N149431998 Embraer EMB-145EP
This N-number isn't registered right now. Below is its last known registration, canceled May 26, 2015.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply107 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Bank Of Utah Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- May 6, 2015
- Canceled
- May 26, 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 dataAirframe
- Manufacturer
- Embraer
- Model
- EMB-145EP
- Year
- 1998
- Serial number
- 145040
- 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
- A0C71F
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- 2015Bank Of Utah TrusteeSalt Lake City, UT
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 (107)
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 · drag angle · crackedOct 29, 2013
DURING 2A INSPECTION THE LT VERTICLE STAB TO FUSELAGE LT DRAG ANGLE WAS FOUND TO HAVE A 20MM CRACK AT FRAME 76. MAINTENANCE R & R THE AFFECTED LT DRAG ANGLE, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · light · inoperativeOct 19, 2013
DURING MAINTENANCE INSPECTION, LEFT FWD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE R & R THE AFFECTED EMERGENCY LIGHT, 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 · corrodedMar 7, 2013
DURING C-CHECK THE COCKPIT BELLY SKIN WAS FOUND TO BE CORRODED BETWEEN FRAMES 13-14 AND STRINGERS 18R-19L. MX R & R THE SKIN IAW SRM 51-40-02. 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
- Fuselage · shear angle · crackedFeb 26, 2013
DURING C-CHECK THE RIB 1 SHEAR CLIP FROM FRAMES 40-45 WAS FOUND TO BE CRACKED. MX R & R THE SHEAR CLIP IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear angle · corrodedFeb 26, 2013
DURING C-CHECK THE SHEAR CLIP AT FRAME 68 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear tie · corrodedFeb 26, 2013
DURING C-CHECK THE SHEAR CLIP AT FRAME 65 BETWEEN STRINGERS 15L-16L WAS FOUND TO BE CORRODED. MX REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5330-01458. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · beam · corrodedFeb 26, 2013
DURING C-CHECK THE CARGO DOOR CUT-OUT LOWER BEAM WAS FOUND TO BE CORRODED FROM FRAMES 65-68 BETWEEN STRINGERS 15L-16L. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedNov 26, 2012
DURING MX INSPECTION, THE FUSELAGE SKIN WAS FOUND TO BE CRACKED AT FRAME 75, STRINGER 02L. MX PERFORMED A DOUBLER REPAIR TO THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedNov 26, 2012
DURING MX INSPECTION, FUSELAGE SKIN WAS FOUND TO BE CRACKED ACROSS A RIVET HOLE APPROX 16MM IN LENGTH BETWEEN FRAME 77-78 JUST ABOVE STR 6R. MX INSTALLED A REPAIR DOUBLER ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedNov 26, 2012
DURING MX INSPECTION, THE FUSELAGE SKIN AT FR 75 ON EITHER SIDE OF STRINGER 2R WAS FOUND TO HAVE TWO CRACKS ONE APPROX .039" AND 1 APPROX .157" LONG. MX PERFORMED A DOUBLER REPAIR ON THE AFFECTED AREA, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE ON 12/02/12.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 107 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