This N-number isn't registered right now. Below is its last known registration, canceled Jul 29, 2024.
Safety record in brief:1 NTSB accident (substantial damage, May 2012)4 ADs may apply59 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 B747 Captain's failure to maintain a safe clearance between his wing and the tail of the EMB135 that was stopped on a taxiway.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA12CA082)
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.
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.
MAIN DOOR EXIT SIGN INOP. C/A-REMOVED AND REPLACED NR 1 INVERTER IAW AMM 33-50-11 OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.STRONG FUEL ODOR ON FLIGHT DECK AFTER PACK 2 WAS RUNNING ON APU-C/A-SHUT DOWN AND TURNED ON APU IAW GHC. CYCLED THROUGH THE AIR CONDITION PACKS IAW AMM 21-20-00. NO SMELL DETECTED BY MECHANIC AND CREW. PERFORMED GVI OF APU AND APU INLETS AND EXHAUST AND ALL APU LINES IAW 49-15-01. PERFORMED GVI OF…
From FAA Service Difficulty Reports; matched by N-number and serial number.E2 FIRE DET FAIL-C/A-C/W FIM TASK 26-11-00-810-804-A ENG FIRE LOOP CHECKS BAS. REMOVED AND REPLACED E2 ENGINE FIRE DETECTOR LOOP IAW ERJ 140 AMM 26-11-01. OCK GOOD AT THIS TIME. P/N 3601-133-500/230 S/N 227642
From FAA Service Difficulty Reports; matched by N-number and serial number.LH EXT EMERGENCY LIGHT INOP-C/A-RAR LH EXT EMERGENCY LIGHT IAW EMB140 AMM 33-50-10. OPC GOOD. NO DEFECTS NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.BRAKE FLUID FOUND ON RIGHT MAIN BRAKE SMOKING BADLY ALL BRAKE LINES APPEARED WET AND LOUD CRACKING SOUND COMING FROM WHEEL NR 3. EFR RESPONDED AND DETERMINED IT REQUIRED TO BE SPRAYED DOWN. SUSPECT BRAKE FLUID LEAK ON. HYDRAULIC LEAK ON BRAKE PAD. PERFORMED GVI OF RIGHT MAIN BRAKE ASSEMBLY LINES…
From FAA Service Difficulty Reports; matched by N-number and serial number.SUPPLEMENTAL SMOKKING BRAKE NR 3 MLG BRAKE ASSY REQUIRES REPLACEMENT DUE TO RAPID COOLING BY CINCINNATI FIRE DEPARTMENT-C/A-REMOVED AND REPLACED NR 3 MLG WHEEL ASSY IAW W/C 32-700-11 AND PERFORMED CARBON BRAKE INSPECTION IAW W/C 32-700-18. REMOVED AND REPLACED NR 3 MLG BRAKE ASSY. IAW W/C…
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT EXTERIOR OVERWING EMERGENCY LIGHT FAILED TO ILLUMINATE. R & R THE LAMP IAW AMM 33-50-10. OPS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.MAIN DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-50-10-000-801-A AND 33-50-10-400-801-A, OPS CHECKED GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.SURFACE CORROSION FOUND ON SKIN JOINT STRAP AT FRAME 13 BETWEEN STRINGERS 21L AND 21R. SKIN STRAP AT FR 13 BLENDED IAW SRM 51-10-05 REF FCBS 53-10-14-001 BLEND DIMENSION L 2.800 X W 2500" X D 0.004 IS OUT OF LIMITS IAW SRM 51-10-05 AT FRAME 13 BETWEEN STRINGERS 21L AND 21R. SKIN JOINT STRAP…
From FAA Service Difficulty Reports; matched by N-number and serial number.RT SILL NUMBER 2 CORRODED AT SEVERAL PLACES. RT SILL NUMBER 2 BLEND IAW SRM 51-10-03 AND FOUND ( OUT OF LIMITS) IAW SRM 53-22-10. RT SILL NUMBER 2 REPLACED IAW SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 59 reports.