N285SK2001 Embraer EMB-145LR
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
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 dataAirframe
- 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- 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, 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-145LR) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145LR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145LR) |
| 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-145LR)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-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. |
| 2000-09-09 | EMBRAER Model EMB-145 Series Airplanes | Jun 16, 2000 | Airframe (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. |
| 2000-09-05 | 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 (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 reportsShow fewer 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