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Aircraft record

N283SK2001 Embraer EMB-145LR

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 2, 2022.

Safety record in brief:1 NTSB accident (Feb 2013)11 ADs may apply29 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2020
NTSB events
1
2013
ADs may apply
11
confirm with A&P
Service reports
29
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Bank Of Utah Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Mar 25, 2020
Canceled
May 2, 2022
Airworthiness
Standard · Transport
Airworthiness date
Apr 28, 2001

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 data

Airframe

Manufacturer
Embraer
Model
EMB-145LR
Year
2001
Serial number
145424
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
A2DABA

Engine

Make and model
Allison Ae 3007a
Type
Turbo-fan
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
  1. 2020 – 2022Bank Of Utah 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, 2026

NTSB events (1)

Accident

Feb 19, 2013 · Hebron, KY

an inadvertent fall out of the open service door because the safety strap was not attached.

Injuries
Serious
Report
DCA13CA056

From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA13CA056)

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2025-08-07Flight ControlsJun 26, 2025Airframe (EMB-145LR)
2024-26-07FuselageMar 11, 2025Airframe (EMB-145LR)
2021-07-14Main landing gearApr 20, 2021Airframe (EMB-145LR)
2020-16-13Turbine Engine Compressor SectionAug 14, 2020Engine (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.
2007-24-05Rolls-Royce Corporation AE 3007A and AE 3007C Series Turbofan EnginesJan 2, 2008Engine (AE 3007A)
Show all 11 ADs
ADSubjectEffectiveApplies to
2004-22-03Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series AirplanesDec 3, 2004Airframe (EMB-145LR)Serial numbers per EMBRAER Service Bulletin 145-57-0034, Change 01, dated January 9, 2002
2004-04-05Rolls-Royce Corporation (Formerly Allison Engine Company) AE 3007 Series Turbofan EnginesMar 9, 2004Engine (AE 3007A)
2002-14-23Empresa Brasileira de Aeronautica S.A.Aug 2, 2002Airframe (EMB-145LR)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.
2000-09-09EMBRAER Model EMB-145 Series AirplanesJun 16, 2000Airframe (EMB-145LR)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.
2000-09-05Allison Engine Company AE 3007 Series Turbofan EnginesJul 5, 2000Engine (AE 3007A)Only with: Cone shafts P/Ns 23050728 and 23070729 installed.
99-03-03Allison Engine Company Model AE 3007A and AE 3007A1/1 Turbofan EnginesFeb 16, 1999Engine (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 (29)

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 · floor support · corrodedApr 26, 2016

    FLOOR STRUCTURE MIDDLE GUSSET CORRODED. R & R CF1 FLOOR STRUCTURE MIDDLE GUSSET 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 · corrodedApr 26, 2016

    CF1 FLOOR STRUCTURE MIDDLE ANGLE SUPPORT CORRODED. R & R CF1 FLOOR STRUCTURE MIDDLE SUPPORT WITH SOLID RIVETS IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door sill · corrodedApr 26, 2016

    CF1 FLOOR STRUCTURE FWD AND AFT SERVICE DOOR SILL CORRODED. CF1 FLOOR STRUCTURE FWD DOOR SILL REPAIRED IAW SRM 53-21-10. CF1 FLOOR STRUCTURE AFT SILL OF SERVICE DOOR REPAIRED IAW SRM 53-21-10.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Doors · structure · corrodedApr 26, 2016

    PASSENGER DOOR LOWER STRUCTURE FWD AND AFT U-SHAPE ANGLE CORRODED. R & R PASSENGER DOOR LOWER STRUCTURE FWD AND AFT U-SHAPE ANGLES AND INSTALLED WITH SOLID RIVETS IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery · dischargedJul 26, 2014

    DURING INSPECTION THE EMER LIGHTS AFT OF ROW 12 WERE FOUND TO BE INOPERATIVE. REPLACED THE NR 3 EMER LIGHT BATTERY. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Hydraulic power · hydraulic system · low pressureMar 29, 2014

    CREW REPORTED THAT AFTER TAKEOFF, RECEIVED A HYD SYS 1 LOW QTY MSG DURING GEAR RETRACTION. RETURNED TO FIELD & LANDED WITHOUT INCIDENT.. SERVICED HYD SYS 1. FURTHER, INSPECTIONS WERE COMPLETED ON THE FLIGHT CONTROLS, THE BRAKE SYS, THE HYD SYS, THE SPOILER & ENG 1. NO LEAKS WERE NOTED & THE ACFT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · bentOct 10, 2013

    DURING INSPECTION, FRAME 72 WAS FOUND TO BE BENT BETWEEN STRINGERS 15R AND 16R. THE FRAME WAS REPAIRED IAW ETD 2013-145-048739.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · shear tie · crackedOct 10, 2013

    DURING INSPECTION, A CRACK WAS FOUND IN THE SHEAR TIE AT FRAME 73 BETWEEN STINGERS 7 & 9R. THE SHEAR TIE WAS REPLACED IAW SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ice and rain protection · b-nut · looseApr 12, 2013

    CREW REPORTED BLEED SYSTEM 1 LEAK MESSAGE ON EICAS ON CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND LOOSE WING ANTI-ICE B-NUT AND TIGHTENED. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · inoperativeJan 7, 2013

    DURING INSPECTION, THE EMERGENCY LIGHT FLOOR PROXIMITY STRIPS WERE FOUND TO BE INOPERATIVE AT ROW 8. MAINTENANCE REPLACED THE EMERGENCY FLOOR PROXIMITY LIGHT STRIP AT ROW 8. OPERATIONAL CHECKS WERE GOOD WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 29 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

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