N149371997 Embraer EMB-145EP
This N-number isn't registered right now. Below is its last known registration, canceled Oct 4, 2016.
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply104 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Strong Tower Services LLC Trustee
- Owner type
- Corporation
- City, state
- New Castle, DE
- Certificate issued
- Aug 31, 2016
- Canceled
- Oct 4, 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
- 145026
- 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
- A0C700
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- 2016Strong Tower Services LLC TrusteeNew Castle, DE
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (104)
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 · beam · corrodedMay 17, 2014
DURING C-CHECK THE LT WINDSHIELD LOWER FRONT CUTOUT BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED BUSHING REPAIRS IAW EC5310-01782. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Power plant · fitting · crackedMay 13, 2014
DURING C-CHECK THE NR 2 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED AND VERIFIED WITH EDDY CURRENT. MAINTENANCE R & R THE FITTING IAW EC5450-01088. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · shear tie · corrodedMay 13, 2014
DURING C-CHECK THE CARGO DOOR CUTOUT FWD SHEAR TIE WAS FOUND TO BE CORRODED AT FRAME 65, STRINGERS 15L-16L. MAINTENANCE R & R THE SHEAR CLIP IAW SRM 53-31-04. 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 · skin · corrodedMay 13, 2014
DURING C-CHECK THE CENTRAL FUSELAGE LOWER SKIN WAS FOUND TO BE CORRODED AT FRAME 21, STRINGERS 21L AND 21R. MAINTENANCE R & R THE SKIN IAW EC5330-02895. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · bracket · gougedMay 13, 2014
DURING C-CHECK THE LT WINDSHIELD PILLAR BRACKET AT FRAME 10, STRINGER 5L, WAS FOUND TO BE GOUGED. MAINTENANCE R & R THE BRACKET 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 · stringer · crackedMay 13, 2014
DURING C-CHECK STRINGER 6R WAS FOUND TO BE CRACKED BETWEEN FRAME 12-13. MAINTENANCE R & R THE STRINGER 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. - Fuel · flapper valve · leakingApr 1, 2014
THE CREW REPORTED THAT PILOT REPORTED MASSIVE AMOUNTS OF FLUID LOSS JUST INBD OF THE LT AILERON DURING FLIGHT WITH A HEAVY SCENT OF FUEL IN THE AREA. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R THE OTBD FLAPPER VALVE IN THE LT WING, LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Ice and rain protection · relay · inoperativeJan 15, 2014
CREW REPORTED A NR 2 PITOT HEAT INOPERATIVE ON EICAS ACCOMPANIED BY A FAINT ELECTRICAL ODOR ON FINAL APPROACH. THE ACFT LANDED WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE ACFT, R & R RELAY K0055, 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 · crackedJan 6, 2014
DURING MAINTENANCE INSPECTION, THE COCKPIT FUSELAGE SKIN WAS FOUND TO BE CRACKED AT THE UPPER AFT CORNER OF THE F/O DV WINDOW. MAINTENANCE REMOVED THE DAMAGE AND INSTALLED A FILLER/ TRIPLER REPAIR, LEAK CHECKED 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 · inverter · inoperativeAug 20, 2013
DURNG MX INSPECTION, SEVERAL FLOOR EMERGENCY LIGHT PROXIMITY STRIPS DID NOT ILLUMINATE. MX R & R THE NR 3 EMERGENCY LIGHT INVERTER, OPERATIONALLY 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.
Showing the 10 most recent of 104 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