# N563RP: Embraer EMB-145LR, registration cancelled 2018-07-11 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 11, 2018 - Exported to: Madagascar - 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: 145509 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 23, 2002 - Certificate issued: February 26, 2018 - Last registry action: February 26, 2018 - Mode S code: A73394 - 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/N563RP - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=563RP - Page: https://openairdocs.org/deregistered/N563RP-2018-07-11 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 (39) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR UHLA201512210838](https://openairdocs.org/sdr/UHLA201512210838), Dec 21, 2015: ARM. FAILED. THE MAIN ENTRY DOOR WAS UNABLE TO BE OPENED FROM THE EXTERIOR AND MAINTENANCE FOUND THE LT HINGE AT THE BASE OF THE DOOR INOPERATIVE. MAINTENANCE R & R THE RT M - [SDR UHLA201510230774](https://openairdocs.org/sdr/UHLA201510230774), Oct 23, 2015: STEP. BROKEN. THE MAIN ENTRY DOOR STEPS WERE FOUND TO BE BROKEN. MAINTENANCE ADJUSTED THE SPRINGS ON THE MAIN ENTRY DOOR STEPS IAW AMM 52-10-01 AND ALL OPS CHECKS WERE GOOD. - [SDR UHLA201506120495](https://openairdocs.org/sdr/UHLA201506120495), Jun 12, 2015: SKIN. DENTED. DURING INSPECTION, THE BAGGAGE COMPARTMENT DOOR WAS FOUND TO BE DENTED. THE DENT WAS REPAIRED IAW SRM 52-30-01. - [SDR UHLA201506050490](https://openairdocs.org/sdr/UHLA201506050490), Jun 5, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE UPRIGHT AT FRAME 20 ON THE LT OMEGA BEAM. THE STANTION WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506040489](https://openairdocs.org/sdr/UHLA201506040489), Jun 4, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT FRAMES 20-23. THE OMEGA BEAM WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506010494](https://openairdocs.org/sdr/UHLA201506010494), Jun 1, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT THE CAPTAIN'S OTBD FLOOR SILL AT FRAMES 09-12. THE CORROSION WAS REPAIRED IAW ETD 2015-145-053918A. - [SDR UHLA201506010491](https://openairdocs.org/sdr/UHLA201506010491), Jun 1, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CAPTAIN'S INBD SEAT TRACK FLOOR GUSSET AT FRAME 08-09. THE CORROSION WAS REPAIRED IAW ETD 2015-145-053918. - [SDR UHLA201506010488](https://openairdocs.org/sdr/UHLA201506010488), Jun 1, 2015: BUSHING. MIGRATED. DURING INSPECTION, THE RT AILERON DAMPER ATTACH FITTING, OTBD HAT BUSHING WAS FOUND TO BE MIGRATED AND GOUGED. THE FITTING WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506010487](https://openairdocs.org/sdr/UHLA201506010487), Jun 1, 2015: BUSHING. MIGRATED. DURING INSPECTION, THE RT AILERON PCA ATTACH FITTING HAT BUSHINGS WERE FOUND TO BE MIGRATED AND GOUGED. THE FITTING WAS R & R IAW SRM 51-40-02. - [SDR UHLA201506010486](https://openairdocs.org/sdr/UHLA201506010486), Jun 1, 2015: BUSHING. MIGRATED. DURING INSPECTION, THE LT AILERON DAMPER ATTACH FITTING, OTBD HAT BUSHING WAS FOUND TO HAVE MIGRATED. THE FITTING WAS R & R IAW SRM 51-21-06. - [SDR UHLA201506010485](https://openairdocs.org/sdr/UHLA201506010485), Jun 1, 2015: BUSHING. MIGRATED. DURING INSPECTION, THE LT AILERON PCA ATTACH FITTING HAT BUSHINGS WERE FOUND TO HAVE MIGRATED OUT. THE FITTING WAS R & R IAW SRM 51-40-02. - [SDR UHLA201505310492](https://openairdocs.org/sdr/UHLA201505310492), May 31, 2015: STRINGER. CRACKED. DURING INSPECTION, THE STRINGER STIFFENER 3L WAS FOUND TO BE CRACKED BETWEEN FRAMES 18 AND 19. THE STRINGER STIFFENER WAS R & R IAW SRM 51-40-02. - [SDR CHQA20141121331](https://openairdocs.org/sdr/CHQA20141121331), Nov 21, 2014: SWITCH. FAULTY. THE CREW REPORTED THAT THE GUST LOCK LIGHT CAME ON IN CRUISE FLIGHT. THE CREW DECLARED AN EMER & LANDED WITHOUT INCIDENT AT ITS INTENDED DESTINATION. THE GUST L - [SDR CHQA20140508146](https://openairdocs.org/sdr/CHQA20140508146), May 8, 2014: LIGHT. BROKEN. DURING INSPECTION, THE EMERGENCY FLOOR LIGHT STRIP AT ROW 10A WAS FOUND TO BE BROKEN. THE FLOOR STRIP WAS REPLACED & ALL OPERATIONAL CHECKS WERE GOOD. - [SDR CHQA20131229470](https://openairdocs.org/sdr/CHQA20131229470), Dec 29, 2013: BATTERY. DISCHARGED. DURING INSPECTION, THE FWD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER - [SDR CHQA20130608211](https://openairdocs.org/sdr/CHQA20130608211), Jun 11, 2013: FRAME. DAMAGED. FRAME WAS CREASED. THE FRAME WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130608219](https://openairdocs.org/sdr/CHQA20130608219), Jun 8, 2013: STRINGER. BENT. DURING INSPECTION, A STRINGER 12L WAS FOUND TO BE BENT BETWEEN FRAMES 71 AND 72. THE STRINGER WAS REPLACED IAW ETD 2012-145-017997-A. - [SDR CHQA20130608218](https://openairdocs.org/sdr/CHQA20130608218), Jun 8, 2013: FRAME. DAMAGED. DURING INSPECTION, A FINAL REPAIR WAS COMPLETED FOR A DEFERRED MX ITEM ON FRAME 62 AT STRINGER 13L WHICH WAS CREASED. THE FRAME WAS REPAIRED IAW ETD2012-145-017 - [SDR CHQA20130608216](https://openairdocs.org/sdr/CHQA20130608216), Jun 8, 2013: STRINGER. DAMAGED. DURING INSPECTION, A FINAL REPAIR FOR STRINGER 13L DAMAGE BETWEEN FRAME 62 AND FRAME 62A WAS COMPLETED. THE STRINGER WAS REPLACED IAW ETD 2012-145-017997. - [SDR CHQA20130607217](https://openairdocs.org/sdr/CHQA20130607217), Jun 7, 2013: FLOOR SUPPORT. CRACKED. DURING INSPECTION, THE RT SIDE OMEGA BEAM AT FRAME 59 HAS A CRACK IN THE NUT PLATE HOLE. THE BEAM WAS REPAIRED IAW ETD 2013-145-011759. - [SDR CHQA20130603210](https://openairdocs.org/sdr/CHQA20130603210), Jun 3, 2013: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR LOWER FRAME AROUND THE NUT PLATE HOLES. THE FRAME WAS REPAIRED IAW ETD 2013-145-011762. - [SDR CHQA20130602213](https://openairdocs.org/sdr/CHQA20130602213), Jun 2, 2013: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE REPAIR ANGLE AT FRAME 23. THE REPAIR DOUBLER WAS REPLACED IAW SRM 51-40-02. - [SDR CHQA20130601214](https://openairdocs.org/sdr/CHQA20130601214), Jun 1, 2013: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE LOWER DOOR PLATE. THE FRAME WAS REPAIRED IAW SRM 53-31-04 AND SRM 51-40-02. - [SDR CHQA20130601212](https://openairdocs.org/sdr/CHQA20130601212), Jun 1, 2013: FRAME. CORRODED. DURING INSPECTION, A GOUGE WAS FOUND ON FRAME 60 BETWEEN STRINGERS 4L AND 5L. THE FRAME WAS REPAIRED IAW SRM 53-00-04. - [SDR CHQA20130531215](https://openairdocs.org/sdr/CHQA20130531215), May 31, 2013: SKIN. DAMAGED. DURING INSPECTION, THE LEFT HAND ENGINE PYLON WAS FOUND TO HAVE DAMAGE AROUND THE DRILLED SCREW SHANK ON THE UPPER FORWARD SURFACE. THE DAMAGE WAS REPAIRED IAW - [SDR CHQA20121205451](https://openairdocs.org/sdr/CHQA20121205451), Dec 5, 2012: ENGINE. LEAKING. CREW REPORTED THAT THEY RECEIVED A LAVATORY SMOKE INDICATION ON CLIMBOUT. THEY REPORTED NO VISIBLE SMOKE WAS PRESENT, HOWEVER AN ODOR WAS PRESENT IN THE CABIN. - [SDR CHQA201100496](https://openairdocs.org/sdr/CHQA201100496), Dec 22, 2011: WIRE. DAMAGED. CREW REPORTED THAT DURING CLIMB, AT 17,000 FEET, THEY RECEIVED A HIGH OIL PRESSURE INDICATION FOR THE NUMBER 2 ENGINE. AFTER LEVELING, THE CREW RAN THE QUICK RE - [SDR CHQA201100489](https://openairdocs.org/sdr/CHQA201100489), Dec 15, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE EMERGENCY LIGHT POWER SUPPLY IN POSITION 4 FAILED THE FUNCTIONAL CHECK. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERAT - [SDR CHQA201100265](https://openairdocs.org/sdr/CHQA201100265), Jul 4, 2011: FLOOR SUPPORT. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE LEFT OMEGA BEAM BETWEEN FRAMES 23 AND 24 IN CENTER FUSE I. MAINTENANCE REPAIRED THE LEFT OMEGA BEAM BETWEEN FRAME 14 - [SDR CHQA201100262](https://openairdocs.org/sdr/CHQA201100262), Jul 3, 2011: SPAR CAP. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT WING FRONT SPAR LOWER CAP FROM THE CAP EDGE THROUGH THE SCREW HOLE. THE AIRCRAFT IS CURRENTLY IN C-CHECK INSPE - [SDR CHQA201100042](https://openairdocs.org/sdr/CHQA201100042), Feb 23, 2011: INVERTER. INOPERATIVE. DURING INSPECTION, THE FORWARD OVERWING EXIT LOCATOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT INVERTER FOR THE FORWARD OVERWI - [SDR CHQA201000007](https://openairdocs.org/sdr/CHQA201000007), Jan 13, 2010: BATTERY. DISCHARGED. DURING INSPECTION THE LAST 4 EMERGENCY LIGHT STRIPS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY LIGHT BATTERY IAW AMM 33-50-04 AND THE - [SDR CHQA200900138](https://openairdocs.org/sdr/CHQA200900138), Jun 8, 2009: CONNECTOR. LOOSE. DURING INSPECTION, THE EMERGENCY LIGHT OVER THE MAIN DOOR AND FRONT SIDE OF THE EXIT ROW SIGN WERE INOP WHEN TESTED. MAINTENANCE RE-SECURED ALL CONNECTORS ON TH - [SDR CHQA200900085](https://openairdocs.org/sdr/CHQA200900085), Mar 19, 2009: SEAL. LEAKING. FLIGHT 6123, MKE TO CVG - CREW REPORTED THAT THE AUTO PRESSURIZATION SYSTEM WAS INOP, BUT DID NOT TRY THE MANUAL MODE BEFORE RETURNING TO MKE. THEY ALSO REPORTE - [SDR CHQA200800156](https://openairdocs.org/sdr/CHQA200800156), Jul 29, 2008: CONTROL UNIT. FAULTY. FLIGHT 6349, CVG TO LIT. DURING INITIAL CLIMB THE FLIGHT CREW RECEIVED A PTRIM MAIN INOP MESSAGE ON EICAS. THE CREW PERFORMED THE APROPRIATE QRH CHECKLIST ITEMS - [SDR CHQA200800036](https://openairdocs.org/sdr/CHQA200800036), Feb 20, 2008: ENGINE. MAKING METAL. CVG TO GSP - AFTER TAKEOFF, THE FLIGHT CREW REPORTED SMOKE IN THE CABIN AND THE AUTO SHUTDOWN OF ENGINE NR 1. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT - [SDR CHQA200600130](https://openairdocs.org/sdr/CHQA200600130), Oct 3, 2006: BATTERY. DISCHARGED. EMERGENCY LIGHTS IN BACK HALF OF AIRPLANE (INSIDE) WERE ON WHEN ARRIVED AT THE AIRCRAFT. AIRPLANE WAS COMPLETELY POWERED DOWN. REMOVED AND REPLACED EMERGENCY BA - [SDR CHQA200600007](https://openairdocs.org/sdr/CHQA200600007), Jan 15, 2006: BULB. BURNED OUT. RIGHT AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB ON RIGHT AFT EMERGENCY LIGHT IAW EMB MM 33-50-10. - [SDR CHQA200500174](https://openairdocs.org/sdr/CHQA200500174), Oct 6, 2005: STATIC INVERTER. INOPERATIVE. LEFT OVERWING EMERGENCY EXIT MARKER LIGHT INOPERATIVE. REMOVED AND REPLACED NR 4 STATIC INVERTER IAW EMB 145 MM 33-50-11. OPS CHECK GOOD. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). 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