Safety record in brief:1 NTSB accident (substantial damage, Jul 2025)16 ADs may apply44 service difficulty reports
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The captain’s decision to continue the landing after the bounce and the subsequent misapplication of pitch controls. Contributing to the accident was the ongoing “land and hold short” operations that may have created an urgency to land.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for DCA25LA286)
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.
FOUND CRACK AT RT WING MAIN BOX, LOWER SKIN, AT SPAR II RIB 4A JUNCTION. REMOVED OLD DOUBLER, CUTOUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW ETD2026-170-015132 REV.A. REF. NRWC VP-041666-2026/1-1 THROUGH NRWC VP-041666-2026/1-11
From FAA Service Difficulty Reports; matched by N-number and serial number.CARGO FIRE SYSTEM FAIL MSG IN FLIGHT. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FWD CARGO FIRE BOTTLE.
From FAA Service Difficulty Reports; matched by N-number and serial number.SUSPECT CABIN PRESSURIZATION PROBLEM AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MX DETERMINED THIS IS NORMAL OPERATIONS.
From FAA Service Difficulty Reports; matched by N-number and serial number.TAIL STRIKE DAMAGE BETWEEN STR 28L TO 28R AND FRAME 99 TO FRAME 100.REPAIRED STRINGERS AND FRAME IAW AERNNOVA TI-170-25-149 AND ETD2025-170-924890 REV A AND ETD2025-170-925103 REV A. ALSO REF EAMS WO # 10104 FOR WORK ACCOMPLISHED.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING THE EVALUATION OF PROTRUDING DENT LOCATED AT FR90/91 STGR 28L FOUND CORROSION ON END OF STRINGER 28L. PERFORMED STRINGER SPLICE REPAIR ON STGR 28L BETWEEN FRAMES 88-91 AND RESTORED SURFACE PROTECTION TO REWORKED AREA REFER ETD2025-170-900446.
From FAA Service Difficulty Reports; matched by N-number and serial number.FRAME 90 CORRODED BETWEEN STRINGERS 29L-28R.REMOVED AND REPLACED FRAME 90 FROM STRINGER 19L-19R. REF. EMB SRM 51-40-08
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON SHEAR CLIP FR 90 29L-28L. REMOVED AND REPLACED SHEAR CLIP AT FR.90 STGRS 29L - 28L REF EMB 170/175 SRM 51-40-08
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION ON STRINGER 23L BETWEEN FRAMES 83-84.REPAIRED STRINGER 23L, BETWEEN FR 86- 87 AND BETWEEN FR 81 - 82. REF EMB ETD2022--170-014482
From FAA Service Difficulty Reports; matched by N-number and serial number.DRILL DAMAGE TO L2 DOOR PROTECTIVE PLATE AND FUSELAGE @ FRAME 88 STR 18L. PERFORMED PERMANENT REPAIR TO DRILL DAMAGE ON FUSELAGE SKIN IAW ETD2022-170--0142691.
From FAA Service Difficulty Reports; matched by N-number and serial number.STRINGER 21L CORRODED BETWEEN FRAMES 88-89. PERFORMED STRINGER 21L REPAIR BETWEEN FR83 AND FR90 REF ETD2022-170-013734
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 44 reports.