# N575RP: 2004 Embraer EMB-145LR, registration cancelled 2018-11-07 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 7, 2018 - Exported to: South Africa - Status when cancelled: Valid registration - Airframe: [Embraer EMB-145LR](https://openairdocs.org/model/embraer-emb-145lr) (registry code 3260212) - Engine: [Rolls-Royce AE-3007A1P](https://openairdocs.org/engine/rolls-royce-ae-3007a1p) (registry code 54571) - Data sheets: [TCDS T00011AT](https://openairdocs.org/tcds/T00011AT), [TCDS TE6CH](https://openairdocs.org/tcds/TE6CH) (OpenAirDocs) - Serial number: 14500847 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 17, 2004 - Certificate issued: January 12, 2017 - Last registry action: May 8, 2018 - Mode S code: A76281 - Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N575RP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=575RP - Page: https://openairdocs.org/deregistered/N575RP-2018-11-07 From the FAA registry file of October 29, 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 Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (29) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA2015041500260](https://openairdocs.org/sdr/UHLA2015041500260), Apr 15, 2015: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. THE LIGHT WAS REPLACED. OPS CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOT - [SDR UHLA2015040300223](https://openairdocs.org/sdr/UHLA2015040300223), Apr 3, 2015: CONTROLLER. FAILED. THE CREW REPORTED THAT WHILE THE AUTO PRESSURIZATION SYSTEM WAS DEFERRED, THE MANUAL PRESSURIZATION SYSTEM WOULD NOT PRESSURIZE THE CABIN. THE CREW RETURNED TO - [SDR UHLA2015012400047](https://openairdocs.org/sdr/UHLA2015012400047), Jan 24, 2015: BLEED VALVE. FAILED. THE CREW REPORTED THAT THEY RECEIVED A NR 1 BLEED VALVE FAIL MESSAGE AND A STAB ANIT-ICE VALVE FAIL MESSAGE DURING CLIMB OUT. THE CREW RETURNED TO FIELD AND LAN - [SDR CHQA20140701221](https://openairdocs.org/sdr/CHQA20140701221), Jul 1, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 BETWEEN FRAME 19 & 23. THE CTR OMEGA BEAM WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140701211](https://openairdocs.org/sdr/CHQA20140701211), Jul 1, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CTR OMEGA BEAM Y=0.0 & FRAME 59. THE BEAM WAS REPAIRED IAW ETD 2014-145-055505. - [SDR CHQA20140629222](https://openairdocs.org/sdr/CHQA20140629222), Jun 29, 2014: FITTING. CRACKED. DURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR FRAME 80 SHEAR CLIP WAS FOUND CRACKED AT STRINGER 1L. THE SHEAR CLIP WAS REPLACED IAW WITH SRM 51-40-02. - [SDR CHQA20140629215](https://openairdocs.org/sdr/CHQA20140629215), Jun 29, 2014: ANGLE. CRACKED. DURING INSPECTION, AFT FUSELAGE INSIDE ACCESS PANEL 312AR ANGLE ON THE APU FIREWALL AT STRINGER 10R & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL ANGLE W - [SDR CHQA20140629214](https://openairdocs.org/sdr/CHQA20140629214), Jun 29, 2014: FITTING. CRACKED. DURING INSPECTION, THE AFT FUSELAGE INSIDE ACCESS 312AR CLIP ON THE APU FIREWALL AT STRINGER 10L & FRAME 80 WAS FOUND TO BE CRACKED. THE APU FIREWALL CLIP AT FR - [SDR CHQA20140629212](https://openairdocs.org/sdr/CHQA20140629212), Jun 29, 2014: REPAIR. DENTED. DURING INSPECTION, A PREVIOUS REPAIR ON THE CARGO DOOR WAS FOUND TO BE DENTED AT THE LOWER AFT EDGE. THE DENT WAS REPAIRED IAW ETD 2014-145-055666. - [SDR CHQA20140628220](https://openairdocs.org/sdr/CHQA20140628220), Jun 28, 2014: RIB. GROOVED. DURING INSPECTION, A GROOVE WAS FOUND ON THE RT ELEVATOR NOSE RIB AT ELEVATOR STATION YH-1280.00 & HORIZONTAL & STAB YH=1310.00. THE RIB WAS REPLACED IAW SRM 51 - [SDR CHQA20140628219](https://openairdocs.org/sdr/CHQA20140628219), Jun 28, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & 16R WAS FOUND TO CRACKED. THE SHEAR CLIP WAS REPLACED IAW ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA20140628217](https://openairdocs.org/sdr/CHQA20140628217), Jun 28, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 24 & STRINGER 15R WAS FOUND CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140627218](https://openairdocs.org/sdr/CHQA20140627218), Jun 27, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 25 & STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140627214](https://openairdocs.org/sdr/CHQA20140627214), Jun 27, 2014: SKIN. DENTED. DURING HEAVY MX, A DENT BELOW & AFT OF ENG 2 ON THE FUSELAGE SKIN WAS REPAIRED IAW ETD 2014-145-054213. - [SDR CHQA20140627213](https://openairdocs.org/sdr/CHQA20140627213), Jun 27, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 26 AND STRINGER 16R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140511147](https://openairdocs.org/sdr/CHQA20140511147), May 11, 2014: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER AIRSTAIR DOOR SKIN. THE DOOR WAS REPAIRED IAW ETD2014-145-039320. - [SDR CHQA20140303072](https://openairdocs.org/sdr/CHQA20140303072), Mar 3, 2014: LIGHT. INOPERATIVE. DURING INSPECTION THE RT OVERWING EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE RT OVERWING EMERGENCY LIGHT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS - [SDR CHQA20130721282](https://openairdocs.org/sdr/CHQA20130721282), Jul 21, 2013: VALVE. FAULTY. CREW RECEIVED A NR 2 BLEED LOW TEMPERATURE MESSAGE DURING ICING CONDITIONS IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MX REPLACED NR 2 HIGH STAGE VALVE. O - [SDR CHQA20130702253](https://openairdocs.org/sdr/CHQA20130702253), Jul 2, 2013: SIGN. INOPERATIVE. DURING INSPECTION, THE RT OVERWING EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MX REPLACED THE EMERGENCY EXIT SIGN AND ALL OPS CHECKS WERE GOOD. - [SDR CHQA20120527182](https://openairdocs.org/sdr/CHQA20120527182), May 27, 2012: SHEAR TIE. CORRODED. DURING HEAVY MAINTENANCE, CORROSION WAS FOUND ON FRAME 65 SHEAR TIE. MAINTENANCE REPLACED THE SHEAR TIE AT FRAME 65 IN ACCORDANCE WITH ETD 2012-145-007624. - [SDR CHQA201100290](https://openairdocs.org/sdr/CHQA201100290), Jul 25, 2011: FLEX COUPLING. TORN. CREW REPORTED THAT DURING FLIGHT THE NUMBER 2 COOLING PACK WAS MAKING A LOUD RUSHING AIR NOISE. THEY ALSO REPORTED A SLIGHT BURNING SMELL FROM THE NUMBER 2 COOL - [SDR CHQA200800255](https://openairdocs.org/sdr/CHQA200800255), Dec 24, 2008: LIGHT. INOPERATIVE. CREW REPORTED A SMOKE SMELL FROM EMERGENCY ROW AROUND SEAT 10A. THE FLIGHT DIVERTED TO LEX AND LANDED WITHOUT INCIDENT. FOUND SIDEWALL LIGHT AT 10A INOPERATIVE - [SDR CHQA200800067](https://openairdocs.org/sdr/CHQA200800067), Mar 30, 2008: NOISE ATTENUATOR. MELTED. FLIGHT 6380, STL TO CVG - AFTER LEVELING OFF AT FL230, THE FLIGHT CREW NOTICED AN ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. THE AIRCRAFT DIVERTED TO IND AND L - [SDR CHQA200800047](https://openairdocs.org/sdr/CHQA200800047), Mar 6, 2008: ENGINE. LEAKING. CMH TO BOS - WHILE CLIMBING THROUGH FL190, THE CREW RECEIVED AN E1 IMPENDING OIL BYPASS MESSAGE. THE FIRST OFFICER PERFORMED THE QRH CHECKLISTS, WHILE THE CAPTA - [SDR CHQA200800002](https://openairdocs.org/sdr/CHQA200800002), Jan 2, 2008: UNKNOWN. SMOKE. CVG TO IND, ON INITIAL CLIMB AT APPROXIMATELY 1500 FEET, THE CREW RECEIVED A "LAV SMOKE" EICAS MESSAGE. THE CREW RAN THROUGH THE APPROPRIATE QRH CHECK LISTS AND - [SDR CHQA200800001](https://openairdocs.org/sdr/CHQA200800001), Jan 1, 2008: VELOCITY SENSOR. FAILED. CVG TO IND - ATTEMPTED TO RETRACT FLAPS DURING CLIMB AND RECEIVED A FLAP FAIL EICAS MESSAGE. RAN ALL APPLICABLE QRH CHECK LISTS, RETURNED TO FIELD, AND LANDED W - [SDR CHQA200700041](https://openairdocs.org/sdr/CHQA200700041), Aug 21, 2007: BALLAST. BURNED OUT. JFK TO IND JUST AFTER LIFT OFF RECEIVED THE "LAV SMOKE" WARNING. FA CHECKED FOR SMOKE OR FIRE AND NOTICED A HOT ELECTRICAL BURNING SMELL IN THE REAR OF THE CABI - [SDR CHQA200800003](https://openairdocs.org/sdr/CHQA200800003), Jan 2, 2007: SMOKE DETECTOR. MALFUNCTIONED. CVG TO IND - DURING TAKEOFF A "LAV SMOKE" EICAS MESSAGE WAS DISPLAYED AT APPROXIMATELY 1500 FEET. THE FLIGHT CREW PREPARED TO RETURN TO FIELD AND PERFORMED THE - [SDR CHQA200600066](https://openairdocs.org/sdr/CHQA200600066), May 24, 2006: PROBE. BURNED. FLIGHT 6383 - CVG-STL - WHILE ON VISUAL APPROACH AT APPROXIMATELY THE OUTER MARKER, NOTICED A HOT OR BURNING SMELL IN THE AIRCRAFT. WHILE RUNNING LANDING CHECK ## 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 20060524007919I](https://openairdocs.org/incident/20060524007919I), May 24, 2006: Emb EMB145LR (N575RP), St Louis, MO. (-23) Crew reported smoke in the cockpit, aircraft landed without incident. All passengers were deplaned on taxiway 32 through the main cabin door, no… --- 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.