N128SY

Service difficulty reports · 16

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2024081208Skin · damagedCOMPLY 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: , POSAug 8, 2024 · N128SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2023010567081Hinge · wornLEFT 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.Dec 17, 2022 · N128SY · Emb ERJ170200LR · Elevator StructureSDR SWIA2023010567080Flap Track · out of limitsL/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.Dec 16, 2022 · N128SY · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2023010567079Flap Track · wornL/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.Dec 16, 2022 · N128SY · Emb ERJ170200LR · AileronsSDR SWIA2023010567078Flap Track · out of limitsR/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.Dec 16, 2022 · N128SY · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2023010567077Flap Track · gougedR/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.Dec 16, 2022 · N128SY · Emb ERJ170200LR · Trailing Edge FlapsSDR SWIA2023010567076Seat Track · corrodedCABIN 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 EFFEDec 15, 2022 · N128SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2023010567075Frame · dentedADM 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-Dec 12, 2022 · N128SY · Emb ERJ170200LR · Fuselage Main, FrameSDR SWIA2020011447667Crossbeam · corrodedCORROSION AFT WET AREA ON THE FR84 CROSSBEAM AS MARKED (C-CHECK) RO 1/11/2020 PERFORMED INNER DOUBLER REPAIR ON FR84 CROSSBEAM IAW SRM.Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Main, StructureSDR SWIA2020011447666Floor Support · corrodedCORROSION 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.Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020011447665Floorbeam · corrodedCORROSION 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.Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2020011447664Splice Plate · corrodedCORROSION 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.Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020011447663Floorbeam · corrodedFLOOR 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.Dec 23, 2019 · N128SY · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR SWIA2020011447668Frame · chafedR/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.Dec 22, 2019 · N128SY · Emb ERJ170200LR · Nacelle/Pylon, Main FrameSDR SWIA2020011447662Service Door · corrodedCORROSION 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 DOODec 21, 2019 · N128SY · Emb ERJ170200LR · Fluid Service DoorsSDR SWIA201541434Skin · dentedSKIN HAS A DENT JUST AFT OF THE CAPT'S SIDE WINDOW. REPAIRED IAW SRM.Sep 14, 2015 · N128SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
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