This N-number isn't registered right now. Below is its last known registration, canceled Oct 18, 2019.
Safety record in brief:1 NTSB accident (substantial damage, Oct 2014)6 ADs may apply23 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
The A340 captain's failure to maintain adequate clearance between his wing and the tail of the EMB-145.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA15FA004)
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) |
| 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 |
| 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. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 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. |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
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.
DURING INSPECTION, THE SHEAR CLIP AT FRAME 65 WAS FOUND TO BE CRACKED AT STRINGERS 18L & 19L. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON THE LOWER FWD PAX DOOR STRUCTURE. THE LOWER FWD PAX DOOR STRUCTURE WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10R WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE SHEAR CLIP AT FRAME 81 & STRINGER 10L WAS FOUND TO BE CRACKED. THE SHEAR CLIP WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, A CHAFE WAS FOUND ON THE INNER AFT FACE OF THE MAIN ENTRY DOOR FOLDING FLAP. THE CHAFE WAS REPAIRED IAW ETD 2014-145-034319.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, THE LT AILERON ACTUATOR ATTACH LUG OTBD HAT BUSHING WAS FOUND TO BE MIGRATING AWAY FROM THE LUG. THE LT AILERON PCA FITTING WAS REPLACED IAW SRM 51-20-01 & SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON FRAME 65 AT THE CARGO DOOR FRAME JUST BELOW THE DOOR BUMPER PLATE. THE FRAME WAS REPAIRED IAW ETD 2014-145-034902.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND AROUND THE THE REINFORCEMENT FOR THE BOTTOM DOOR STOP INSIDE THE AFT STRUCTURE OF THE MAIN ENTRY DOOR. THE DOOR STOP WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND ON THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR. THE INNER STRUCTURE OF THE LOWER FWD AREA OF THE MAIN ENTRY DOOR WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING INSPECTION, CORROSION WAS FOUND & A CRACK WAS FOUND ON THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT ON THE MAIN ENTRY DOOR. THE STRUCTURE UNDER THE MIDDLE FWD STAIR SUPPORT WAS REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 23 reports.