Safety record in brief:1 NTSB incident (minor damage, Dec 2016)16 ADs may apply36 service difficulty reports
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A failure of the nose landing gear down lock spring which precluded normal downlock operation of the nose landing gear. The spring failure was due to the presence of too much retained austenite which led to the formation of progressive cracking and subsequent failure of the spring.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for ENG17IA005)
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.
INSPECTED SKIN DEFORMATION/DENT OBSERVED BTWN FR10 & FR12, STR 14 THROUGH STR 16, DAMAGED AREA INITIATES APPROX 2.00 IN FWD OF FR10 & EXTENTS AFT TO FR12. OVERALL AFFECTED AREA MESSURES 27.0 IN IN LENGTH & 7 INCHES IN WIDTH, WITH A MAX DEPTH OF 0.204 IN ALONG WITH A DENT/GOUGE LOCATED AT STR 15 &…
From FAA Service Difficulty Reports; matched by N-number and serial number.L/H FLAP TRACK #2A OUTBOARD HAS WIDTH REDUCTION DAMAGE WITH A MAXIMUM LOSS OF .40 MM. TC2-8916 CAL DUE 11-20-24. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH #2A OB FLAP TRACK REF EMB AMM 57-54-25-400-801-A TW: TC2-7543 CAL DUE: 05/13/2025
From FAA Service Difficulty Reports; matched by N-number and serial number.CORROSION, AFT WET AREA, ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 7/22/2024) PERFORMED PERMANENT SPLICE REPAIR ON RH INBD FLOOR BEAM SEAT TRACK FR 83-84 REF. ETD2022-170-022163 REV. B. CHANGE IN WEIGHT MEASURES 308.96 GRAMS. WEIGHT LESS THAN 2.5 LBS, NO WEIGHT AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.LH OB LATERAL SEAT TRACK FROM FR 74 TO FR 84 HAS CORROSION AS MARKED. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH OB LATERAL SEAT TRACK FROM FR 74 TO FR 84 REF EMB SRM 51-40-08. SEAT TRACK REPLACED WITH OEM PART NO CHANGES TO WEIGHT AND BALANCE NOTED
From FAA Service Difficulty Reports; matched by N-number and serial number.MAIN CABIN FLOOR STRUCTURE LEFT OUTBOARD SEAT TRACK SECTION FR 34/43 - 59 HAS GOUGING AT FRS 45, 47, 51, 53, 55, 57 AND 59. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED LH OB SEAT TRACK FR 34-59 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. PART WAS REPLACED WITH OEM PART NO…
From FAA Service Difficulty Reports; matched by N-number and serial number.RH IB FLOOR SEAT TRACK HAS MULTIPLE AREAS WHERE CORROSION IS PRESENT AS MARKED FR 23- FR 34 (C-CHECK RO 7/22/2024) REMOVED AND REPLACED RH IB FLOOR SEAT TRACK FR 23- FR 34 REF EMB SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
From FAA Service Difficulty Reports; matched by N-number and serial number.LH IB FLOOR SEAT TRACK HAS MULTIPLE AREAS WHERE CORROSION IS PRESENT AS MARKED FR 30- FR 34 (C-CHECK RO 7/22/2024) REMOVED AND REPLACED R/H I/B SEAT TRACK BETWEEN FR23 - FR34 REF: SRM 51-40-08. 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 AND STR 28 CORRODED. (C-CHECK RO 7/22/2024) REMOVED AND REPLACED SHEAR CLIP AT FR 84 BETWEEN STR 28R -27R REF: SRM 51-40-08
From FAA Service Difficulty Reports; matched by N-number and serial number.TRANSFER FROM EAML 1239521 : WRITE UP FROM EAML 1239214. FOUND GOUGE IN SKIN AT FRAME 20.5 AND STRINGER 9 TO BE .042" DEEP, 1.5 INCHES LONG, AND 0.249 INCHES WIDE. (FILED CLOSED)REPAIR ACCOMPLISHED BY MHIRJ REFER TO SOW MIS-4505 DATED 11/11/2023 - I/A/W ETD 2023-170-027824 REV B DATED NOV 8 2023
From FAA Service Difficulty Reports; matched by N-number and serial number.LH LOWER FUSELAGE FRAME 52 L-ANGLE HAS A CRACK EMANATING FROM THE OUTBOARD MOST RIVET. (C-CHECK RO 10/28/2021) REMOVED AND REPLACED L-ANGLE AT LH LOWER FUSELAGE FRAME 52. / REF SRM 51-40-08
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 36 reports.