Safety record in brief:1 NTSB accident (Jul 2009)16 ADs may apply76 service difficulty reports
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The passenger's failure to comply with crewmember instructions to remain seated while the airplane was in turbulent weather conditions, resulting in an injury to the passenger.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN09LA461)
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.
SUSPECTED CRACK AT RH WING UPPER SKIN N EAR SPOILER #3 INBOARD HINGE. INSTALLED REPAIR DOUBLER REF ETD 2025-170-900513
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON AFT FUSELAGE INTERNAL ON SHEAR CLIP FORWARD INBOARD SIDE AT FR87 BETWEEN ST27R AND 28R ON SHEAR CLIP FORWARD INBOARD SIDE. : REMOVED AND REPLACED NEW SHEAR CLIP AT FR87 BETWEEN ST27R AND 28R REF SRM 51-40-08.
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON SHEAR CLIP FR88 BETWEEN ST27R AND 28R. REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN ST 27R AND 28R REF SRM 51-40-08
From FAA Service Difficulty Reports; matched by N-number and serial number.L/H WING LOWER SKIN CRACKED 16MM LONG AT FASTENER OTBD OF RIB 4A AND AFT OF SPAR 2 (HFEC VERIFIED). PERFORMED TEMPORARY REPAIR BY CUTOUT AND DOUBLER INSTALLATION ON L/H WING LOWER SKIN OTBD OF RIB 4A IN ACCORDANCE WITH, REF ETD2021-170-033505
From FAA Service Difficulty Reports; matched by N-number and serial number.L2 DOOR WILL NOT DISARM. INSPECTED L2 DOOR AND FOUND FLOOR MAT TO BE INTERFERING DOOR MECHANISM. TRIMMED COIN MAT IAW AMM 25-24-01. PERFORMED OPERATIONAL CHECK ON L2 DOOR, OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY MAINT CHECK FOUND CORROSION - SHEAR CLIP FR86 STR27R/28R. REMOVED SHEAR CLIP FR 86, STR 27R/28R REF. SRM 51-40-08. REINSTALLED NEW SHEAR CLIP, REF. SRM 51-40-08. APPLIED TOP COAT REF. SRM 51-23-06. TOP COATED AND CIC REF SRM 51-23-04, 51-23-05, 51-23-06. ACFT REMAINS IN HEAVY CHECK…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK FOUND CORROSION - SHEAR CLIP FR83 STR27R/28R. REMOVED SHEAR CLIP FR 83, STR 27R/28R, INSTALLED FR 83, STR 27R/28R SHEAR CLIP REF. SRM 51-40-08. APPLIED TOP COAT REF. SRM 51-23-06. APPLIED TOP COAT AS REQUIRED REF SRM 51-23-04,51-23-05. 51-23-6. ACFT REMAINS IN HEAVY CHECK UNTIL…
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK - INBOUND DMI - MAJOR REPAIR - FORWARD RT SIDE FUSELAGE NOSE DENT. REPAIRED 3EA DENTS, BETWEEN FRAME- 1/FRAME2 AND STR 26R/27R, BY CUTTING OUT DAMAGE. REPAIR PARTS WERE FABRICATED, LOCATED AND INSTALLED AT FRAME1 - FRAME 2 AND STR 26R/27R. REF SRM 53-10-01/R12, AND PREPPED AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE IN HEAVY CHECK - INBD DEFERAL - MAJOR REPAIR - DENTS IN FUSELAGE BELOW CAPTIONS WINDOW FORWARD OF EXISTING NR 3 REPAIR. PERFORMED PERMANENT REPAIR BY FABRICATING AND INSTALLING DOUBLER AT LT FF FR11-12 STR 15L IN ACCORDANCE WITH REF ETD2017-170-076298.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE IN HEAVY CHECK - MAJOR REPAIR - LT HORIZONTAL STABILIZER RIB 12 CRACKED AS MARKED. REMOVED AND REPLACED RIB 12A ON LT HORIZONTAL STABILIZER AND RESTORED SURFACE PROTECTION REF SRM 51-40-08, 51-23-04, 51-23-05, 51-23-06.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 76 reports.