# N566RP: 2003 Embraer EMB-145LR, registration cancelled 2018-12-17

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: December 17, 2018
- Exported to: Bahamas
- 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: 145691
- Year built: 2003
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 13, 2003
- Last registry action: December 17, 2018
- Mode S code: A73EB9
- Owner when cancelled: [Enterprise Lease Finance LLC](https://openairdocs.org/faa-owner/ENTERPRISE%20LEASE%20FINANCE%20LLC)
- Location: [Saint Louis, MO](https://openairdocs.org/faa-place/MO/Saint%20Louis)
- Owner type: LLC
- Owner's area on the map: 38.6443° N, 90.3281° W: Placed by OpenAirDocs at the center of ZIP code 63105, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N566RP
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=566RP
- Page: https://openairdocs.org/deregistered/N566RP-2018-12-17

From the FAA registry file of November 4, 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 (53, newest 50)

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

- [SDR UHLA201508040633](https://openairdocs.org/sdr/UHLA201508040633), Aug 4, 2015: SHEAR TIE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR TIE AT STRINGER 16L AT FRAME 65. THE SHEAR TIE WAS R & R IAW SRM 51-21-06.
- [SDR UHLA201508030631](https://openairdocs.org/sdr/UHLA201508030631), Aug 3, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT WALL SEAT TRACK SUPPORT BETWEEN FRAMES 43-47. THE LATERAL SUPPORT WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201508030629](https://openairdocs.org/sdr/UHLA201508030629), Aug 3, 2015: SEAT TRACK. CORRODED. DURING INSPECTION, CORROSION WAS FOUND BETWEEN FRAMES 48-50 ON THE RT WALL SEAT TRACK SUPPORT. THE RT LATERAL SUPPORT WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201508020636](https://openairdocs.org/sdr/UHLA201508020636), Aug 2, 2015: STRUCTURE. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE PILOT FLOOR FRAME OTBD OF INBD SEAT TRACK BETWEEN FRAMES 10-12. THE CORROSION WAS REPAIRED IAW ETD2015-145-072011.
- [SDR UHLA201508020635](https://openairdocs.org/sdr/UHLA201508020635), Aug 2, 2015: FLOORBEAM. CORRODED. DURING INPSECTION, CORROSION WAS FOUND ON THE PILOT INBD FLOOR FRAME AFT OF THE RT RUDDER PEDAL AT FRAME 10. THE CORROSION WAS REPAIRED IAW ETD2015-145-072011.
- [SDR UHLA201508020634](https://openairdocs.org/sdr/UHLA201508020634), Aug 2, 2015: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE RT FLOOR SILL AT FRAME 61. THE RIGHT FLOOR SILL WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201508020632](https://openairdocs.org/sdr/UHLA201508020632), Aug 2, 2015: TEE FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT FORWARD LOWER T-FITTING AT FRAME 65. THE PROFILE TEE FITTING WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201508020630](https://openairdocs.org/sdr/UHLA201508020630), Aug 2, 2015: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR CUTOUT THRESHOLD AT FRAME 65. THE CARGO DOOR THRESHOLD WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201508020627](https://openairdocs.org/sdr/UHLA201508020627), Aug 2, 2015: STRIKER. CORRODED. DURING INSPECTION, CORROSION WAS FOUND BEHIND THE LOWER FORWARD STRIKER PLATE AT FRAME 65. THE CORROSION WAS REPAIRED IAW SRM 53-31-04.
- [SDR UHLA201508010639](https://openairdocs.org/sdr/UHLA201508010639), Aug 1, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS SUSPECTED AT FRAME 79 BETWEEN STR 5LT AND 6LT. THE FILLER AND DOUBLER WERE R & R IAW ETD2015-145-073315.
- [SDR UHLA201508010638](https://openairdocs.org/sdr/UHLA201508010638), Aug 1, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS SUSPECTED AT FRAME 78 BETWEEN STRINGERS 5R-6R. THE FILLER AND DOUBLER WERE R & R IAW ETD2015-145-075243.
- [SDR UHLA201508010637](https://openairdocs.org/sdr/UHLA201508010637), Aug 1, 2015: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS SUSPECTED AT FRAME 78 BETWEEN STRINGERS 6RT-7RT. THE FILLER AND DOUBLER WERE R & R IAW ETD2015-145-075243.
- [SDR UHLA201508010628](https://openairdocs.org/sdr/UHLA201508010628), Aug 1, 2015: FLOORBEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MAIN CABIN DOOR FLOORBEAM AT FRAME 16. THE CROSSBEAM WAS R & R IAW SRM 51-40-02.
- [SDR UHLA201507080551](https://openairdocs.org/sdr/UHLA201507080551), Jul 8, 2015: LIGHT. SMOKE. THE F/O'S YOKE CHART HOLDER LIGHTS BEGAN SMOKING IN FLIGHT. THE CREW MADE AN UNEVENTFUL LANDING AND MAINTENANCE REMOVED THE CHART HOLDER AND SECURED THE CONNECT
- [SDR UHLA201505030338](https://openairdocs.org/sdr/UHLA201505030338), May 3, 2015: CLAMP. LOOSE. THE CREW REPORTED A BLEED SYSTEM 2 LEAK MESSAGE ON CLIMBOUT. THE CREW MADE AN UNEVENTFUL UNSCHEDULED LANDING AT THE FIELD OF DEPARTURE. MAINTENANCE FOUND A LOOS
- [SDR CHQA20140920279](https://openairdocs.org/sdr/CHQA20140920279), Sep 20, 2014: SKIN. CRACKED. DURING INSPECTION A HIGH FREQUENCY EDDY CURRENT INSPECTION FOUND THE SKIN TO CRACKED AT 1 FASTENER ABOVE STRINGER 6R & 1 BELOW STRINGER 6R AT FRAME 79. THE SKIN
- [SDR CHQA20140920277](https://openairdocs.org/sdr/CHQA20140920277), Sep 20, 2014: FLOOR SUPPORT. CORRODED. DURING INSPECTION THE CTR OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 19 - 23. THE OMEGA BEAM WAS REPLACED IAW SRM 51-40-02.
- [SDR CHQA20140919280](https://openairdocs.org/sdr/CHQA20140919280), Sep 19, 2014: SKIN. DAMAGED. DURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 24 & STRINGER 15R IAW ETD2014-145-015228A.
- [SDR CHQA20140919278](https://openairdocs.org/sdr/CHQA20140919278), Sep 19, 2014: SKIN. DAMAGED. DURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 25 & STRINGER 15R IAW ETD2014-145-015228A.
- [SDR CHQA20140919276](https://openairdocs.org/sdr/CHQA20140919276), Sep 19, 2014: SKIN. DAMAGED. DURING HEAVY MX A LIGHTNING STRIKE REPAIR WAS COMPLETED ON THE SKIN AT FRAME 17 & STRINGER 17R IAW ETD2014-145-015228A.
- [SDR CHQA20140912275](https://openairdocs.org/sdr/CHQA20140912275), Sep 19, 2014: SKIN. GOUGED. DURING INSPECTION THE RT FUSELAGE SKIN WAS FOUND TO BE GOUGED AT THE INSIDE PYLON ACCESS PANEL 424DB AT FRAME 67 & STRINGER 9R. THE SKIN WAS REPAIRED IAW ETD201
- [SDR CHQA20140210047](https://openairdocs.org/sdr/CHQA20140210047), Feb 10, 2014: BATTERY. DISCHARGED. DURING INSPECTION, THE NR 4 EMERGENCY LIGHT BATTERY WAS FOUND TO BE DISCHARGED. REPLACED THE BATTERY & ALL OPERATIONS CHECKED ARE GOOD.
- [SDR CHQA20130719305](https://openairdocs.org/sdr/CHQA20130719305), Jul 19, 2013: BEAM. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE SERVICE DOOR CUTOUT LOWER BEAM. THE THRESHOLD PLATE WAS REPAIRED IAW SRM 53-40-02.
- [SDR CHQA20130719304](https://openairdocs.org/sdr/CHQA20130719304), Jul 19, 2013: THRESHOLD. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CARGO DOOR THRESHOLD BENEATH THE FLOOR PANEL 271FF. THRESHOLD REPAIRED IAW SRM 51-40-02.
- [SDR CHQA20130709262](https://openairdocs.org/sdr/CHQA20130709262), Jul 9, 2013: CONTROL MODULE. FAULTY. RECEIVED A BAGGAGE EXTINGUISHING BOTTLE INOPERATIVE MESSAGE DURING CRUISE. MESSAGE CLEARED ON ITS OWN AND THE F/A REPORTED THAT THERE WAS NO INDICATION OF SMOKE
- [SDR CHQA20130623232](https://openairdocs.org/sdr/CHQA20130623232), Jun 23, 2013: WIRE. BROKEN. DURING INSPECTION, MAIN ENTRY DOOR HAND RAIL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MX FOUND A DAMAGED WIRE IN THE MAIN ENTRY DOOR WIRING HARNESS AND REPA
- [SDR CHQA20130315081](https://openairdocs.org/sdr/CHQA20130315081), Mar 15, 2013: BATTERY. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS WER
- [SDR CHQA20121202449](https://openairdocs.org/sdr/CHQA20121202449), Dec 2, 2012: SKIN. DAMAGED. CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. THE CREW DIVERTED TO CMH AND LANDED WITHOUT INCIDENT. DURING THE LIGHTNING STRIKE INSPECTION, MAINTENANCE FOUND BU
- [SDR CHQA20121015384](https://openairdocs.org/sdr/CHQA20121015384), Oct 15, 2012: BATTERY. DISCHARGED. DURING INSPECTION, BOTH EXTERNAL OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NUMBER 4 EMERGENCY LIGHT BATTERY. OPERATIONAL 
- [SDR CHQA20120607190](https://openairdocs.org/sdr/CHQA20120607190), Jun 8, 2012: SKIN. CORRODED. DURING INSPECTION, CORROSION WAS FOUND AT A SCREW HOLE ON THE LOWER SERVICE DOOR CUT-OUT AT FRAME 22. FRAME 22 WAS REPAIRED IN ACCORDANCE WITH ETD2012-145-00824
- [SDR CHQA201100308](https://openairdocs.org/sdr/CHQA201100308), Aug 5, 2011: BATTERY. DISCHARGED. DURING INSPECTION THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE NR 4 EMERGENCY BATTERY. OPERATIONAL CHECKS WERE GOOD WITH
- [SDR CHQA201100269](https://openairdocs.org/sdr/CHQA201100269), Jul 7, 2011: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT CHANNEL FRAME AT FRAME 65 BETWEEN STRINGER 15L AND 16L. THE CORRODED AREA MEASURED 2.9" BY 0.8". MAINTENANCE 
- [SDR CHQA201100268](https://openairdocs.org/sdr/CHQA201100268), Jul 7, 2011: FITTING. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FRAME BAGGAGE DOOR SHEAR CLIP. THE AIRCRAFT IS STILL IN INSPECTION AND THE FINAL CORRECTIVE ACTION WILL BE S
- [SDR CHQA201100267](https://openairdocs.org/sdr/CHQA201100267), Jul 5, 2011: FLOOR SUPPORT. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE MIDDLE TOILET OMEGA BEAM 5 INCHES FORWARD OF FRAME 61. MAINTENANCE REPAIRED THE MIDDLE TOILET OMEGA BEAM IN ACCORD
- [SDR CHQA201100264](https://openairdocs.org/sdr/CHQA201100264), Jul 4, 2011: FRAME. CORRODED. DURING INSPECTION, CORROSION WAS FOUND ON THE CHANNEL FRAME AT FRAME 65 BETWEEN STRINGERS 15L AND 16L. THE CORRODED AREA MEASURED 2.9" BY 0.8". MAINTENANCE REPL
- [SDR CHQA201100263](https://openairdocs.org/sdr/CHQA201100263), Jul 4, 2011: SUPPORT BRACKET. CRACKED. DURING INSPECTION, A CRACK WAS FOUND ON THE RIGHT SUPPORT BRACKET AT FRAME 8 AND STRINGER 9R IN THE FORWARD FUSE II SECTION. MAINTENANCE REPLACED THE RIGHT FORW
- [SDR CHQA201100281](https://openairdocs.org/sdr/CHQA201100281), Jul 1, 2011: FRAME. CRACKED. DURING INSPECTION, A CRACK WAS FOUND AT FORWARD FUSELAGE II, LEFT AND RIGHT FRAME 10 AT THE INTERSECTION OF THE EMERGENCY ESCAPE HATCH LOWER BEAM. MAINTENANCE R
- [SDR CHQA201100280](https://openairdocs.org/sdr/CHQA201100280), Jun 29, 2011: SKIN. DENTED. DURING INSPECTION, THE RIGHT WING LEADING EDGE II WAS FOUND TO HAVE TWO DENTS ON THE SKIN COUPLED WITH A CRACK ON THE RIGHT LEADING EDGE II RIB. THE TWO DENTS O
- [SDR CHQA201100053](https://openairdocs.org/sdr/CHQA201100053), Mar 9, 2011: LIGHT. INOPERATIVE. DURING INSPECTION, THE RIGHT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE RIGHT OVERWING EMERGENCY LIGHT ASSEMBLY WITH NO FURT
- [SDR CHQA201000191](https://openairdocs.org/sdr/CHQA201000191), Oct 3, 2010: FLAP SYSTEM. MALFUNCTIONED. ON DESCENT INTO LGA, CREW SELECTED FLAPS FROM 0 TO 9 AND RECEIVED A FLAP FAIL MESSAGE ON EICAS. THE FLAPS DID NOT MOVE FROM 0 DEGREES. THE CREW ABORTED THE APPR
- [SDR CHQA201000151](https://openairdocs.org/sdr/CHQA201000151), Aug 6, 2010: LIGHT. INOPERATIVE. DURING INSPECTION, THE EMERGENCY LIGHT ON THE AIR STAIR HANDRAIL WAS FOUND TO BE INOPERATIVE. MAINTENANCE RELAMPED THE AIR STAIR EMERGENCY LIGHT AND THE EMERGEN
- [SDR CHQA201000116](https://openairdocs.org/sdr/CHQA201000116), Jun 9, 2010: AMPLIFIER. FAULTY. AFTER TAKEOFF THE CREW REPORTED A CONSTANT CABIN TO COCKPIT CHIME AND WERE UNABLE TO COMMUNICATE WITH THE FLIGHT ATTENDANT. THE FLIGHT RETURNED TO LEX AND LANDE
- [SDR CHQA201000060](https://openairdocs.org/sdr/CHQA201000060), Mar 20, 2010: BATTERY PACK. DISCHARGED. DURING INSPECTION THE NR 4 EMERGENCY LIGHT BATTERY WAS INOP WHEN TESTED. MAINTENANCE REPLACED THE NR 4 BATTERY IAW EMB 145 AMM 33-50-04, OPS CHECK GOOD.
- [SDR CHQA201000009](https://openairdocs.org/sdr/CHQA201000009), Jan 17, 2010: O-RING. BLOWN. THE FLIGHT CREW REPORTED A BLEED 1 LEAK MESSAGE ON EICAS UPON ENTERING ICING CONDITIONS DURING CLIMB. THE CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAIN
- [SDR CHQA200900134](https://openairdocs.org/sdr/CHQA200900134), May 27, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION THE OVER-WING EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. THE NR4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE OVER-WING EMERGENCY LIGHTS O
- [SDR CHQA200900081](https://openairdocs.org/sdr/CHQA200900081), Mar 14, 2009: BATTERY PACK. DISCHARGED. DURING INSPECTION, THE OVERWING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR 4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYSTEM OPERATED NO
- [SDR CHQA200900068](https://openairdocs.org/sdr/CHQA200900068), Mar 2, 2009: PROXIMITY SWITCH. DIRTY. FLIGHT 9940, AVL TO TRI. AFTER TAKEOFF WHEN THE GEAR WAS COMMANDED UP, THE FLIGHT CREW NOTICED THAT THE NOSE GEAR DOORS HAD NOT CLOSED. THE AIRCRAFT CONTINUED I
- [SDR CHQA200900006](https://openairdocs.org/sdr/CHQA200900006), Jan 5, 2009: CABIN PRESSURE. MALFUNCTIONED. ON CLIMB OUT AT 4,000 FT THE DIFFERENTIAL PRESSURE INDICATION DROPPED FROM 1.6 TO ZERO IN AUTO PRESSURIZATION MODE. THE CREW DID NOT FEEL A CHANGE IN PRESSURIZA
- [SDR CHQA200900266](https://openairdocs.org/sdr/CHQA200900266), Jan 3, 2009: BATTERY PACK. INOPERATIVE. DURING A SERVICE CHECK THE OVER WING EMERGENCY LIGHTS WERE FOUND TO BE INOP. THE NR4 EMERGENCY LIGHT BATTERY WAS REPLACED AND THE EMERGENCY LIGHT SYS OPERATED N
- [SDR CHQA200800079](https://openairdocs.org/sdr/CHQA200800079), Apr 14, 2008: GASKET. MISSING. FLIGHT 6239, BOS TO SAV, DURING CRUISE, THE FLIGHT ATTENDANT NOTIFIED THE FLIGHT CREW OF A FLUID LEAK COMING FROM THE LEFT WING. THE FLIGHT CREW VERIFIED THE FL

All 53: https://openairdocs.org/deregistered/N566RP-2018-12-17/reports.md

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