N373SK2001 Embraer EMB-135KL
This N-number isn't registered right now. Below is its last known registration, canceled Oct 18, 2016.
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply28 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
- Oct 18, 2016
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jan 4, 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
- 2001
- Serial number
- 145543
- 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
- A4408A
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- 2016Wells 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 (28)
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.
- Pneumatic · air filter · dirtyJul 8, 2014
THE CREW REPORTED THAT DURING CLIMB THEY RECEIVED A BLEED 2 OVERTEMP MSG IN ICING CONDITIONS. THE ACFT WAS DIVERTED & LANDED WITHOUT FURTHER INCIDENT. MX CLEANED DEBRIS FROM THE ENG 2 FAN AIR VLV FILTER. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · control unit · faultyJun 1, 2014
CREW REPORTED THAT UPON LANDING THAT THE BRAKING SYS SEEMED TO BE UNRESPONSIVE. THE BRAKING SYS WORKED NORMALLY AT LOW SPEEDS & THE ACFT TAXIED TO THE GATE UNEVENTFULLY. MX REPLACED THE BRAKE CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · proximity switch · dirtyJan 9, 2014
CREW REPORTED THAT THE ACFT HAD A SLIGHT UNINTENDED ROLL TO THE LT DURING DESCENT. THE CREW FURTHER REPORTED THAT THE SPOILERS SHOWED OPEN WITH THE HANDLE IN THE CLOSED POSITION. THE SITUATION WAS REMEDIED & THE ACFT LANDED WITHOUT FURTHER INCIDENT. PERFORMED THE GND SPOILER SYS ADJUSTMENT TEST…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · fitting · damagedNov 22, 2013
LEFT AILERON PCA FITTING HOLES WERE FOUND TO BE ELONGATED. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · fitting · damagedNov 21, 2013
RIGHT AILERON PCA FITTING HOLES WERE FOUND TO BE ELONGATED. THE RT AILERON PCA FITTING WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · fitting · damagedNov 21, 2013
LEFT AILERON DAMPER LUG HOLES WERE FOUND TO BE ELONGATED. THE AILERON DAMPER FITTING WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Air conditioning and pressurization · unknown · odorOct 18, 2013
CREW REPORTED THAT THERE WAS A BURNING ODOR IN THE CABIN, DURING FLIGHT AROUND ROW 5. CREW TURNED BOTH PACK SYSTEMS AND THE RECIRCULATION FAN OFF AND THE ODOR DISSIPATED. THE FLIGHT LANDED NORMALLY WITHOUT INCIDENT. MAINTENANCE INSPECTED ALL LIGHTING BALLASTS WITH NO DEFECTS NOTED. THE PACK…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · dentedApr 25, 2012
DURING INSPECTION, A DENT WAS FOUND ON CENTER FUSELAGE IV SKIN BETWEEN FRAME 59 AND FRAME 60, AND STRINGERS 12R AND 13R. THE CENTER FUSELAGE IV SKIN BETWEEN FRAME 59 AND FRAME 60, AND STRINGERS 12R AND 13R, WAS REPAIRED IN ACCORDANCE WITH SRM 53-24-01.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · skin · debondedApr 24, 2012
DURING INSPECTION, THE RIGHT INBOARD FLAP TRAILING EDGE AND LOWER SKIN WERE FOUND TO BE DISBOUND. MAINTENANCE REPAIRED THE RIGHT INBOARD FLAP TRAILING EDGE UPPER AND LOWER SKIN IN ACCORDANCE WITH ETD 2012-145-005883 REVISION B.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · angle · crackedApr 23, 2012
DURING INSPECTION, THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES WERE FOUND TO BE CRACKED. THE CENTER FUSELAGE III RIGHT OMEGA BEAM ANGLES WERE REPAIRED IN ACCORDANCE WITH SRM 53-23-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 28 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