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Aircraft record

N567RP2003 Embraer EMB-145LR

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Jan 15, 2019.

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply40 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2017
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
40
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Wells Fargo Trust Co NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Jan 12, 2017
Canceled
Jan 15, 2019
Airworthiness
Standard · Transport
Airworthiness date
Mar 8, 2003

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Embraer
Model
EMB-145LR
Year
2003
Serial number
145698
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
55
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A74270

Engine

Make and model
Rolls-Royc Ae 3007a1p
Type
Turbo-fan
Power
8,338 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2017 – 2019Wells Fargo Trust Co NA TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (6)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

ADSubjectEffectiveApplies to
2025-08-07Flight ControlsJun 26, 2025Airframe (EMB-145LR)
2024-26-07FuselageMar 11, 2025Airframe (EMB-145LR)
2021-07-14Main landing gearApr 20, 2021Airframe (EMB-145LR)
2004-22-03Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series AirplanesDec 3, 2004Airframe (EMB-145LR)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002
2002-14-23Empresa Brasileira de Aeronautica S.A.Aug 2, 2002Airframe (EMB-145LR)Serial numbers per EMBRAER Service Bulletin 145-27-0088, dated February 1, 2002. Only with: Equipped with horizontal stabilizer actuator (HSA) assemblies having part numbers and serial numbers listed in EMBRAER Service Bulletin 145-27-0088.
Show all 6 ADs
ADSubjectEffectiveApplies to
2000-09-09EMBRAER Model EMB-145 Series AirplanesJun 16, 2000Airframe (EMB-145LR)Certain serial numbers: EMB-145 145004–145047; EMB-145 145049–145051. Only with: Equipped with IC-600 #1 P/N 7017000-82402; excluding airplanes modified per EMBRAER SB 145-22-0001, SB 145-22-0004 Rev 01, or SB 145-31-0007 Rev 02.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (40)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Doors · seal · damagedMay 18, 2016

    LARGE GAP IN UPPER LT CORNER OF MAIN CABIN DOOR SEAL, WHEN CLOSED. FOUND MISSING SEALANT ON DOOR SEAL. APPLIED SEALANT TO UPPER LT CORNER OF MAIN CABIN DOOR IAW AMM 52-10-04. OPS CHECK GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · roller · bentOct 21, 2015

    THE MAIN ENTRY DOOR ROLLER WAS FOUND BENT. MAINTENANCE R & R THE MAIN DOOR FRAME ROLLER SUPPORT ACTUATOR IAW AMM 53-21-02 AND ALL OPS CHECKS WERE GOOD. NO FURTHER DEFECTS HAVE BEEN NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · support · corrodedJun 26, 2015

    DURING INSPECTION, CORROSION WAS FOUND ON THE RT OBSERVERS SEAT TRACK MOUNT FLANGE AT FRAME 33. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · support · corrodedJun 26, 2015

    DURING INSPECTION, CORROSION WAS FOUND ON THE RT OBSERVERS SEAT TRACK MOUNT FLANGE AT FRAME 52. MAINTENANCE REPLACED THE SUPPORT IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedJun 26, 2015

    DURING INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75 AND STRINGER 2L. THE SKIN WAS REPAIRED IAW ETD 2015-145-059490.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · threshold · corrodedJun 26, 2015

    DURING INSPECTION, CORROSION WAS FOUND AT THE SERVICE DOOR THRESHOLD AT FRAMES 20-22. THE CORROSION WAS REPAIRED IAW SRM 53-21-02AD AND SRM 53-21-02RE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · corrodedJun 22, 2015

    DURING INSPECTION, CORROSION WAS FOUND ON THE OMEGA BEAM AT FRAME 20. THE CORROSION WAS REPAIRED IAW SRM 53-00-10.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Pneumatic · filter · dirtyDec 23, 2014

    THE CREW REPORTED THAT THEY RECEIVED A BLEED 2 OVER TEMP MSG DURING CLIMB. THE CREW UTILIZED THE QRH & RETURNED TO FIELD. THE ACFT LANDED WITHOUT FURTHER INCIDENT. CLEANED THE FAN AIR VLV FILTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedSep 27, 2014

    DURING INSPECTION THE AFT FUSELAGE END CLIP AT THE APU FIREWALL INSIDE ACCESS AT FRAME 81 & STRINGER 9R WAS FOUND TO BE CRACKED. THE END CLIP WAS REPLACED IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedSep 27, 2014

    DURING INSPECTION THE AFT FUSELAGE END CLIP AT THE APU FIREWALL INSIDE ACCESS AT FRAME 81& STRINGER 8R WAS FOUND TO BE CRACKED. THE END CLIP WAS REPLACED IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 40 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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