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Aircraft record

N285SK2001 Embraer EMB-145LR

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Aug 30, 2018.

Safety record in brief:No NTSB accidents or incidents since 198211 ADs may apply37 service difficulty reports

Registration
Deregistered
Last based in
St Louis, MO
owner city / state
Owners
1
since 2018
NTSB events
None
since 1982
ADs may apply
11
confirm with A&P
Service reports
37
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Avtran LLC
Owner type
Corporation
City, state
St Louis, MO
Certificate issued
Aug 28, 2018
Canceled
Aug 30, 2018
Airworthiness
Standard · Transport
Airworthiness date
May 24, 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
145435
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
A2E228

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. 2018Avtran LLCSt Louis, MO

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

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 (37)

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 · switch · faultyFeb 3, 2014

    CREW REPORTED THAT THEY RECEIVED A BLEED 1 VLV CLOSED MESSAGE DURING FLIGHT. THE CREW RETURNED TO FIELD & AND LANDED WITHOUT INCIDENT. REPLACED THE BLEED 1 PUSHBUTTON SWITCH. OPERATIONS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · light · odorDec 20, 2013

    CREW REPORTED ELECTRICAL SMELL FROM ROW 7. MX TROUBLE SHOT THE ISSUES TO THE CEILING LIGHT AT ROW 7A. THE LIGHT IS CURRENTLY ON DEFERRAL & THE FINAL CORRECTIVE ACTION & PART INFORMATION WILL BE SUBMITTED AS A SUPPLEMENT TO THIS REPORT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery · inoperativeJul 2, 2013

    DURING INSPECTION, NR 4 AND 5 EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. MX REPLACED EMERGENCY LIGHT BATTERY AND OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Ice and rain protection · transducer · failedFeb 24, 2013

    CREW REPORTED A NR 1 ENGINE ANTI-ICE VALVE FAIL MESSAGE IN FLIGHT. DIVERTED TO AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ANTI-ICING PRESSURE TRANSDUCER. OPS CHECKED GOOD WITH NO FURTHER DEFECTS NOTED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · chafedFeb 2, 2013

    DURING INSPECTION, THE PASSENGER DOOR CUTOUT INTERNAL SKIN WAS CHAFED AT THE LOWER HOLE FOR THE LEFT COCKPIT BULKHEAD. THE SKIN WAS REPAIRED IN ACCORDANCE WITH IC2006-145-4495-C.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · corrodedFeb 2, 2013

    DURING INSPECTION, CORROSION WAS FOUND ON THE SHEAR CLIP AT FRAME 60 BETWEEN STRINGERS 19R AND 20R. THE SHEAR CLIP WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedFeb 2, 2013

    DURING INSPECTION, CORROSION WAS FOUND ON THE THE SKIN BETWEEN FRAMES 38 AND 39 AND STRINGERS 21R AND 21L. THE SKIN WAS REPAIRED IN ACCORDANCE WITH ETD 2013-145-002043.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · sill · corrodedFeb 1, 2013

    DURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OUTBOARD SILL FROM FRAME 23 TO FRAME 29. THE LEFT OUTBOARD SILL AT FROM FRAME 23 TO FRAME 29 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · sill · corrodedFeb 1, 2013

    DURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT OUTBOARD SILL FROM FRAME 41 TO FRAME 48. THE RIGHT OUTBOARD SILL FROM FRAME 41 TO FRAME 48 WAS REPLACED IN ACCORDANCE WITH SRM 51-40-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery · dischargedJan 12, 2013

    DURING INSPECTION, THE FLOOR PROXIMITY LIGHT STRIP FORWARD OF THE EMERGENCY EXIT WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE NUMBER 3 EMERGENCY LIGHT BATTERY. 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 37 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

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