N375SK2002 Embraer EMB-135KL
This N-number isn't registered right now. Below is its last known registration, canceled May 31, 2017.
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply36 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Wells Fargo Bank Northwest NA Trustee
- Owner type
- Corporation
- City, state
- Salt Lake City, UT
- Certificate issued
- Oct 5, 2016
- Canceled
- May 31, 2017
- Airworthiness
- Standard · Transport
- Airworthiness date
- Feb 21, 2002
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-135KL
- Year
- 2002
- Serial number
- 145569
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 37
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Type certificate data sheet
- T00011AT
- Mode S code
- A447F8
Engine
- Make and model
- Rolls-Royc Ae 3007a1p
- Type
- Turbo-fan
- Power
- 8,338 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- 2016 – 2017Wells Fargo Bank Northwest NA TrusteeSalt Lake City, UT
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (4)
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 |
|---|---|---|---|
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-135KL) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-135KL) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-135KL)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-135KL)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. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (36)
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.
- Fire protection · warning system · false activationJan 2, 2013
ON DEPARTURE WHILE CLIMBING THROUGH 11,000FT, THE FLIGHT CREW REPORTED A BAGGAGE SMOKE MESSAGE ON EICAS AND A SMOKE ODOR. THE FLIGHT CREW DISCHARGED BOTH BAGGAGE COMPARTMENT FIRE EXTINGUISHING BOTTLES AND DEPLOYED THE PASSENGER OXYGEN MASKS. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Pneumatic · valve · inoperativeMar 23, 2012
CREW REPORTED A BLEED 2 OVERTEMP MESSAGE DURING CLIMB. THE CREW RETURNED TO FIELD AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NUMBER 2 FAN AIR VALVE. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · damagedDec 16, 2011
DURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON FRAME 22 BETWEEN STRINGERS 19R-20R. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-01.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · skin · damagedDec 16, 2011
DURING INSPECTION, A PATCH REPAIR WAS DONE ON THE CENTER FUSELAGE I SKIN ON STRINGER 20R BETWEEN FRAME 15-16. THE REPAIR WAS DONE IN ACCORDANCE WITH SRM 53-21-01.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · corrodedDec 14, 2011
DURING INSPECTION, CORROSION WAS FOUND ON THE CENTER OMEGA BEAM LOWER LIP AT FRAME 27. MAINTENANCE REPAIRED THE CENTER OMEGA BEAM AT FRAME 27 IN ACCORDANCE WITH SRM 53-00-10.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedDec 12, 2011
DURING INSPECTION, A CRACK WAS FOUND ON FRAME 23. MAINTENANCE REPAIRED THE RIGHT-HAND FUSELAGE AT FRAME 23 UNDER SILL NUMBER 1 IN ACCORDANCE WITH ETD 2011-145-109359.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · corrodedDec 12, 2011
DURING INSPECTION, A BLENDOUT ON THE LEFT SKIN BAY BORDERED BY FRAME 19-20 AND BETWEEN STRINGERS 14L-15L WAS FOUND CORRODED. MAINTENANCE REPAIRED THE BLENDOUT ON THE LEFT SKIN BETWEEN FRAME 19-20 AND STRINGERS 14L-15L IN ACCORDANCE WITH SRM 53-21-01.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · crackedDec 10, 2011
DURING INSPECTION, THE COCKPIT LEFT AND RIGHT FRAME 10 WERE FOUND TO BE CRACKED. MAINTENANCE REPLACED THE LEFT (PN: 145-02409-001) AND RIGHT (PN: 145-02409-002) FRAME 10. THE NEW PART WAS INSTALLED WITH A SOLID RIVET IN ACCORDANCE WITH SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · repair · corrodedDec 9, 2011
DURING INSPECTION, THE LEFT BEAM EXISTING REPAIR AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REPAIRED THE LEFT BEAM AT FRAME 20 IN ACCORDANCE WITH SRM 53-00-10.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · beam · corrodedDec 9, 2011
DURING INSPECTION, THE CENTER FUSELAGE I FLOOR STRUCTURE HAT BEAM AT FRAME 23 STATION WAS FOUND CORRODED. MAINTENANCE REPLACED THE CENTER FUSELAGE I FLOOR STRUCTURE HAT BEAM AT FRAME 23. THE NEW PART WAS INSTALLED WITH SOLID RIVETS IN ACCORDANCE WITH SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 36 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026