# N561RP: 2002 Embraer EMB-145LR, registration cancelled 2019-09-25 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 25, 2019 - Exported to: Namibia - 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: 145447 - Year built: 2002 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: February 12, 2019 - Certificate issued: November 8, 2018 - Last registry action: November 8, 2018 - Mode S code: A72C26 - Owner when cancelled: [Alf Vi Inc](https://openairdocs.org/faa-owner/ALF%20VI%20INC) - Location: [Chicago, IL](https://openairdocs.org/faa-place/IL/Chicago) - Owner type: Corporation - Owner's area on the map: 41.8830° N, 87.6291° W: Placed by OpenAirDocs at the center of ZIP code 60602, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N561RP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=561RP - Page: https://openairdocs.org/deregistered/N561RP-2019-09-25 From the FAA registry file of November 7, 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 (57, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201507170565](https://openairdocs.org/sdr/UHLA201507170565), Jul 17, 2015: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMERGENCY LIGHT STRIP AT ROW 16 WAS FOUND TO BE INOPERATIVE. R & R IAW AMM 33-50-12. NO FURTHER DEFECTS HAVE BEEN NOTED. - [SDR UHLA2015042000273](https://openairdocs.org/sdr/UHLA2015042000273), Apr 20, 2015: SOLENOID VALVE. FAULTY. THE CREW REPORTED THAT THERE WAS A LOUD AIR NOISE FROM THE FRONT OF THE ACFT AND PRESUMED THAT THE LANDING GEAR DOORS REMAINED OPEN IN FLIGHT. THE CREW RETURNED - [SDR CHQA20140515158](https://openairdocs.org/sdr/CHQA20140515158), May 15, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CTR OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. THE FRAME WAS REPAIRED IAW SRM 51-40-02. - [SDR CHQA20140514173](https://openairdocs.org/sdr/CHQA20140514173), May 14, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LT OMEGA BEAM AT FRAME 20. THE FRAME WAS REPLACED IAW SRM 53-0010 & SRM 51-40-02. - [SDR CHQA20140514162](https://openairdocs.org/sdr/CHQA20140514162), May 14, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 59 & 60. THE BEAM WAS REPAIRED IAW ETD 2014-145-040625. - [SDR CHQA20140514157](https://openairdocs.org/sdr/CHQA20140514157), May 14, 2014: FRAME. CRACKED. DURING INSPECTION, FRAME 23 AT STRINGER 15L WAS FOUND TO BE CRACKED. FRAME 23 WAS REPAIRED IAW SRM 53-00-04. - [SDR CHQA20140512161](https://openairdocs.org/sdr/CHQA20140512161), May 12, 2014: FITTING. DAMAGED. DURING INSPECTION, THE LT AILERON PCA ROD END ATTACH FITTING ON THE AILERON OTBD ROD INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUTWARD. THE LT AILERON PCA ROD E - [SDR CHQA20150512160](https://openairdocs.org/sdr/CHQA20150512160), May 12, 2014: FITTING. DAMAGED. DURING INSPECTION, THE RT AILERON DAMPER ROD END ATTACH FITTING WAS ON THE AILERON INBD HAT BUSHING WAS FOUND TO BE MIGRATED OUT. THE FITTING WAS REPLACED IAW S - [SDR CHQA20140512159](https://openairdocs.org/sdr/CHQA20140512159), May 12, 2014: FITTING. GOUGED. DURING INSPECTION, THE LT AILERON DAMPNER ROD END FITTING WAS FOUND TO BE GOUGED ON THE INBD SIDE. THE LT AILERON DAMPNER ROD END FITTING WAS REPLACED IAW SRM 5 - [SDR CHQA20140512156](https://openairdocs.org/sdr/CHQA20140512156), May 12, 2014: HINGE FITTING. DAMAGED. DURING INSPECTION, THE RT AILERON OTBD HINGE ATTACH FITTING ON THE AILERON HAT BUSHING WAS FOUND TO BE MIGRATED & THE INBD SIDE HOLE ELONGATED. THE RT AILERON O - [SDR CHQA20140510174](https://openairdocs.org/sdr/CHQA20140510174), May 10, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE RT OMEGA BEAM REPAIR AT FRAME 23 HAS CORROSION. THE REPAIR DOUBLER WAS REPLACED IAW ETD 2014-145-041404. - [SDR CHQA20140510168](https://openairdocs.org/sdr/CHQA20140510168), May 10, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE LT OMEGA BEAM CTR FLOOR FLANGE WAS FOUND TO BE CORRODED AT FRAME 24 & FRAME 25. THE BEAM WAS REPAIRED IAW SRM 53-00-10 & 51-40-02. - [SDR CHQA20140510166](https://openairdocs.org/sdr/CHQA20140510166), May 10, 2014: ANGLE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02. - [SDR CHQA20140510165](https://openairdocs.org/sdr/CHQA20140510165), May 10, 2014: RIB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 12L. THE Z RIB & L ANGLE WERE REPLACED IAW SRM 51-40-02. - [SDR CHQA20140510164](https://openairdocs.org/sdr/CHQA20140510164), May 10, 2014: PROFILE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & MID FRAME AT STRINGER 14L. THE FRAME PROFILE WAS REPLACED IAW SRM - [SDR CHQA20140510163](https://openairdocs.org/sdr/CHQA20140510163), May 10, 2014: PROFILE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE MID FWD FRAME & STRINGER 15L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140510155](https://openairdocs.org/sdr/CHQA20140510155), May 10, 2014: FITTING. CRACKED. DURING INSPECTION, THE SHEAR CLIP AT FRAME 28 BETWEEN STRINGERS 15R & 16R WERE FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140509172](https://openairdocs.org/sdr/CHQA20140509172), May 9, 2014: PROFILE. CORRODED. DURING INSPECTION, A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STEP SUPPORT BRACKET ON THE MAIN ENTRY DOOR. THE PROFILE WAS REPLACED IAW SRM 51-40-0 - [SDR CHQA20140509171](https://openairdocs.org/sdr/CHQA20140509171), May 9, 2014: PROFILE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN ENTRY DOOR STRUCTURE AT THE AFT FRAME & STRINGER 10L. THE PROFILE WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140509169](https://openairdocs.org/sdr/CHQA20140509169), May 9, 2014: DOOR FRAME. CORRODED. DURING INSPECTION, THE MAIN ENTRY DOOR STRUCTURE AT THE MID AFT FRAME & STRINGER 14 WAS FOUND TO BE CORRODED. THE MID AFT FRAME WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20140509167](https://openairdocs.org/sdr/CHQA20140509167), May 9, 2014: PROFILE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE STRUCTURE OF THE MAIN ENTRY DOOR AT THE AFT FRAME AT STRINGER 12L. THE FRAME PROFILE WAS REPLACED IAW SRM 51-40-02 - [SDR CHQA20140509154](https://openairdocs.org/sdr/CHQA20140509154), May 9, 2014: NUT PLATE. CORRODED. DURING INSPECTION, MULTIPLE AREAS OF CORROSION WERE FOUND ON THE NUTPLATE HOLES IN THE AFT FRAME OF THE MAIN ENTRY DOOR. THE NUTPLATE WAS REPAIRED IAW ETD 2014- - [SDR CHQA20140507170](https://openairdocs.org/sdr/CHQA20140507170), May 7, 2014: DOUBLER. GOUGED. DURING INSPECTION, THE DOUBLER AT THE FWD NOSE SECTION BELOW THE EXTERNAL POWER RECEPTACLE ON THE LT SIDE AT FRAME 8 WAS FOUND TO BE GOUGED. THE DOUBLER WAS REP - [SDR CHQA20140204040](https://openairdocs.org/sdr/CHQA20140204040), Feb 4, 2014: ISIS. FAULTED. CREW REPORTED THAT DURING FLIGHT THE STANDBY ATTITUDE INDICATOR WENT BLANK & WENT TO, ATT CAGE. THE CREW RETURNED TO FIELD & LANDED WITHOUT INCIDENT.. RESET THE - [SDR CHQA20130520187](https://openairdocs.org/sdr/CHQA20130520187), May 20, 2013: STRINGER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON STRINGER 21 AT FRAME 13. THE STRINGER WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02 AND 51-20-03. - [SDR CHQA20130520186](https://openairdocs.org/sdr/CHQA20130520186), May 20, 2013: ATTACH BOLT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE FLAP POWER DRIVE UNIT ATTACH POINTS. THE ATTACH POINTS WERE REPAIRED IN ACCORDANCE WITH ETD 2013-145-010207. - [SDR CHQA20130519191](https://openairdocs.org/sdr/CHQA20130519191), May 19, 2013: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT. THE SERVICE DOOR CUT OUT WAS REPAIRED IAW SRM 53-21-02. - [SDR CHQA20130519190](https://openairdocs.org/sdr/CHQA20130519190), May 19, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM AT THE SCREW HOLE FRAME 23. THE FRAME WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-010149. - [SDR CHQA20130519189](https://openairdocs.org/sdr/CHQA20130519189), May 19, 2013: FLOOR SUPPORT. CORRODED. DURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OUTBOARD OMEGA BEAM SUPPORT BETWEEN FRAMES 47 AND 48. THE OMEGA BEAM SUPPORT WAS REPLACED IN ACCORDANCE WITH SR - [SDR CHQA20130519188](https://openairdocs.org/sdr/CHQA20130519188), May 19, 2013: DOUBLER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON A REPAIR DOUBLER ON THE INBOARD SIDE OF THE LEFT OMEGA BEAM AT FRAME 20. THE DOUBLER WAS REPLACED IN ACCORDANCE WITH 5 - [SDR CHQA20130213049](https://openairdocs.org/sdr/CHQA20130213049), Feb 14, 2013: ELECTRONIC UNIT. FAULTY. CREW REPORTED THAT AFTER TAKEOFF, DURING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR DID NOT SHOW UP AND LOCKED. THE OTHER GEAR HAD GREEN INDICATIONS AND SHOWE - [SDR CHQA20120423131](https://openairdocs.org/sdr/CHQA20120423131), Apr 23, 2012: DUCT. CRACKED. CREW REPORTED, RECEIVED A BLEED 1 LEAK MESSAGE AFTER TAKEOFF. THE CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE T-DUCT JUST BELOW JOINT 17 - [SDR CHQA20120229068](https://openairdocs.org/sdr/CHQA20120229068), Feb 29, 2012: VALVE. INOPERATIVE. CREW REPORTED THAT THERE WAS AN ELECTRICAL BURNING SMELL IN THE COCKPIT UPON ARRIVING AT THE GATE. MAINTENANCE REPLACED THE GASPER VALVE FOR THE LEFT ELECTRICAL - [SDR CHQA201100419](https://openairdocs.org/sdr/CHQA201100419), Oct 26, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE NUMBER 3 FLOOR PROXIMITY EMERGENCY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 3 FLOOR PROXIMITY EMERGENCY L - [SDR CHQA201100366](https://openairdocs.org/sdr/CHQA201100366), Sep 9, 2011: WARNING SYSTEM. FALSE ACTIVATION. CREW REPORTED THAT DURING CLIMB RECEIVED A BLEED 1 LEAK MESSAGE. THE CREW RETURNED TO KDCA AND LANDED WITHOUT INCIDENT. MAINTENANCE EXPOSED ALL JOINTS IN THE BL - [SDR CHQA201100199](https://openairdocs.org/sdr/CHQA201100199), May 30, 2011: WARNING SYSTEM. FALSE ACTIVATION. FLIGHT CREW REPORTED THAT WHILE CLIMBING THROUGH 9,000FT, THE HAD A BLEED 1 LEAK MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND AN EMERGENCY WAS DECLARED. THE AIRCR - [SDR CHQA201100179](https://openairdocs.org/sdr/CHQA201100179), May 5, 2011: REINFORCEMENT. CORRODED. DURING INSPECTION, THE TOILET CUP ON THE LOWER AFT FUSELAGE WAS FOUND CORRODED. THE TOILET CUP WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201100149](https://openairdocs.org/sdr/CHQA201100149), Apr 22, 2011: BATTERY PACK. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY WITH NO FURTHER DEFECTS NOT - [SDR CHQA201100126](https://openairdocs.org/sdr/CHQA201100126), Apr 1, 2011: OUTFLOW VALVE. INOPERATIVE. CREW REPORTED THAT DURING DESCENT FROM FL320 TO FL240 CABIN ALTITUDE STARTED INCREASING. THE CREW DECLARED AN EMERGENCY AND INCREASED THERE DESCENT RATE. THE AI - [SDR CHQA201000211](https://openairdocs.org/sdr/CHQA201000211), Nov 18, 2010: WARNING SYSTEM. FALSE ACTIVATION. DURING GEAR EXTENSION ON FINAL APPROACH, THE CREW REPORTED A BRAKE DEGRADED MESSAGE ON EICAS. THE QRH WAS FOLLOWED AND THE CREW DECLARED AN EMERGENCY AND THE AI - [SDR CHQA201000207](https://openairdocs.org/sdr/CHQA201000207), Oct 28, 2010: LIGHT. INOPERATIVE. DURING INSPECTION THE LEFT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. THE BULB WAS REPLACED WITH NO FURTHER DEFECTS NOTED. - [SDR CHQA201000138](https://openairdocs.org/sdr/CHQA201000138), Jul 9, 2010: UNKNOWN. MALFUNCTIONED. CREW REPORTED THAT THE CABIN FAILED TO PRESSURIZE AFTER TAKEOFF. CREW ATTEMPTED MANUAL AND AUTO MODES WITH NO SUCCESS, AIRCRAFT RETURNED TO CMH AND LANDED WITHO - [SDR CHQA201000068](https://openairdocs.org/sdr/CHQA201000068), Mar 30, 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 CHQA201000040](https://openairdocs.org/sdr/CHQA201000040), Feb 17, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY PACK PER AMM 33-50-04. OPS CHECKS - [SDR CHQA200900260](https://openairdocs.org/sdr/CHQA200900260), Dec 9, 2009: LIGHT. INOPERATIVE. DURING INSPECTION THE NR 2 EMERGENCY LIGHT FLOOR STRIP WAS FOUND TO BE INOP. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT FLOOR STRIP AND THE EMERGENCY LIGHTS - [SDR CHQA200900242](https://openairdocs.org/sdr/CHQA200900242), Nov 8, 2009: WIRE. BROKEN. DURING INSPECTION THE NR 4 FLOOR PROXIMITY LIGHT STRIP WAS FOUND TO HAVE A BROKEN WIRE. MAINTENANCE REPLACED THE #4 PROXIMITY LIGHT STRIP IAW EMB 145 AMM 32-50- - [SDR CHQA200900140](https://openairdocs.org/sdr/CHQA200900140), Jun 11, 2009: PROXIMITY SENSOR. CRACKED. FLIGHT 6094, CMH TO BOS. UPON GEAR RETRACTION THE CREW RECEIVED A LG AIR/GND FAIL EICAS MESSAGE. THIRTY SECONDS LATER RECEIVED A TAKEOFF FLAPS MESSAGE WITH NO O - [SDR CHQA200900098](https://openairdocs.org/sdr/CHQA200900098), Apr 3, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION THE LEFT-HAND OVER WING EMERGENCY LIGHT WAS INOP WHEN TESTED. THE NR 4 EMERGENCY LIGHT POWER SUPPLY WAS REPLACED AND THE SYSTEM OPERATED NORMA - [SDR CHQA200900077](https://openairdocs.org/sdr/CHQA200900077), Mar 12, 2009: PROXIMITY SWITCH. FAULTY. FLIGHT 6115, CVG TO CMH, CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER TAKEOFF. THE CREW DID NOT ATTEMPT TO RETRACT THE LANDING GEAR AND RETURNED T - [SDR CHQA200900052](https://openairdocs.org/sdr/CHQA200900052), Feb 11, 2009: BATTERY PACK. INOPERATIVE. DURING INSPECTION THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOP WHEN TESTED. THE NR 4 EMERGENCY BATTERY WAS REPLACED ALONG WITH THE INVERTER AND THE All 57: https://openairdocs.org/deregistered/N561RP-2019-09-25/reports.md --- 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.