# Service difficulty reports: N128SY A list on [N128SY](https://openairdocs.org/aircraft/N128SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2024081208](https://openairdocs.org/sdr/SWIA2024081208.md): Skin · damaged · Aug 8, 2024 · N128SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > COMPLY WITH REPAIR AUTHORIZATION: RA92795-ETD2024-170-019819 MXCODEID76651-PR - SKIN DAMAGE ON FORWARD FUSELAGE SKIN FR18-FR19 AND STGR 21R- STGR22R. PER ETD ETD2024-170-019819 PERFORM PERMANENT REPAIR. DUE AT 14559 CYCLES, PART NUMBER:, SERIAL NUMBER:, POS - [SDR SWIA2023010567081](https://openairdocs.org/sdr/SWIA2023010567081.md): Hinge · worn · Dec 17, 2022 · N128SY · Emb ERJ170200LR · Elevator Structure > LEFT ELEVATOR HINGE 2 AND 3 HARDWARE WORN. REPLACED LT ELEVATOR HINGE 2 AND 3 HARDWARE ON RACK SEE CP25810196 FOR FINAL INSTALL IAW AMM 27-31-05. - [SDR SWIA2023010567080](https://openairdocs.org/sdr/SWIA2023010567080.md): Flap Track · out of limits · Dec 16, 2022 · N128SY · Emb ERJ170200LR · Trailing Edge Flaps > L/H I/B FLAP TRACK 2A O/B HAS WIDTH REDUCTION OF.040. OUT OF LIMITS OF SRM 57-52-03/AD01. REMOVED AND RELPACED L/H I/B FLAP TRACK 2A O/B. REF E175 AMM 57-45-25. - [SDR SWIA2023010567079](https://openairdocs.org/sdr/SWIA2023010567079.md): Flap Track · worn · Dec 16, 2022 · N128SY · Emb ERJ170200LR · Ailerons > L/H I/B FLAP TRACK 1A HAS THICKNESS REDUCTION OF.030". LENGTH OF DAMAGE IS.6". REMOVED AND REPLACED LH I/B FLAP TRACK 1A REF EMB 175 AMM 57-54-25. - [SDR SWIA2023010567078](https://openairdocs.org/sdr/SWIA2023010567078.md): Flap Track · out of limits · Dec 16, 2022 · N128SY · Emb ERJ170200LR · Trailing Edge Flaps > R/H I/B FLAP TRACK 2A HAS WIDTH REDUCTION OF.042". OUT OF LIMITS OF SRM 57-52-03/AD01. ASSET TC2-7153 DUE 11-17-23. REMOVED AN REPLACED R/H I/B FLAP TRACK 2A REF. E175 AMM 57-54-25. - [SDR SWIA2023010567077](https://openairdocs.org/sdr/SWIA2023010567077.md): Flap Track · gouged · Dec 16, 2022 · N128SY · Emb ERJ170200LR · Trailing Edge Flaps > R/H I/B FLAP TRACK 1A HAS THICKNESS REDUCTION OF.029" WITH A GOUGE IN RADIUS OF TRACK. (C-CHECK RO 1/3/2023).REMOVED AND REPLACED RH I/B FLAP TRACK 1A REF EMB 175 AMM 57-54-25.ASSET# TC2-552 CAL DUE 4/7/23. - [SDR SWIA2023010567076](https://openairdocs.org/sdr/SWIA2023010567076.md): Seat Track · corroded · Dec 15, 2022 · N128SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CABIN RH SEAT TRACK BEAM CORRODED AT SEAT TRACK FLOOR BETWEEN FR 31-31. (C-CHECK RO 1/3/2023) REMOVED AND REPLACED RH I/B SEAT TRACK BEAM FR 23 - 34 REF EMB 175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS ACTION DOES NOT EFFE - [SDR SWIA2023010567075](https://openairdocs.org/sdr/SWIA2023010567075.md): Frame · dented · Dec 12, 2022 · N128SY · Emb ERJ170200LR · Fuselage Main, Frame > ADM N128SY-6792 DAMAGE LOCATED APPROX ON FR10, 1.9" ABOVE STRL 17L AND 3.8" FWD OF PREVIOUS REPAIR DOUBLER, DENT MEASURES 4.4" LONG BY 2.2" WIDE BY.060" DEEP. REINSPECT EVERY 750 FC FROM 7808 UNTIL OR BEFORE PERMANENT REPAIR DUE BY FC 15308 IAWETD 2019-170- - [SDR SWIA2020011447667](https://openairdocs.org/sdr/SWIA2020011447667.md): Crossbeam · corroded · Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION AFT WET AREA ON THE FR84 CROSSBEAM AS MARKED (C-CHECK) RO 1/11/2020 PERFORMED INNER DOUBLER REPAIR ON FR84 CROSSBEAM IAW SRM. - [SDR SWIA2020011447666](https://openairdocs.org/sdr/SWIA2020011447666.md): Floor Support · corroded · Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION AFT WET AREA ON THE R/H BEAM LOCATED BETWEEN FR89-90 CROSSBEAM Y= +10.748" (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED RH BEAM BETWEEN FR 89-90 CROSSBEAM. REF SRM. - [SDR SWIA2020011447665](https://openairdocs.org/sdr/SWIA2020011447665.md): Floorbeam · corroded · Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > CORROSION AFT WET AREA ON THE FLOOR SUPPORT R/H SIDE LOCATED ON THE FR87 CROSSBEAM (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED FLOOR SUPPORT ON THE RH SIDE LOCATED ON THE FR 97 CROSSBEAM. REF SRM. - [SDR SWIA2020011447664](https://openairdocs.org/sdr/SWIA2020011447664.md): Splice Plate · corroded · Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION AFT WET AREA ON THE L/H SIDE S SPLICE PLATE LOCATED BETWEEN FR87-88 CROSSBEAMS (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED LH SPLICE PLATE LOCATED BETWEEN FR87-88 PER SRM. - [SDR SWIA2020011447663](https://openairdocs.org/sdr/SWIA2020011447663.md): Floorbeam · corroded · Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > FLOOR BEAM AT + Y= 273.0 CORRODED AT FR 16. (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED CORRODED FLOOR BEAM AT + Y= 273.0 AT FR 12-20 REF SRM. SEE CONTINUATION CARD FOR DETATAILS. - [SDR SWIA2020011447668](https://openairdocs.org/sdr/SWIA2020011447668.md): Frame · chafed · Dec 22, 2019 · N128SY · Emb ERJ170200LR · Nacelle/Pylon, Main Frame > R/H AFT PYLON FAIRING FRAME 1 INBD PIP PIN ATTACH POINT HAT BUSHING MIGRATED OUT. (C-CHECK) RO 1/11/2020 REMOVED AND REPLACED R/H AFT PYLON FAIRING FRAME 1 REF EMB SRM. - [SDR SWIA2020011447662](https://openairdocs.org/sdr/SWIA2020011447662.md): Service Door · corroded · Dec 21, 2019 · N128SY · Emb ERJ170200LR · Fluid Service Doors > CORROSION ON INTERNAL SURFACE OF LAV. SERVICE DOOR. (C-CHECK) RO 1/11/2020 REMOVED CORROSION ON INTERNAL SURFACE OF LAV. SERVICE DOOR. DOOR NOMINAL: 0.050". MAX. MATERIAL REMOVED: 0.005". NON SIG ALLOWABLE: 0.001". REMAINING MATERIAL: 0.045". LAV. SERVICE DOO - [SDR SWIA201541434](https://openairdocs.org/sdr/SWIA201541434.md): Skin · dented · Sep 14, 2015 · N128SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > SKIN HAS A DENT JUST AFT OF THE CAPT'S SIDE WINDOW. REPAIRED IAW SRM. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N128SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N128SY/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.