Safety record in brief:1 NTSB accident (Aug 2014)16 ADs may apply95 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 capabilities of the beverage cart were exceeded which resulted in the cart toppling over and fracturing the flight attendant's foot.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA14CA155)
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.
DURING HEAVY CHECK FWD CABIN WET AREA RH IB SEAT TRACK BETWEEN FR 12 TO 20 FOUND WITH CORROSION. FWD CABIN WET AREA RH IB SEAT TRACK BETWEEN FR12 TO 20 REMOVED AND REPLACED IAW SRM 51-43-01 AND 51-41-02.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK LT WING SLAT 2 IB TRACK CUTOUT FOUND CRACKED. LT WING SLAT 2 IB TRACK CUTOUT REPAIRED IAW ETD2026-170-010336. HFEC PERFORMED AFTER REPAIR WITH NO CRACK FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK RT WING SLAT 2 IB TRACK CUTOUT FOUND CRACKED. RT WING SLAT 2 IB TRACK CUTOUT REPAIRED IAW ETD2026-170-010336. HFEC PERFORMED AFTER REPAIR WITH NO CRACK FOUND.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK MULTIPLE AREAS OF CORROSION AROUND PREVIOUSLY BLENDED AREAS OF AFT PAX DOOR THRESHOLD BEAM LOCATED AROUND THE FWD AND AFT EVACUATION SLIDE GIRT BAR CUTOUT, FWD AND AFT SERRATED SHIMS. L2 AFT PAX DOOR THRESHOLD BEAM HAS BEEN REPLACED IAW SRM 51-41-01, SRM 51-43-03 AND SRM 51-43-04.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK MAINTENANCE FOUND LIGHTENING STRIKE THICKNESS REDUCTION AT FR02. CARRIED OUT PERMANENT REPAIR ON EXTERNAL FUSELAGE SKIN AT FWD FUSELAGE FR2 BETWEEN CENTER STRGR AND STGR 2L IAW ETD2025-170-922426 REV B.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING HEAVY CHECK MAINTENANCE FOUND CRACK ON RH LOWER WING SKIN SURFACE BETWEEN RIB 5-6 AND STRGR 18. RT WING LOWER SKIN SURFACE BETWEEN RIB 5-6 AND STRGR 18 REPAIRED IAW ETD2026-170-009575.
From FAA Service Difficulty Reports; matched by N-number and serial number.EMERGENCY LIGHT BATTERY FAILED FUNCTIONAL CHECK. R&R EMERGENCY LIGHT BATTERY 2.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE IN HEAVY CHECK - R/H WING LOWER SKIN AT RIB 4A HAS CRACK. PERFORMED TEMPORARY REPAIR BY CUTOUT, FILLER/DOUBLER REPAIR ON RH WING LOWER SKIN AT RIB 4A IN ACCORDANCE WITH, REF ETD2023-170-031160.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE IN HEAVY CHECK - AFT SERVICE DOOR AFT EVACUATION SLIDE FITTING SERRATED SLIDE SHIM FORWARD NUT HOLDER PLATE HAS SIGNS OF CORROSION ON BOTTOM SIDE OF LOWER BEAM. REMOVED AND REPLACED AFT SERVICE DOOR LOWER BEAM AND AFT EVACUATION SLIDE FITTING FWD NUT HOLDER PLATE.
From FAA Service Difficulty Reports; matched by N-number and serial number.WHILE IN HEAVY CHECK - MAIN CABIN AFT WET AREA RIGHT SIDE FR 84 CROSS BEAM FLOOR STRUCTURE HAS (2) CORROSION SPOTS AND (2) CORRODED FASTENERS AS MARKED. PERFORMED L ANGLE SPLICE REPAIR ON MAIN CABIN AFT WET AREA R/H FR 84 CROSS BEAM. REF: SRM ETD2023-170-031600
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 95 reports.