# N564RP: 2002 Embraer EMB-145LR, registration cancelled 2018-06-20 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 20, 2018 - Exported to: Mexico - 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: 145524 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 21, 2002 - Certificate issued: June 13, 2018 - Last registry action: June 13, 2018 - Mode S code: A7374B - Owner when cancelled: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%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/N564RP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=564RP - Page: https://openairdocs.org/deregistered/N564RP-2018-06-20 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 (44) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201504290333](https://openairdocs.org/sdr/UHLA201504290333), Apr 29, 2015: HYDRAULIC SYSTEM. LOW. THE CREW REPORTED THAT THEY RECEIVED A "HYDRAULIC SYSTEM 1 LOW QUANTITY" MESSAGE AFTER TAKEOFF. THE ACFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENA - [SDR UHLA2015041300249](https://openairdocs.org/sdr/UHLA2015041300249), Apr 13, 2015: WARNING LIGHT. ILLUMINATED. THE CREW REPORTED THAT THEY RECEIVED A PITOT 2 INOPERATIVE MESSAGE IN FLIGHT FOLLOWED BY SMOKE IN THE COCKPIT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT - [SDR CHQA20140914273](https://openairdocs.org/sdr/CHQA20140914273), Sep 14, 2014: SKIN. GOUGED. DURING HEAVY MX A PERMANENT REPAIR OF THE BAGGAGE DOOR SKIN NEAR THE FWD VENT FLAP WAS REPAIRED IAW ETD2013-145-040730. - [SDR CHQA20140914272](https://openairdocs.org/sdr/CHQA20140914272), Sep 14, 2014: GUSSET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA GUSSET AT FRAME 16 TO 19. THE GUSSET WAS REPAIRED IAW ETD2014-145-077627A. - [SDR CHQA20140209046](https://openairdocs.org/sdr/CHQA20140209046), Feb 9, 2014: CONVERTER. INOPERATIVE. DURING INSPECTION, THE FWD FACING OVERWING EXIT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 6 LIGHT CONVERTER & ALL OPERATIONS CHECKED WERE GOO - [SDR CHQA20140209045](https://openairdocs.org/sdr/CHQA20140209045), Feb 9, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE RT EXTERNAL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY & ALL OPERATIONS CHECKED WERE GOOD. - [SDR CHQA20140209044](https://openairdocs.org/sdr/CHQA20140209044), Feb 9, 2014: LIGHT. INOPERATIVE. DURING INSPECTION, THE LT EXTERNAL OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE LIGHT ASSEMBLY & ALL OPERATIONS CHECKED GOOD. - [SDR CHQA20130904338](https://openairdocs.org/sdr/CHQA20130904338), Sep 4, 2013: LIGHT. INOPERATIVE. DURING INSPECTION, AN OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED AN OVERWING EMERGENCY LIGHT, OPS CHECKED GOOD. - [SDR CHQA20130724187](https://openairdocs.org/sdr/CHQA20130724187), Jul 24, 2013: CONTROL LEVER. INOPERATIVE. CREW REPORTED THAT AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AND THAT THE LANDING GEAR HANDLE WAS STUCK IN DOWN POSITION. THE CREW RETURNED TO FIELD AND - [SDR CHQA20130724186](https://openairdocs.org/sdr/CHQA20130724186), Jul 24, 2013: UNKNOWN. UNKNOWN. CREW REPORTED AN ABNORMALLY LOUD NOISE FROM THE NOSE AREA OF THE ACFT AFTER GEAR RETRACTION. NOISE PRESENT FOR REMAINDER OF FLIGHT. ALL 3 LANDING GEAR SHOWED UP - [SDR CHQA20130623250](https://openairdocs.org/sdr/CHQA20130623250), Jun 23, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAME 20. THE BEAM WAS REPAIRED IAW ETD 2013-145-012966. - [SDR CHQA20130623244](https://openairdocs.org/sdr/CHQA20130623244), Jun 23, 2013: SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT OTBD SEAT TRACK SUPPORT BEAM AT FRAME 50. THE SEAT TRACK SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130620249](https://openairdocs.org/sdr/CHQA20130620249), Jun 20, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAMES 24 AND 25. THE BEAM WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20130620248](https://openairdocs.org/sdr/CHQA20130620248), Jun 20, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR DOUBLER ON THE LT OMEGA BEAM AT FRAME 20 AT THE CROSSMEMBER. THE DOUBLER WAS REPLACED IAW SRM 53-00-10 AND - [SDR CHQA20130620247](https://openairdocs.org/sdr/CHQA20130620247), Jun 20, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT OMEGA BEAM AT FRAME 23. THE BEAM WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20130620246](https://openairdocs.org/sdr/CHQA20130620246), Jun 20, 2013: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA A CROSSMEMBER AT FRAME 29. THE LT OMEGA BEAM WAS REPAIRED IAW SRM 53-00-10. - [SDR CHQA20130620245](https://openairdocs.org/sdr/CHQA20130620245), Jun 20, 2013: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE FWD SCREW HOLES ON THE SERVICE DOOR THRESHOLD BEAM. THE BEAM WAS REPAIRED IAW SRM 53-21-02. - [SDR CHQA20120712211](https://openairdocs.org/sdr/CHQA20120712211), Jul 12, 2012: STRUT. LEAKING. CREW REPORTED THAT AFTER TAKEOFF, LANDING GEAR LEVER WOULD NOT MOVE AND THAT THEY RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE. RETURNED TO FIELD AND LANDED - [SDR CHQA201100476](https://openairdocs.org/sdr/CHQA201100476), Dec 8, 2011: MODULE. MALFUNCTIONED. CREW REPORTED THAT AFTER TAKEOFF, AT APPROXIMATELY 700FT AGL, THE CABIN ALTITUDE ON THE EICAS WENT TO DASHES. THE CREW DECIDED TO RETURN TO KDTW. DURING THE RET - [SDR CHQA201100450](https://openairdocs.org/sdr/CHQA201100450), Nov 16, 2011: SCREW. BROKEN. THE FIRST OFFICER REPORTED THAT THE LAVATORY DOOR WAS STUCK CLOSED WITH THE CAPTAIN INSIDE DURING FLIGHT. AN EMERGENCY WAS DECLARED WHEN A PASSENGER APPROACHED - [SDR CHQA201100420](https://openairdocs.org/sdr/CHQA201100420), Oct 26, 2011: PRESSURE SWITCH. BROKEN. CREW REPORTED, RECEIVED A BLEED 2 OVERTEMP MESSAGE DURING CLIMB. THE CREW DIVERTED TO KCMH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT ENGINE HIGH - [SDR CHQA201100277](https://openairdocs.org/sdr/CHQA201100277), Jul 10, 2011: BUTTSTRAP. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER BUTT STRAP BETWEEN FRAMES 57-61. MAINTENANCE REPLACED THE CENTER BUTT STRAP BETWEEN FRAMES 57-61 IN ACCORDA - [SDR CHQA201100276](https://openairdocs.org/sdr/CHQA201100276), Jul 8, 2011: FRAME. CRACKED. DURING INSPECTION, FRAME 10 LEFT SIDE WAS FOUND TO BE CRACKED ON THE UPPER INBOARD SIDE. MAINTENANCE REMOVED THE CRACKED FRAME AND INSTALLED THE NEW FRAME IN AC - [SDR CHQA201100279](https://openairdocs.org/sdr/CHQA201100279), Jul 7, 2011: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR FRAME 22 BELOW THE LOWER DOOR STOP. MAINTENANCE REPLACED THE SERVICE DOOR FRAME 22 IN ACCORDANCE WITH - [SDR CHQA201100278](https://openairdocs.org/sdr/CHQA201100278), Jul 7, 2011: FLOORBEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER FLOORBEAM AT FRAME 15. MAINTENANCE REPLACED THE CENTER FLOORBEAM GUSSET AT FRAME 15 IN ACCORDANCE WITH SRM - [SDR CHQA201100177](https://openairdocs.org/sdr/CHQA201100177), May 15, 2011: LIGHT. INOPERATIVE. DURING POWER-UP THE CREW REPORTED THAT WHEN THE EMERGENCY LIGHT SWITCH WAS MOVED TO THE ARMED POSITION, HALF OF THE EMERGENCY LIGHTS WOULD TURN ON. MAINTENANCE - [SDR CHQA201100139](https://openairdocs.org/sdr/CHQA201100139), Apr 17, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, MAINTENANCE FOUND THE FORWARD OVERWING EMERGENCY LIGHT AT ROW 12 TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY EXIT - [SDR CHQA201100130](https://openairdocs.org/sdr/CHQA201100130), Apr 10, 2011: O-RING. TORN. CREW REPORTED A BLEED 1 LEAK MESSAGE ON CLIMBOUT WITH A BLEED 1 CLOSED MESSAGE AT THE SAME TIME. THE MESSAGE REMAINED ON UNTIL CROSS BLEED WAS CLOSED AND BLEED - [SDR CHQA201000223](https://openairdocs.org/sdr/CHQA201000223), Dec 3, 2010: BATTERY. DISCHARGED. DURING INSPECTION BOTH EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS N - [SDR CHQA201000132](https://openairdocs.org/sdr/CHQA201000132), Jun 29, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION, BOTH OVERWING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-50-04 WITH NO FURTHER - [SDR CHQA201000110](https://openairdocs.org/sdr/CHQA201000110), Jun 2, 2010: ENGINE. LEAKING. ON FINAL APPROACH IN TO MEM BETWEEN 1000FT AND 500FT THE CREW NOTICED A RAPID LOSS OF OIL PRESSURE ON E2 ALONG WITH DECREASING N1 INDICATIONS. THEN REPORTED AN - [SDR CHQA200900190](https://openairdocs.org/sdr/CHQA200900190), Sep 1, 2009: BATTERY. DISCHARGED. DURING MAINTENANCE THE NR 4 EMERGENCY BATTERY WAS FOUND TO BE DISCHARGED. IT WAS REPLACED IAW 145AMM 33-50-04 AND THE OPERATIONAL CHECKS WERE GOOD. - [SDR CHQA200900189](https://openairdocs.org/sdr/CHQA200900189), Sep 1, 2009: LIGHT. DISCONNECTED. DURING MAINTENANCE THE AFT EMERGENCY FLOOR LIGHT STRIP BETWEEN ROWS 17 & 18 WAS FOUND TO BE INOPERATIVE. THE LIGHT STRIP WAS THEN FOUND TO BE UNPLUGGED. THE STR - [SDR CHQA200900181](https://openairdocs.org/sdr/CHQA200900181), Aug 17, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA200900163](https://openairdocs.org/sdr/CHQA200900163), Jul 23, 2009: PROXIMITY SWITCH. FAULTY. FLIGHT 9000, CMH TO YQB. THE CREW REPORTED THAT AFTER TAKEOFF, THE LEFT MAIN LANDING GEAR WOULD NOT RETRACT AND HAD LANDING GEAR LEVER DISAGREE MESSAGE. THE FLI - [SDR CHQA200900013](https://openairdocs.org/sdr/CHQA200900013), Jan 10, 2009: BATTERY PACK. INOPERATIVE. DURING INSP THE LT AND RT AFT EMERGENCY WING COURTESY LIGHTS WERE INOPERATIVE. THE NR 3 EMERGENCY LIGHT BATTERY PACK WAS REPLACED AND THE SYS OPERATED NORMALLY. - [SDR CHQA200900011](https://openairdocs.org/sdr/CHQA200900011), Jan 6, 2009: BATTERY PACK. INOPERATIVE. DURING INSP, BOTH OF THE OVER-WING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHTS OPERATED N - [SDR CHQA200800253](https://openairdocs.org/sdr/CHQA200800253), Dec 20, 2008: BATTERY PACK. DISCHARGED. DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE NR 4 EMERGENCY LIGHT BATTERY PACK WAS REPLACED AND THE EMERGENCY LIGHTS OPERAT - [SDR CHQA200800235](https://openairdocs.org/sdr/CHQA200800235), Dec 2, 2008: BATTERY PACK. DISCHARGED. THE OVERWING EMERGENCY LIGHTS DO NOT OPERATE WHEN TESTED. THE EMERGENCY BATTERY WAS REPLACED IAW EMB 145 AMM 33-50-04 AND THE EMERGENCY LIGHTS OPERATED NORMALLY - [SDR CHQA200800213](https://openairdocs.org/sdr/CHQA200800213), Oct 28, 2008: BATTERY PACK. DISCHARGED. DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP WHEN TESTED. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED, AND THE EMERGENCY LIGHTS OPERA - [SDR CHQA200800175](https://openairdocs.org/sdr/CHQA200800175), Sep 7, 2008: SEAL. MISSING. FLIGHT 6142, CMH TO JFK. DURING CRUISE AT FL330, THE CABIN ALTITUDE RAPIDLY ROSE TO APPROXIMATELY 12,000FT. THE FLIGHT CREW FOLLOWED THE QRH CHECKLISTS AND DESC - [SDR CHQA200800125](https://openairdocs.org/sdr/CHQA200800125), Jun 25, 2008: BATTERY. DISCHARGED. MAINTENANCE FOUND THAT THE OVERWING EMERGENCY LIGHTS INOP DURING TEST. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE OVERWING LIGHTS OPERATED NORMALLY. - [SDR CHQA200800018](https://openairdocs.org/sdr/CHQA200800018), Jan 30, 2008: ENGINE. SMOKE. JFK TO BUF - AT APPROXIMATELY 500FT AGL, THE FLIGHT CREW NOTICED SMOKE IN THE COCKPIT. OXYGEN MASKS WERE DONNED AND THE AIRCRAFT WAS PREPARED TO RETURN TO FIELD - [SDR CHQA200600041](https://openairdocs.org/sdr/CHQA200600041), Apr 5, 2006: BULB. BURNED OUT. EMERGENCY LIGHT AT EXTERIOR OVERWING (AFT) IS INOPERATIVE. RELAMPED RIGHT HAND OVERWING EMERGENCY LIGHT AS PER MM 33-50-07. OPS CHECK GOOD. ## 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 20150413003509I](https://openairdocs.org/incident/20150413003509I), Apr 13, 2015: Embraer EMB-145LR (N564RP), Flushing, NY, Minor damage. On descent to lga, aircraft had smoke/burn smell in cabin and cockpit. Crew declared emergency landing, landed, stopped aircraft on taxiway, shutdown aircraft… --- 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.