Safety record in brief:1 NTSB incident (Jun 2018)6 ADs may apply198 service difficulty reports
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The local controller failing to follow established facility directives and issuing a clearance for takeoff from a runway not under his control.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for OPS18IA014)
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 APP NOTICED OIL/RUBBER BURNING SMELL IN FLT DECK AT ABOUT 2000 FT. PERFORMED E1 & E2 HIGH POWER RUN IAW MAINTENANCE RUNUP CHECKLIST. NO DEFECTS NOTED DURING RUNUP. A/C OK FOR SERVICE AT THIS TIME.
From FAA Service Difficulty Reports; matched by N-number and serial number.CREW NOTIFIED CLT MX OF EXHAUST FUMES IN COCKPIT. CLT MX CREW REPORTED SMELL IN COCKPIT, CABIN NORMAL, FUTHER TROUBLESHOOTING FOUND APU BLEED CAUSE OF FUMES AND WAS PUT ON MEL. A/C DEPARTED WITH NO FURTHER ISSUES IN FLIGHT.
From FAA Service Difficulty Reports; matched by N-number and serial number.OIL SMELL IN FLIGHTDECK FROM PACK 1. FACT 27JUL26 01:02 CLT INSPECTED PAX 1. FOUND TO BE GOOD. FOUND PAX 2 TO HAVE MELTED DUCT. REMOVED AND REPLACED DUCT AS REQUIRED. PERFORMED OP CHECK IAW 21-51-00. OP CHECK GOOD. NO DEFECTS NOTED A/C OKAY FOR SERVICE
From FAA Service Difficulty Reports; matched by N-number and serial number.COCKPIT UNDERFLOOR HATCH 123BL HAS TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL. REPAIRED COCKPIT UNDERFLOOR HATCH 123BL TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL IAW PIEDMONT EO1-52-26-0223 AND ETD2026-145-007987.
From FAA Service Difficulty Reports; matched by N-number and serial number.LAVATORY RT HAT BEAM AT FR 59-60, CRACK ON FWD END OF NUT-PLATE. PERFORMED DOUBLER REPAIR FOR LAVATORY R/H HAT BEAM AT FR 59-60 IAW ETD2026-145-007317 AND SRM 53-24-10RE
From FAA Service Difficulty Reports; matched by N-number and serial number.GALLEY FLOOR, FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L AROUND NUT PLATE HOLE HAS CORROSION. PERFORMED DOUBLER ON GALLEY FLOOR FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L IAW EMB 145 SRM 53-21-10RE ITEM 2 FIG. 201 SHEET 5 DETAIL C AND EO1-05-26-0232.
From FAA Service Difficulty Reports; matched by N-number and serial number.STRINGER 19R (INTERIOR STRINGER) STRINGER SPLICE BETWEEN FR 52/53 CHAFED. REMOVED AND REPLACED STGR 19R SPLICE BTW FR 52-53 IAW EMB 145 SRM 51-40-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.CRACKED FRAME 72, BETWEEN STRINGER 17L AND 16L. R & R FRAME 72 IAW ETD-2026-145-007557 AND EO1-53-26-0206.
From FAA Service Difficulty Reports; matched by N-number and serial number.FOUND CRACKS ON LH OMEGA BEAM #2 AT FR 29. PERFORMED CUT-OUT OF DAMAGE, AND DOUBLER REPAIR TO LT OMEGA BEAM #2 AT FR 29 IAW EMB ETD2026-145-007261 AND EO1-53-26-0215.
From FAA Service Difficulty Reports; matched by N-number and serial number.MAIN DOOR LOWER FRAME AFT NUTPLATE HOLE DOUBLER HAS NO DTA INFORMATION. REPAIR WAS ACCOMPLISHED IAW ETN-EM-52-041. RE-ACCOMPLISHED DOUBLER FOR REPAIR OF MAIN DOOR LOWER FRAME AT AFT NUT-PLATE HOLE IAW SRM 52-10-04RE, ITEM 3, FIG 201, SHEET 3 AND EO1-52-26-0199.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 198 reports.