# N572RP: 2004 Embraer EMB-145LR, registration cancelled 2019-10-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 18, 2019 - Exported to: Colombia - Status when cancelled: First renewal notice - 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: 14500828 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 22, 2004 - Certificate issued: January 12, 2017 - Last registry action: May 8, 2018 - Mode S code: A7575C - 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/N572RP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=572RP - Page: https://openairdocs.org/deregistered/N572RP-2019-10-18 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 Embraer EMB-145LR: https://openairdocs.org/model/embraer-emb-145lr.md ## Service difficulty reports (43) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CHQA20140501136](https://openairdocs.org/sdr/CHQA20140501136), May 1, 2014: FITTING. CORRODED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CRACKED AT STRINGERS 18L & 19L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140427142](https://openairdocs.org/sdr/CHQA20140427142), Apr 27, 2014: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FWD PAX DOOR STRUCTURE. THE LOWER FWD PAX DOOR STRUCTURE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140425132](https://openairdocs.org/sdr/CHQA20140425132), Apr 25, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140425131](https://openairdocs.org/sdr/CHQA20140425131), Apr 25, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140423144](https://openairdocs.org/sdr/CHQA20140423144), Apr 23, 2014: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER AFT CORNER OF THE MAIN ENTRY DOOR. THE LOWER AFT CORNER STRUCTURE OF THE LOWER MAIN E - [SDR CHQA20140423143](https://openairdocs.org/sdr/CHQA20140423143), Apr 23, 2014: REINFORCEMENT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE DOOR STOP REINFORCEMENT INSIDE OF THE FWD FRAME OF THE MAIN ENTRY DOOR. THE DOOR STOP REINFORCEMENT WAS REPLACED I - [SDR CHQA20140423141](https://openairdocs.org/sdr/CHQA20140423141), Apr 23, 2014: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND & A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT ON THE MAIN ENTRY DOOR. THE STRUCTURE UNDER THE M - [SDR CHQA20140423140](https://openairdocs.org/sdr/CHQA20140423140), Apr 23, 2014: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR. THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAI - [SDR CHQA20140423139](https://openairdocs.org/sdr/CHQA20140423139), Apr 23, 2014: REINFORCEMENT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AROUND THE THE REINFORCEMENT FOR THE BOTTOM DOOR STOP INSIDE THE AFT STRUCTURE OF THE MAIN ENTRY DOOR. THE DOOR STOP WAS - [SDR CHQA20140423138](https://openairdocs.org/sdr/CHQA20140423138), Apr 23, 2014: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE CARGO DOOR FRAME JUST BELOW THE DOOR BUMPER PLATE. THE FRAME WAS REPAIRED IAW ETD 2014-145-034902. - [SDR CHQA20140423137](https://openairdocs.org/sdr/CHQA20140423137), Apr 23, 2014: FITTING. DAMAGED. DURING INSPECTION, THE LT AILERON ACTUATOR ATTACH LUG OTBD HAT BUSHING WAS FOUND TO BE MIGRATING AWAY FROM THE LUG. THE LT AILERON PCA FITTING WAS REPLACED IAW - [SDR CHQA20140423133](https://openairdocs.org/sdr/CHQA20140423133), Apr 23, 2014: DOOR. CHAFED. DURING INSPECTION, A CHAFE WAS FOUND ON THE INNER AFT FACE OF THE MAIN ENTRY DOOR FOLDING FLAP. THE CHAFE WAS REPAIRED IAW ETD 2014-145-034319. - [SDR CHQA20140422135](https://openairdocs.org/sdr/CHQA20140422135), Apr 22, 2014: SUPPORT. CORRODED. DURING INSPECTION, THE LT SIDEWALL SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED AT FRAME 45. THE SEAT TRACK SUPPORT WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140422134](https://openairdocs.org/sdr/CHQA20140422134), Apr 22, 2014: DOUBLER. CORRODED. DURING INSPECTION, A PREVIOUS REPAIR DOUBLER ON THE LT FWD OMEGA BEAM FWD CAP AT FRAME 20 WAS FOUND TO BE CORRODED. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-4 - [SDR CHQA20131206442](https://openairdocs.org/sdr/CHQA20131206442), Dec 6, 2013: SMOKE DETECTOR. FALSE ACTIVATION. CREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE MESSAGE ON CLIMB OUT. THE CREW FURTHER REPORTED NO VISIBLE SMOKE. THE SMELL OF DE-ICING FLUID WAS REPORTED AS - [SDR CHQA20130831331](https://openairdocs.org/sdr/CHQA20130831331), Aug 31, 2013: LIGHT. INOPERATIVE. DURING INSPECTION, THE RT OVERWING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MX REPLACED THE RT OVERWING LIGHT ASSY. OPS CHECKED GOOD WITH NO FURTHER DE - [SDR CHQA20130708261](https://openairdocs.org/sdr/CHQA20130708261), Jul 8, 2013: CONTROL VALVE. FAULTY. CREW REPORTED THAT ON GEAR EXTENSION, RECEIVED A BRAKE DEGRADED MESSAGE ON THE EICAS DISPLAY. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX REPLACED THE - [SDR CHQA20130405105](https://openairdocs.org/sdr/CHQA20130405105), Apr 5, 2013: SWITCH. DIRTY. CREW REPORTED THAT THEY RECEIVED A BAGGAGE DOOR INDICATION IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED THE BAGGAGE D - [SDR CHQA20130117020](https://openairdocs.org/sdr/CHQA20130117020), Jan 17, 2013: TIRE. SEPARATED. CREW REPORTED DURING TAKEOFF THE RIGHT INBOARD MAIN LANDING GEAR TIRE SEPARATED. THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENAN - [SDR CHQA20120727247](https://openairdocs.org/sdr/CHQA20120727247), Jul 27, 2012: SUPPORT FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AN - [SDR CHQA20120727246](https://openairdocs.org/sdr/CHQA20120727246), Jul 27, 2012: SUPPORT FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR FORWARD AND AFT STEP SUPPORT FITTING AT THE STEP BUSHING AREAS. MAINTENANCE REPLACED THE FORWARD AN - [SDR CHQA20120726242](https://openairdocs.org/sdr/CHQA20120726242), Jul 26, 2012: SHEAR PLATE. CRACKED. DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR FOOT FRAME 68 BETWEEN STRINGER 6L-7L. MAINTENANCE REPLACED THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 6L AND - [SDR CHQA20120726241](https://openairdocs.org/sdr/CHQA20120726241), Jul 26, 2012: SHEAR PLATE. CRACKED. DURING INSPECTION A CRACK WAS FOUND IN SHEAR FOOT FRAME 61 BETWEEN STRINGER 6R-7R. MAINTENANCE REPLACED THE SHEAR FOOT AT FRAME 61. - [SDR CHQA20120725240](https://openairdocs.org/sdr/CHQA20120725240), Jul 25, 2012: DOOR FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND IN THE MAIN PASSENGER LOWER DOOR FRAME AT THE AFT STOP, SECOND FROM THE BOTTOM, WITH THE DOOR IN THE OPEN POSITION. MAINTEN - [SDR CHQA201100389](https://openairdocs.org/sdr/CHQA201100389), Sep 27, 2011: WIRE HARNESS. DEFECTIVE. CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE CREW FOLLOWED ALL CHECKLISTS AND RETURNED TO KDCA. THE AIRCRAFT LANDED WITHOUT INCIDENT - [SDR CHQA201100367](https://openairdocs.org/sdr/CHQA201100367), Sep 10, 2011: PROXIMITY SWITCH. DIRTY. CREW REPORTED, COULD NOT LIFT THE LANDING GEAR LEVER AND THE LANDING GEAR WOULD NOT RETRACT. RETURNED TO KIAD AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED A - [SDR CHQA201100344](https://openairdocs.org/sdr/CHQA201100344), Aug 15, 2011: SKIN. SCRATCHED. DURING INSPECTION, SEVERAL SCRATCHES WERE FOUND ON THE FUSELAGE UPPER SKIN UNDERNEATH ADF ANTENNA NUMBER 1 AND NUMBER 2. MAINTENANCE REPAIRED THE SCRATCHES ON T - [SDR CHQA201100347](https://openairdocs.org/sdr/CHQA201100347), Aug 11, 2011: STOP FITTING. DAMAGED. DURING INSPECTION, THE PASSENGER DOOR STOP WAS FOUND TO BE DAMAGED. MAINTENANCE BLENDED THE PASSENGER DOOR STOPS IN ACCORDANCE WITH SRM 53-21-15. A HIGH FREQUEN - [SDR CHQA201100346](https://openairdocs.org/sdr/CHQA201100346), Aug 10, 2011: BONDING STRAP. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT AND RIGHT AILERON UPPER SHROUD BONDING STRAP. MAINTENANCE REWORKED THE LEFT AND RIGHT AILERON UPPER SHROUD BO - [SDR CHQA201100345](https://openairdocs.org/sdr/CHQA201100345), Aug 10, 2011: SKIN. DAMAGED. DURING INSPECTION, THE SKIN WAS FOUND TO BE DAMAGED AND AN ANCHOR NUT MISSING ON RUDDER II, BETWEEN X27083 AND X27621 AS WELL AS BETWEEN ZV1932 AND ZV2277. MAIN - [SDR CHQA201100343](https://openairdocs.org/sdr/CHQA201100343), Aug 10, 2011: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MIDDLE BEAM AT Y0.0. MAINTENANCE REPLACED THE MIDDLE BEAM AT Y0.0 IN ACCORDANCE WITH SRM 51-40-02. - [SDR CHQA201100342](https://openairdocs.org/sdr/CHQA201100342), Aug 10, 2011: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PASSENGER DOOR LOWER STRUCTURE FORWARD AND AFT U-SHAPE. MAINTENANCE REPLACED THE FORWARD (PN:145-24131-009) AND AF - [SDR CHQA201100340](https://openairdocs.org/sdr/CHQA201100340), Aug 10, 2011: BEAM. CORRODED. DURING INSPECTION, AN EXISTING REPAIR ON THE LEFT BEAM Y479.0 AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT BEAM, Y479.0 AT FRAME 20 IN AC - [SDR CHQA201100314](https://openairdocs.org/sdr/CHQA201100314), Aug 10, 2011: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 15L AND 16L. MAINTENANCE REPAIRED THE FORWARD FRAME OF THE CARGO - [SDR CHQA201100313](https://openairdocs.org/sdr/CHQA201100313), Aug 10, 2011: SHEAR PLATE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE AFT AND FORWARD L-SHAPE SHEAR CLIP. MAINTENANCE REPAIRED THE FORWARD AND AFT L-SHAPE SHEAR CLIPS IN ACCORDANCE WIT - [SDR CHQA201100348](https://openairdocs.org/sdr/CHQA201100348), Aug 9, 2011: SKIN. DENTED. DURING C-CHECK, A DENT, FORWARD OF THE SERVICE DOOR, ON THE CENTER FUSELAGE I, BETWEEN STRINGERS 12R AND 13R, WAS REPAIRED. THE DENT WAS PREVIOUSLY DEFERRED (DM - [SDR CHQA201100026](https://openairdocs.org/sdr/CHQA201100026), Jan 26, 2011: UNKNOWN. CONTAMINATED. PRIOR TO TAKEOFF THE AIRCRAFT WAS DE-ICED, AND AT APPROXIMATELY 500FT ON TAKEOFF, THE FLIGHT ATTENDANT REPORTED HAZE IN THE CABIN THAT SMELLED LIKE GLYCOL. THER - [SDR CHQA200900202](https://openairdocs.org/sdr/CHQA200900202), Sep 8, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION WHILE TESTING EMERGENCY LIGHT SYSTEM THE OVERWING EMERGENCY LIGHTS WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTER - [SDR CHQA200900061](https://openairdocs.org/sdr/CHQA200900061), Feb 20, 2009: STRUT. UNDERSERVICED. UPON GEAR RETRACTION THE CREW RECEIVED A L/G AIR/GND FAIL MESSAGE ON THE EICAS. FOLLOWED SHORTLY BY E1-2 REVERSE DISAGREE MESSAGE. THE CREW RETURNED TO THE FIEL - [SDR CHQA200700090](https://openairdocs.org/sdr/CHQA200700090), Dec 5, 2007: WARNING MESSAGE. FALSE ACTIVATION. IND TO CVG - DURING CLIMB-OUT OF IND IN ICING CONDITIONS THE CREW RECEIVED A BLEED 1 LEAK EICAS MESSAGE WITH LEAK ILLUMINATED ON THE ENGINE BLEED VALVE SELECTOR - [SDR CHQA200700010](https://openairdocs.org/sdr/CHQA200700010), Apr 7, 2007: O-RING. BROKEN. FLIGHT 6218 - CVG-CMH - ON DESCENT INTO CMH, RECEIVED NR 2 ENGINE BLEED LEAK. SHUT OFF ENGINE PER QRH. INTERMITTENTLY IN AND OUT OF ICING CONDITIONS, SHUTTING O - [SDR CHQA200600005](https://openairdocs.org/sdr/CHQA200600005), Jan 6, 2006: BULB. MISSING. FLOOR PROXIMITY LIGHT STRIP MISSING. INSTALLED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 MM 33-50-12. - [SDR CHQA200500049](https://openairdocs.org/sdr/CHQA200500049), Mar 9, 2005: LIGHT. INOPERATIVE. AFT EMERGENCY FLOOR PROXIMITY LIGHT STRIP IS INOP. REMOVED AND REPLACED FLOOR PROXIMITY LIGHT STRIP IAW EMB 145 AMM 33-50-12-4. OPS CHECK GOOD. ## NTSB investigations (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA15FA004](https://openairdocs.org/ntsb/DCA15FA004), Oct 5, 2014: Embraer EMB 145LR (N572RP), Jamaica, NY, substantial damage. Probable cause: The A340 captain's failure to maintain adequate clearance between his wing and the tail of the EMB-145. --- 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.