THE CIRCUIT BREA - [SDR 2012FA0000431](https://openairdocs.org/sdr/2012FA0000431), Jun 23, 2012: CIRCUIT BREAKER. FAILED. 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 LA - [SDR 2012FA0000366](https://openairdocs.org/sdr/2012FA0000366), Jun 9, 2012: CIRCUIT BREAKER. FAILED. 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 - [SDR 2012FA0000136](https://openairdocs.org/sdr/2012FA0000136), Feb 26, 2012: CIRCUIT BREAKER. FAILED. PILOT REPORTED STROBE LIGHTS INOPERATIVE. ON TOUBLESHOOTING, TECH FOUND CIRCUIT BREAKER TO BE AT FAULT. CIRCUIT BREAKER HAD BEEN REPLACED 1939 FLIGHT HOURS PRIO - [SDR 2011FA0000737](https://openairdocs.org/sdr/2011FA0000737), Nov 9, 2011: CIRCUIT BREAKER. FAILED. 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), Apr 4, 2010: PUMP. LOW PRESSURE. (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 - [SDR 2010FA0000077](https://openairdocs.org/sdr/2010FA0000077), Jan 27, 2010: CIRCUIT BREAKER. FAILED. 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 BR - [SDR 2010FA0000027](https://openairdocs.org/sdr/2010FA0000027), Dec 3, 2009: CIRCUIT BREAKER. FAILED. 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 - [SDR 2003FA0000732](https://openairdocs.org/sdr/2003FA0000732), Jun 12, 2003: RELAY. STICKING. RELAY FAILED TO FUNCTION ON THREE SEPARATE OCCASIONS CAUSING LANDING GEAR NOT TO EXTEND, PROBABLE CAUSE IS STICKING SOLENOID. RELAY IS SCHEDULED FOR CHANGE EVER - [SDR 2003FA0000741](https://openairdocs.org/sdr/2003FA0000741), Jun 5, 2003: MOTOR. INOPERATIVE. 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 V - [SDR 2003FA0000494](https://openairdocs.org/sdr/2003FA0000494), May 5, 2003: PUMP. WORN. 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 R - [SDR VJ32002F00000](https://openairdocs.org/sdr/VJ32002F00000), Dec 11, 2001: DISTRIBUTOR. INOPERATIVE. 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 - [SDR 20010607CW003](https://openairdocs.org/sdr/20010607CW003), May 18, 2001: FUEL CONTROL. DEFECTIVE. 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 - [SDR 96ZZZX62](https://openairdocs.org/sdr/96ZZZX62), Dec 4, 1995: PUMP. SHAFT SHEARED. ENGINE DRIVEN FUEL PUMP FAILED ON CLIMB AT 400 FEET AGL. - [SDR 96ZZZX822](https://openairdocs.org/sdr/96ZZZX822), Dec 1, 1995: VAPOR SEPARATOR. FOD JAMMED 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 DI - [SDR 95ZZZX4184](https://openairdocs.org/sdr/95ZZZX4184), Jun 27, 1995: RELAY. FAILED. 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 ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19921013044829I](https://openairdocs.org/incident/19921013044829I), Oct 13, 1992: Beech F33A (N5587K), Goodyear, AZ, Minor damage. Solo student pilot landed gear up. ## Other aircraft with N5587K - [Cancelled 1984-08-16](https://openairdocs.org/deregistered/N5587K-1984-08-16): Grumman S-2A, S/N 136465. Exported to Canada. Owner: [Reagan Enterprises](https://openairdocs.org/faa-owner/REAGAN%20ENTERPRISES), [Chico, CA](https://openairdocs.org/faa-place/CA/Chico) --- 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.