Safety record in brief:1 NTSB incident (Jun 2009)6 ADs may apply75 service difficulty reports
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The local controller did not visually scan the runways and ensure that the E145 had crossed runway 24L prior to issuing a takeoff clearance to the DH8, did not ensure separation between the two airplanes, and did not cancel takeoff clearance for the DH8 in a timely manner.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for OPS09IA009)
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-145XR) |
| 2024-26-07 | Fuselage | Mar 11, 2025 | Airframe (EMB-145XR) |
| 2021-07-14 | Main landing gear | Apr 20, 2021 | Airframe (EMB-145XR) |
| 2004-22-03 | Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 and -145 Series Airplanes | Dec 3, 2004 | Airframe (EMB-145XR)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-145XR)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-145XR)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.
RH AFT OVER WING EMERGENCY LIGHT IS INSTALLED UPSIDE DOWN. RE-INSTALLED RH EXTERNAL EMERGENCY LIGHT REFLECTOR.
From FAA Service Difficulty Reports; matched by N-number and serial number.O2 MASK WONT TEST. RESECURED O2 MASK BOX. OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.EXTERNAL EMERGENCY MAIN DOOR LIGHT INOPERATIVE. REMOVED AND REPLACED EXTERNAL EMERGENCY MAIN DOOR LIGHT. OPS CHECK SAT
From FAA Service Difficulty Reports; matched by N-number and serial number.TYS- CRACK ON FRAME FWD OF LH COCKPIT CEILING SPEAKER BETWEEN FRAME 10-11. THE CRACKED SECTION WAS REMOVED A SUPPORT AND SPLICE WERE FABRICATED AND INSTALLED IAW ENGINEERING DOCUMENT PROVIDED.
From FAA Service Difficulty Reports; matched by N-number and serial number.ACTUATOR ATTACH POINT ON R/H GROUND SPOILER HAT BUSHING MISSING. REAMED BOTH BUSHING HOUSINGS, INSTALLED NEW HAT BUSHINGS. AIRCRAFT STILL IN C CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number.TYS A/C WAS FOUND WITH THE NLG UP LOCK SUPPORT FRAME ON THE AFT SIDE CRACKED. MAINTENANCE REPLACED THE UP LOCK SUPPORT BRACKET IAW EMB 145XR SRM 51-40-02. ALL WORK ACCOMPLISHED AND WAS RELEASED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE CREW REPORTED STRONG OIL ODOR DURING DESCENT WHEN THROTTLES WERE AT IDLE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.IAH - DURING INSPECTION THE FORWARD RADIO ALTIMETER ANTENNA WAS FOUND TO HAVE CORROSION INSIDE THE BASE IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED THE CORRODED SKIN BETWEEN FRAMES 64-65 STR 21L-21R, PERFORMED HFEC WITH NO DEFECTS NOTED AND INSTALLED A FILLER / DOUBLER REPAIR. OPERATIONAL CHECKS…
From FAA Service Difficulty Reports; matched by N-number and serial number.IAH - DURING INSPECTION THE FORWARD RADIO ALTIMETER ANTENNA WAS FOUND TO HAVE CORROSION INSIDE THE BASE IN THE CARGO COMPARTMENT. MAINTENANCE REMOVED THE CORRODED SKIN BETWEEN FRAMES 68-69 STR 21L-21R, PERFORMED HFEC WITH NO DEFECTS NOTED AND INSTALLED A FILLER / DOUBLER REPAIR. OPERATIONAL CHECKS…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING MX INSPECTION THE EMERGENCY LIGHT OVER SEAT 18A WAS INOP. MX REMOVED AND REPLACED THE BULB WITH OPS CHECK GOOD. A/C WAS APPROVED FOR RETURN TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 75 reports.