N149381997 Embraer EMB-145EP
This N-number isn't registered right now. Below is its last known registration, canceled Mar 15, 2016.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply86 service difficulty reports
- Registration
- Deregistered
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
- Mar 15, 2016
- 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 dataAirframe
- Manufacturer
- Embraer
- Model
- EMB-145EP
- Year
- 1997
- Serial number
- 145029
- 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
- A0C701
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- 1998 – 2016Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT
- 1951 – 1955Lease Air INCBurbank, CA · different airframe: Lockheed Electra 10-A S/N 1027
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB 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.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2025-08-07 | Flight Controls | Jun 26, 2025 | Airframe (EMB-145EP) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145EP) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145EP) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145EP)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002 |
| 2002-14-23 | Empresa Brasileira de Aeronautica S.A. | Aug 2, 2002 | Airframe (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 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-09-09 | EMBRAER Model EMB-145 Series Airplanes | Jun 16, 2000 | Airframe (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 (86)
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.
- Lights · bulb · burned outSep 17, 2014
DURING MAINTENANCE INSPECTION THE LT WING AFT EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED LIGHT BULB, 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. - Lights · light · inoperativeAug 7, 2014
DURING A 3A INSPECTION, THE LT EMERGENCY LIGHT ON THE FUSELAGE WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE LIGHT ASSY, 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. - Wings · attach fitting · damagedMay 14, 2014
DURING 2A-CHECK INSPECTION, THE RT AILERON PCA ATTACH FITTING WAS FOUND TO HAVE SEVERAL TOOL MARKS. MAINTENANCE PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING THAT AFFECTED FITTING, OPERATIONALLY TESTING WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · attach fitting · damagedMay 14, 2014
DURING 2A-CHECK INSPECTION, THE RT AILERON PCA ATTACH FITTING WAS FOUND TO HAVE SEVERAL TOOL MARKS. MAINTENANCE PERFORMED A MAJOR REPAIR BY REMOVING AND REPLACING THA AFFECTED FITTING, OPERATIONALLY TESTING WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · light · inoperativeMar 19, 2014
DURING PREFLIGHT, CREW REPORTED THAT THE CABIN FLOOR EMERGENCY LIGHT STRIP AT SEAT 4A WAS INOPERATIVE. R & R EMERGENCY LIGHT AND OPS TESTED WITH NO DEFECTS. APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · seal · debondedMar 11, 2014
EXPERIENCED CABIN DEPRESSURIZATION AT ALTITUDE AND THEN DIVERTED. MAINTENANCE FOUND CARGO DOOR RUBBER TRIM SEAL DEBONDED AND HANGING OUT IN THE AIRSTREAM. REINSTALLED CARGO DOOR RUBBER TRIM SEAL IAW AMM 52-30-02. PERFORMED LEAK CHECK ON PRESSURIZATION AND OPS CHECK ON THE PRESSURIZATION SYS IN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · socket · shortedDec 16, 2013
THE CREW REPORTED A STRONG ELECTRICAL BURNING ODOR IN FRONT CABIN. MAINTENANCE INSPECTED AND FOUND THE OVERHEAD LIGHT SOCKET SHORTED AND MELTED. R & R AFFECTED 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 · crackedJul 17, 2013
DURING 2A INSPECTION, THE LT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT A RIVET ON FRAME 77, BELOW STRINGER 4. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A BUSHING REPAIR, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedFeb 26, 2013
DURING A-CHECK INSPECTION, THE RT AFT FUSELAGE SKIN WAS FOUND TO HAVE A .2" (5MM) CRACK AT FRAME 75 BETWEEN STR 2R & 3R. MX REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A FILLER/DOUBLER REPAIR IAW ENGINEERING CHANGE REPAIR AUTHORIZATION EC5330-02353, AND THE ACFT WAS APPROVED FOR RETURN TO…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedNov 7, 2012
DURING C-CHECK, THE INTERNAL SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 17-19 AND STRINGERS 21L-21R. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-02633. 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 86 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