Safety record in brief:1 NTSB accident (minor damage, Feb 2019)16 ADs may apply135 service difficulty reports
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an inadvertent encounter with convective turbulence that resulted in a TCAS RA, which required an abrupt control input by the flight crew to resolve the conflict.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA19CA081)
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 |
|---|---|---|---|
| 2025-01-05 | Time Limits/ Maintenance Checks | Mar 17, 2025 | Airframe (ERJ 170-200 LR)Certain serial numbers: 17000002; 17000004–17000013; 17000015–17000948 |
| 2023-03-19 | Instruments | Apr 7, 2023 | Airframe (ERJ 170-200 LR)Serial numbers per ANAC AD 2022-05-03 |
| 2023-02-05 | Turbine Engine Combustion Section | Mar 14, 2023 | Engine (CF34-8E5) |
| 2022-16-01 | Windows | Aug 15, 2022 | Airframe (ERJ 170-200 LR)Only with: Equipped with any NORDAM passenger window having PMA P/N NP00038-3. |
| 2020-25-08 | Flight controls | Jan 21, 2021 | Airframe (ERJ 170-200 LR)Serial numbers per ANAC AD 2020-05-01 (ERJ 170) and ANAC AD 2020-05-02 (ERJ 190) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2020-12-12 | Nacelles/ pylons | Aug 13, 2020 | Airframe (ERJ 170-200 LR) |
| 2019-19-03 | Fuselage | Oct 31, 2019 | Airframe (ERJ 170-200 LR)Serial numbers per Embraer Service Bulletins SB170-53-0142 Rev 01, SB190-53-0098 Rev 01, and SB190LIN-53-0072 Rev 01 |
| 2017-21-09 | Fuselage | Nov 27, 2017 | Airframe (ERJ 170-200 LR)Serial numbers per Embraer Service Bulletin 170-53-0051, Revision 03 (ERJ 170); Embraer Service Bulletin 190-53-0019, Revision 03 (ERJ 190) |
| 2016-12-14 | Pneumatic | Jul 27, 2016 | Airframe (ERJ 170-200 LR) |
| 2014-16-05 | Pneumatic | Oct 2, 2014 | Airframe (ERJ 170-200 LR)Serial numbers per EMBRAER Service Bulletin 170-36-0019, dated August 23, 2011 |
| 2013-25-04 | Embraer S.A. Airplanes | Feb 10, 2014 | Airframe (ERJ 170-200 LR)Only with: ERJ 170 airplanes equipped with Goodrich escape slides P/N 4A4030-5; ERJ 190 airplanes equipped with Goodrich escape slides P/N 104003-2. |
| 2013-16-22 | Fuselage | Sep 27, 2013 | Airframe (ERJ 170-200 LR)Serial numbers per Embraer Service Bulletins 170-53-0093 Rev 01, 190-53-0054 Rev 01, and 190LIN-53-0059 Rev 01, dated March 16, 2012 |
| 2013-11-17 | Pneumatic | Aug 6, 2013 | Airframe (ERJ 170-200 LR)Only with: Having Hamilton Sundstrand low pressure check valve (LPCV) P/N 1001447-3 or 1001447-4 installed. |
| 2013-05-12 | Fire Protection | May 3, 2013 | Airframe (ERJ 170-200 LR)Serial numbers per Embraer Service Bulletins 170-26-0011 Rev 02, 190-26-0011 Rev 02, and 190LIN-26-0006 Rev 02 |
| 2013-03-13 | Doors | Mar 19, 2013 | Airframe (ERJ 170-200 LR)Serial numbers per EMBRAER Service Bulletins 170-52-0055 Rev 01, 190-52-0038 Rev 01, and 190LIN-52-0020 |
| 2012-16-09 | Air Conditioning | Sep 21, 2012 | Airframe (ERJ 170-200 LR) |
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.
HORIZONTAL AFT RH HINGE BEARING LUG HAS SCORING AND PITTING ON THE LUG BUSHING AND O/B FACE OF LUG (C-CHECK RO 9/26/2024) REMOVED DAMAGE TO RH HINGE BEARING LUG/INBD FACE ON HORIZONTAL STAB BY REAMING AND SPOT FACING, REF E 175 SRM 55-10-02 , 55-10-08 AND ETD2024-170-024527 REV.: A. TRI HOLE MIKE…
From FAA Service Difficulty Reports; matched by N-number and serial number.LH FLAP TRACK 1A HAS DAMAGE TO RADIUS IN SEVERAL PLACES. ASSET # TC2- 7153 DUE: 11-15-24. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED LH FLAP TRACK 1A. REF AMM 57-54-25. TORQUE WRENCH ID#602 CAL DUE 1-31-25.
From FAA Service Difficulty Reports; matched by N-number and serial number.LH FLAP TRACK 3A O/B HAS WIDTH REDUCTION OF 0.043"- FLAPS DOWN. OUT OF LIMITS. ASSET # TC2- 7153 DUE: 11-15-24 (C-CHECK RO 9/26/2024) REMOVED AND REPLACED L/H #3 OUTBOARD AFT FLAP TRACK. REF AMM 57-57-35. TORQUE WRENCH ID#7543 CAL DUE 5-13-25.
From FAA Service Difficulty Reports; matched by N-number and serial number.HORIZONTAL AFT LH HINGE BEARING LUG HAS SCORING AND PITTING ON THE LUG BUSHING AND I/B FACE OF LUG
From FAA Service Difficulty Reports; matched by N-number and serial number.SHEAR CLIP AT FR.86 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 86 BETWEEN STR. 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
From FAA Service Difficulty Reports; matched by N-number and serial number.SHEAR CLIP AT FR.85 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 85 BETWEEN STR. 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED.
From FAA Service Difficulty Reports; matched by N-number and serial number.SHEAR CLIP AT FR.84 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 84 BETWEEN SRT. 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
From FAA Service Difficulty Reports; matched by N-number and serial number.SHEAR CLIP AT FR.88 BETWEEN STR27R-28R HAS EVIDENCE OF CORROSION. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED SHEAR CLIP AT FR. 88 BETWEEN STR 27R - 28R REF: SRM 51-40-08. SHEAR CLIP REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
From FAA Service Difficulty Reports; matched by N-number and serial number.RH FLAP TRACK 1A HAS DAMAGE IN LOWER INTERNAL RADIUS (NO DAMAGE ALLOWED AREA). (C-CHECK RO 9/26/2024) REMOVED AND REPLACED RH FLAP TRACK 1A. REF. E175 AMM 57-54-25. ASSET# TC1-602, CAL. DATE:1-31-25. SEE CONTINUE CARD FOR GAP CHECK.
From FAA Service Difficulty Reports; matched by N-number and serial number.LH FLAP TRACK 2A I/B HAS THICKNESS REDUCTION OF 0.037" FLAPS UP. ASSET # TC2- 7153 DUE: 11-15-24. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED LH FLAP TRACK 2A I/B. REF. E175 AMM 57-54-25. ASSET# TC2-7401, CAL. DATE: 5-13-25. REMOVED AND REINSTALLED LH FLAP TRACK #2 CARRIAGE. REF. E175 AMM 57-54-28…
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 135 reports.