# N562RP: 2002 Embraer EMB-145LR, registration cancelled 2022-10-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 1, 2022
- Status when cancelled: Registration expired, pending cancellation
- 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: 145451
- Year built: 2002
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 26, 2002
- Certificate issued: June 20, 2019
- Last registry action: June 20, 2019
- Mode S code: A72FDD
- Owner when cancelled: [Bai Bayview Aviation LLC](https://openairdocs.org/faa-owner/BAI%20BAYVIEW%20AVIATION%20LLC)
- Location: [Mount Pleasant, SC](https://openairdocs.org/faa-place/SC/Mount%20Pleasant)
- Owner type: LLC
- Owner's area on the map: 32.8174° N, 79.8551° W: Placed by OpenAirDocs at the center of ZIP code 29464, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N562RP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=562RP
- Page: https://openairdocs.org/deregistered/N562RP-2022-10-01

From the FAA registry file of November 3, 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 (67, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR UHLA201602100043](https://openairdocs.org/sdr/UHLA201602100043), Feb 10, 2016: LIGHT. MISINSTALLED. EMERGENCY LIGHT OVER LT WING IS INSTALLED UPSIDE DOWN. REPOSITIONED LEFT EMERGENCY LIGHT IAW AMM 33-50-10. OPS CHECK GOOD.
- [SDR UHLA201602060042](https://openairdocs.org/sdr/UHLA201602060042), Feb 6, 2016: WASHER. MISSING. AREA WASHER MISSING ON MED STEP ACTUATOR RAMP. INSTALLED WASHER TO MED STEP ACTUATOR ARM IN REF WITH AMM 52-10-01.
- [SDR UHLA201602060041](https://openairdocs.org/sdr/UHLA201602060041), Feb 6, 2016: BOLT. SHEARED. MED REAR HINGE HAS SHEARED BOLT AT ACTUATOR ATTACH. R & R BOLT IN REAR HINGE ROTATING ARM IAW AMM 52-11-03.
- [SDR UHLA201602060040](https://openairdocs.org/sdr/UHLA201602060040), Feb 6, 2016: ARM. DAMAGED. MED REAR ROTATING ARM FOUND DAMAGED. R & R MED REAR ROTATING ARM IAW AMM 52-11-03.
- [SDR CHQA20141203350](https://openairdocs.org/sdr/CHQA20141203350), Dec 3, 2014: PROFILE. PUNCTURED. DURING INSPECTION, PUNCTURE DAMAGE WAS FOUND ON THE PAX DOOR U LATERAL PROFILE. THE PROFILE WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141203344](https://openairdocs.org/sdr/CHQA20141203344), Dec 3, 2014: PROFILE. CORRODED. DURING INSPECTION, THE PAX DOOR U PROFILE WAS FOUND TO BE CORRODED. THE PROFILE WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141202349](https://openairdocs.org/sdr/CHQA20141202349), Dec 2, 2014: STEP. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PAX DOOR ON THE NR 1 STEP. THE NR 1 PAX DOOR STEP WAS REPLACED IAW SRM 51-21-02.
- [SDR CHQA20141201343](https://openairdocs.org/sdr/CHQA20141201343), Dec 1, 2014: SERVICE DOOR. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE BOTTOM OF THE SERVICE DOOR. THE SERVICE DOOR WAS REPAIRED IAW ETD 2014-145-101279.
- [SDR CHQA20141130348](https://openairdocs.org/sdr/CHQA20141130348), Nov 30, 2014: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT SHEAR CLIP AT FRAME 65. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141130347](https://openairdocs.org/sdr/CHQA20141130347), Nov 30, 2014: DOOR SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR FLOOR SILL AT FRAME 66. THE CARGO DOOR SILL WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20141130346](https://openairdocs.org/sdr/CHQA20141130346), Nov 30, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION, THE LT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. THE BEAM WAS REPLACED IAW SRM 51-40-02 & SRM 53-00-10.
- [SDR CHQA20141130345](https://openairdocs.org/sdr/CHQA20141130345), Nov 30, 2014: SUPPORT. CRACKED. DURING INSPECTION, THE RT OMEGA BEAM INBD SUPPORT WAS FOUND TO BE CRACKED AT FRAMES 47 & 48. THE SUPPORT WAS REPLACED IAW SRM 53-23-02.
- [SDR CHQA20140602184](https://openairdocs.org/sdr/CHQA20140602184), Jun 2, 2014: CONTROL UNIT. FAULTY. CREW REPORTED THAT THEY RECEIVED A BRAKE OTBD INOPERATIVE CAUTION MSG WHEN THE LG WAS SELECTED DOWN. THE CREW DECLARED AN EMER. THE ACFT LANDED WITHOUT INCIDENT
- [SDR CHQA20131124436](https://openairdocs.org/sdr/CHQA20131124436), Nov 24, 2013: SEAT TRACK. CORRODED. LEFT OTBD SEAT TRACK BEAM AT THE OVERWING EXIT WAS FOUND TO BE CORRODED. THE SEAT TRACK BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20131124435](https://openairdocs.org/sdr/CHQA20131124435), Nov 24, 2013: SEAT TRACK. CORRODED. RIGHT SIDEWALL TRACK MOUNTING FLANGE AT FRAME 42 - 48 WAS FOUND TO BE CORRODED. THE SEAT TRACK MOUNTING FLANGE WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20130815314](https://openairdocs.org/sdr/CHQA20130815314), Aug 15, 2013: VALVE. LEAKING. CREW REPORTED DURING CLIMB, FUEL REPORTED TO BE LEAKING FROM LEFT WING. VERIFIED VAPOR COMING FROM THE LT WING AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT. M
- [SDR CHQA20130712270](https://openairdocs.org/sdr/CHQA20130712270), Jul 12, 2013: RADAR. MALFUNCTIONED. CREW REPORTED THAT DURING FLIGHT, WEATHER RADAR BEGAN MALFUNCTIONING. DUE TO WEATHER CONDITIONS ALONG FLIGHT ROUTE, ELECTED TO RETURN TO FIELD. LANDED WITHOUT I
- [SDR CHQA20130622227](https://openairdocs.org/sdr/CHQA20130622227), Jun 22, 2013: WIRE. INOPERATIVE. DURING INSPECTION, THE MAIN ENTRY DOOR HAND RAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX FOUND A DAMAGED WIRE IN THE MAIN ENTRY DOOR WIRING HARNESS. REP
- [SDR CHQA20121210458](https://openairdocs.org/sdr/CHQA20121210458), Dec 10, 2012: PROFILE. CORRODED. DURING INSPECTION, THE SERVICE DOOR LOWER AFT CORNER WAS FOUND TO BE CORRODED AT THE DOOR TRIM ATTACH POINT. THE AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2012-1
- [SDR CHQA20121206564](https://openairdocs.org/sdr/CHQA20121206564), Dec 6, 2012: RIB. DAMAGED. DURING INSPECTION, THE LEFT ELEVATOR INTERNAL RIB AT STATION YH-1310 HAS TWO DAMAGED HOLES. THE DAMAGED AREA WAS REPAIRED IN ACCORDANCE WITH ETD 2012-145-017677
- [SDR CHQA20121206455](https://openairdocs.org/sdr/CHQA20121206455), Dec 6, 2012: FRAME. BENT. DURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN RIGHT STRINGER 14R AND 15R. THE DAMAGED AREA WAS REPAIRED IN ACCORDANCE WITH SRM 53-00-04.
- [SDR CHQA20121205457](https://openairdocs.org/sdr/CHQA20121205457), Dec 5, 2012: GUSSET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE NUT PLATES ON THE CENTER OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR CROSS BEAM. THE GUSSET WAS
- [SDR CHQA20121205456](https://openairdocs.org/sdr/CHQA20121205456), Dec 5, 2012: GUSSET. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AROUND THE NUT PLATES AND FASTENER ON THE RIGHT OMEGA BEAM TOP GUSSET PLATE AT FRAME 59 TO THE COMPOSITE FLOOR. THE GUSSE
- [SDR CHQA20121125453](https://openairdocs.org/sdr/CHQA20121125453), Nov 25, 2012: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OMEGA BEAM JUST FORWARD OF THE "Z" PROFILE AT FRAME 23. THE BEAM WAS REPAIRED IN ACCORDANCE WITH SRM 53-21-1
- [SDR CHQA20121125452](https://openairdocs.org/sdr/CHQA20121125452), Nov 25, 2012: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR ENTRY BEAM AFT OF THE NUT PLATE. THE CORROSION WAS BLENDED IN ACCORDANCE WITH SRM 51-10-03 AND A PREV
- [SDR CHQA201100486](https://openairdocs.org/sdr/CHQA201100486), Dec 14, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE EMERGENCY AISLE LIGHTS FROM THE ROW 8 TO ROW 12. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH N
- [SDR CHQA201100465](https://openairdocs.org/sdr/CHQA201100465), Dec 3, 2011: BATTERY. DISCHARGED. DURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY AND THE NUMB
- [SDR CHQA201100456](https://openairdocs.org/sdr/CHQA201100456), Nov 18, 2011: FADEC. MALFUNCTIONED. CREW REPORTED THAT WHILE ON APPROACH, E2 N1 ROLLED BACK TO 38 PERCENT WHILE E1 N1 STAYED AT 68 PERCENT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET 
- [SDR CHQA201100436](https://openairdocs.org/sdr/CHQA201100436), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 53. MAINTENANCE REPAIRED THE FLOOR SILL AT FRAME 53 IN ACCORDANCE WITH ETD 2011-145-1077
- [SDR CHQA201100435](https://openairdocs.org/sdr/CHQA201100435), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 49. MAINTENANCE REMOVED THE CORROSION AT FLOOR SILL FRAME 49 RIGHT SIDE. THE REMAINING T
- [SDR CHQA201100434](https://openairdocs.org/sdr/CHQA201100434), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 44. MAINTENANCE REMOVED THE CORROSION AT FRAME 44 RIGHT FLOOR SILL. THE REMAINING THICKN
- [SDR CHQA201100433](https://openairdocs.org/sdr/CHQA201100433), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 39. MAINTENANCE BLENDED THE CORROSION ON THE LEFT FLOOR SILL AT FRAME 39. CORROSION WAS F
- [SDR CHQA201100432](https://openairdocs.org/sdr/CHQA201100432), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL FROM FRAME 43 TO FRAME 44. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 43 TO FRAME 44 IN ACC
- [SDR CHQA201100431](https://openairdocs.org/sdr/CHQA201100431), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 35. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 35 IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA201100430](https://openairdocs.org/sdr/CHQA201100430), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT FLOOR SILL AT FRAME 31. MAINTENANCE REPLACED THE LEFT FLOOR SILL AT FRAME 31 IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA201100429](https://openairdocs.org/sdr/CHQA201100429), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 39. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 39 IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA201100428](https://openairdocs.org/sdr/CHQA201100428), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 35. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 35 IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA201100427](https://openairdocs.org/sdr/CHQA201100427), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 31. MAINTENANCE REPLACED THE FLOOR SILL AT FRAME 31 IN ACCORDANCE WITH SRM 51-40-02.
- [SDR CHQA201100426](https://openairdocs.org/sdr/CHQA201100426), Nov 7, 2011: SILL. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT FLOOR SILL AT FRAME 28. MAINTENANCE INSPECTED AND REMOVED THE CORROSION FROM THE FLOOR SILL AT FRAME 28 RIGH
- [SDR CHQA201100422](https://openairdocs.org/sdr/CHQA201100422), Oct 31, 2011: HYDRAULIC SYSTEM. LOW. CREW REPORTED THAT AFTER LANDING GEAR RETRACTION RECEIVED A HYDRAULIC SYSTEM 1 LOW QUANTITY MESSAGE. THE CREW CONTINUED TO MONITOR THE HYDRAULIC SYSTEM DURING T
- [SDR CHQA201100310](https://openairdocs.org/sdr/CHQA201100310), Aug 6, 2011: RELAY. FAILED. CREW REPORTED THAT DURING FLIGHT RECEIVED A COOLING PACK 2 VALVE CLOSED MESSAGE. COOLING PACK 1 WAS DEFERRED THE PREVIOUS DAY. AS A RESULT THE AIRCRAFT LOST PRE
- [SDR CHQA201100303](https://openairdocs.org/sdr/CHQA201100303), Jul 29, 2011: TRANSCEIVER. DEFECTIVE. CREW REPORTED THAT THE WEATHER RADAR WAS NOT DEPICTING THE WEATHER AS SEEN VISUALLY OUTSIDE THE AIRCRAFT. THE CREW TRIED USING BOTH AUTOMATIC AND MANUAL GAIN MO
- [SDR CHQA201100167](https://openairdocs.org/sdr/CHQA201100167), Apr 24, 2011: PROFILE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER. THE MAIN PASSENGER DOOR STRUCTURE FORWARD BOTTOM CORNER WAS R
- [SDR CHQA201100166](https://openairdocs.org/sdr/CHQA201100166), Apr 24, 2011: FRAME SPLICE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME SPLICE. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME SPLI
- [SDR CHQA201100165](https://openairdocs.org/sdr/CHQA201100165), Apr 24, 2011: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FRAME 1. THE MAIN PASSENGER DOOR STRUCTURE FRAME 1 WAS REPLACED WITH NO FURTHER DEFE
- [SDR CHQA201100164](https://openairdocs.org/sdr/CHQA201100164), Apr 24, 2011: STRUCTURE. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE AFT BOTTOM CORNER. THE MAIN PASSENGER DOOR STRUCTURE AFT BOTTOM CORNER WAS REPLACED W
- [SDR CHQA201100163](https://openairdocs.org/sdr/CHQA201100163), Apr 24, 2011: RIB. CORRODED. DURING INSPECTION CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 1ST FROM FORWARD. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 1ST FROM FO
- [SDR CHQA201100162](https://openairdocs.org/sdr/CHQA201100162), Apr 24, 2011: RIB. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 2ND FROM FORWARD. THE MAIN PASSENGER DOOR STRUCTURE BOTTOM RIB 2ND FROM F
- [SDR CHQA201100161](https://openairdocs.org/sdr/CHQA201100161), Apr 24, 2011: DOOR FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME. THE MAIN PASSENGER DOOR STRUCTURE FORWARD SIDE FRAME WAS REPLACE
- [SDR CHQA201100160](https://openairdocs.org/sdr/CHQA201100160), Apr 24, 2011: CASTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN PASSENGER DOOR STRUCTURE DOOR OPENING HANDLE BACK CASTING. THE PASSENGER DOOR STRUCTURE DOOR OPENING HANDLE B

All 67: https://openairdocs.org/deregistered/N562RP-2022-10-01/reports.md

## 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 20040203003089I](https://openairdocs.org/incident/20040203003089I), Feb 3, 2004: Emb EMB145LR (N562RP), Columbus, OH. (-23) Departing cmh and climbing through 3,000 feet MSL, the flight entered icing conditions. The automatic anti-ice came followed by a pop and then a hissing…

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