N265SK2000 Embraer EMB-145
This N-number isn't registered right now. Below is its last known registration, canceled Sep 8, 2018.
Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply76 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 17, 2026- Last registered owner
- Wells Fargo Trust Co NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Jun 27, 2000
- Canceled
- Sep 8, 2018
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 25, 2000
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-145
- Year
- 2000
- Serial number
- 145226
- 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
- A2932A
Engine
- Make and model
- Allison Ae 3007a
- Type
- Turbo-jet
- Power
- 7,580 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- 2000 – 2018Wells 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 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (11)
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-145) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145) |
| 2020-16-13 | Turbine Engine Compressor Section | Aug 14, 2020 | Engine (AE 3007A)Serial numbers per Figure 1 to paragraph (c) of this AD. Only with: 3rd-stage compressor wheel P/N 23084158 installed with serial number listed in Figure 1. |
| 2007-24-05 | Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan Engines | Jan 2, 2008 | Engine (AE 3007A) |
Show all 11 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002 |
| 2004-04-05 | Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan Engines | Mar 9, 2004 | Engine (AE 3007A) |
| 2002-14-23 | Empresa Brasileira de Aeronautica S.A. | Aug 2, 2002 | Airframe (EMB-145)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. |
| 2000-09-09 | EMBRAER Model EMB-145 Series Airplanes | Jun 16, 2000 | Airframe (EMB-145)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. |
| 2000-09-05 | Allison Engine Company AE 3007 Series Turbofan Engines | Jul 5, 2000 | Engine (AE 3007A)Only with: Cone shafts P/Ns 23050728 and 23070729 installed. |
| 99-03-03 | Allison Engine Company Model AE 3007A and AE 3007A1/1 Turbofan Engines | Feb 16, 1999 | Engine (AE 3007A) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (76)
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.
- Wings · attach fitting · damagedApr 2, 2015
DURING INSPECTION, ON THE LT WING, THE OTBD FLAP ROLLER ATTACHMENT ON THE RIB INBD SIDE WAS FOUND TO BE DAMAGED. THE FLAP ROLLER ATTACHMENT WAS REPAIRED IAW ETD 2015-145-031617.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · track · corrodedMar 27, 2015
DURING INSPECTION, THE LT UPPER HALF BEARING TRACK ON THE NLG LEG WAS FOUND TO BE CORRODED. THE BEARING TRACK WAS REPAIRED IAW ETD2015-145-030179.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · skin · damagedMar 26, 2015
DURING INSPECTION, DAMAGE ON THE RUDDER 2, LT LOWER SKIN WAS REPAIRED IAWETD 2015-145-030496-B.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · frame · crackedMar 26, 2015
DURING INSPECTION, A CRACK WAS FOUND AT FRAME 75 AND STRINGERS 2R AND 2L. THE CRACK WAS REPAIRED IAW ETD 2015-145-029344.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · track · corrodedMar 25, 2015
DURING INSPECTION, CORROSION WAS FOUND ON THE RT UPPER HALF BEARING TRACK OF THE NLG LEG. THE BEARING TRACK WAS REPAIRED IAW ETD2015-145-030179.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedMar 24, 2015
DURING INSPECTION, THE LT REAR FUSELAGE, END FRAME 66, AT THE LOWER BEAM, WAS FOUND TO BE CRACKED. THE BEAM WAS REPAIRED IAW ETD2015-145-028481, REV A.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedMar 24, 2015
DURING INSPECITON, A CRACK WAS FOUND ON THE LT FLANGE AT FRAME 67. THE AREA WAS REPAIRED IAW ETD2015-145-028481, REV A.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedMar 23, 2015
DURING INSPECTION, THE CENTER FUSELAGE IV LT FLOOR STRUCTURE SILL NR 7 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedMar 23, 2015
DURING INSPECTION, THE CENTER FUSELAGE III LT FLOOR STRUCTURE SILL NR 6 WAS FOUND TO BE CORRODED. THE SILL WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedMar 23, 2015
DURING INSPECTION, THE RT REAR FUSELAGE SILL WAS FOUND TO BE CORRODED BETWEEN FRAME 65 AND FRAME 68. THE SILL 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 76 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