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Aircraft record

N149401997 Embraer EMB-145EP

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 13, 2015.

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply78 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 1998
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
78
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Wells Fargo Bank Northwest NA Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Feb 23, 1998
Canceled
Aug 13, 2015
Airworthiness
Standard · Transport
Airworthiness date
Jun 27, 2005

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-145EP
Year
1997
Serial number
145.033
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
A0C71C

Engine

Make and model
Rolls-Royc Ae3007 Ser
Type
Turbo-fan
Power
6,442 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. 1998 – 2015Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT
  2. Date unknownLockheed Aircraft Corp/Burbank Californiadifferent airframe: 1935 Lockheed Electra 10-A S/N 1029

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

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

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-145EP)
2024-26-07FuselageMar 11, 2025Airframe (EMB-145EP)
2021-07-14Main landing gearApr 20, 2021Airframe (EMB-145EP)
2004-22-03Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series AirplanesDec 3, 2004Airframe (EMB-145EP)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-145EP)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-145EP)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 (78)

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.

  • Fuselage · skin · crackedApr 6, 2014

    DURING 3A INSPECTION THE RT FUSELAGE AFT SKIN WAS FOUND TO HAVE ONE RIVET AT FRAME 78, ONE RIVET BELOW STRINGER 06R WITH TWO CRACKS EMINATING FROM IT. MAINTENANCE REMOVED THE DAMAGE AND PERFORMED A BUSHING REPAIR IAW TECHNICAL DISPOSITION ETD2014-145-029237, AND THE ACFT WAS APPROVED FOR RETURN TO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedApr 6, 2014

    DURING 3A INSPECTION THE RT FUSELAGE AFT SKIN WAS FOUND TO HAVE ONE RIVET WITH TWO CRACKS EMINATING FROM IT ON FRAME 78, ONE RIVET BELOW STRINGER 6R. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A FILLER/DOUBLER REPAIR IAW ETD2014-145-029237, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedApr 6, 2014

    DURING 3A INSPECTION THE LT AFT FUSELAGE SKIN WAS FOUND TO HAVE ONE RIVET WITH THREE CRACKS EMINATING FROM IT ON FRAME 79, ONE RIVET BELOW STR06L. MAINTENANCE REMOVED THE DAMAGED SECTION AND INSTALLED A BUSHING REPAIR IAW TECHNICAL DISPOSTION ETD2014-145-029237, AND THE ACFT WAS APPROVED FOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · floor support · corrodedMar 12, 2014

    DURING C-CHECK. LT OMEGA BEAM CORRODED AT FRAME 44. REPAIRED LT OMEGA BEAM IAW EC5320-01907. ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · corrodedMar 12, 2014

    DURING C-CK. LT OMEGA BEAM CORRODED BETWEEN FRAMES 49-50. REPAIRED OMEGA BEAM IAW EC5320-01907. ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · floor support · corrodedMar 12, 2014

    DURING C-CHECK, LT OMEGA BEAM CORRODED BETWEEN FR 58-59. REPAIRED OMEGA BEAM IAW EC5320-01907. ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · wire harness · overheatedOct 18, 2013

    THE F/A REPORTED ELECTRICAL BURNING ODOR WHEN ACFT ENTERED ICING CONDITIONS. MAINTENANCE INSPECTED THE ACFT AND REMOVED AND REPLACED THE FWD CABIN LIGHT HARNESS, OPS TESTED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedMar 17, 2013

    DURING 2A INSPECTION, THE LT SKIN AT FRAME 78 BETWEEN STR 5L AND 6L WAS FOUND TO BE CRACKED. MX PERFORMED A DOUBLER REPAIR AMD THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedMar 17, 2013

    DURING 2A CHECK THE FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED, PROTRUDING FROM A PREVIOUS REPAIR BETWEEN STR 00 & 01R. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedMar 17, 2013

    DURING 2A INSP THE LT FUSELAGE SKIN AT FRAME 75 WAS FOUND TO BE CRACKED BELOW STR 1R. MX PERFORMED A DOUBLER REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

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

Showing the 10 most recent of 78 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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