# Service difficulty reports: N175SY A list on [N175SY](https://openairdocs.org/aircraft/N175SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWI2025F01515](https://openairdocs.org/sdr/SWI2025F01515.md): Beam · corroded · Oct 13, 2025 · N175SY · Emb ERJ170200LR · Fuselage Main, Structure > AFT WET AREA FLOOR STRUCTURE LT INBOARD BEAM AT FR 87 HAS CORROSION. REMOVED AND REPLACED LT INBOARD BEAM AT FR 87. IAW SRM 51-40-08. - [SDR SWIA20251107003](https://openairdocs.org/sdr/SWIA20251107003.md): Seat Track · gouged · Oct 13, 2025 · N175SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > RT INBOARD SEAT TRACK FR 74-84 HAS GOUGES IN 11 LOCATIONS. REMOVED AND REPLACED RT INBD SEAT TRACK IAW SRM 51-40-08. - [SDR SWI2025F01516](https://openairdocs.org/sdr/SWI2025F01516.md): Slide · unpacked · Oct 11, 2025 · N175SY · Emb ERJ170200LR · Escape Slide > DURING REMOVAL OF AFT SERVICE DOOR EVAC SLIDE, IT WAS FOUND THAT THE LOWER SAFETY PIN WOULD NOT LOCK INTO PLACE, AND SLIDE UNRAVELLED OFF OF BOARD DURING REMOVAL. REMOVED AND REPLACED AFT SERVICE DOOR EVAC SLIDE. REF EMB 175 AMM 25-65-01. - [SDR SWIA2025110701](https://openairdocs.org/sdr/SWIA2025110701.md): Rib · cracked · Oct 11, 2025 · N175SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib > SUSPECTED CRACK RT HORIZONTAL STAB RIB 12A UPPER FLANGE BETWEEN FRONT SPAR AND FIRST STRINGER AT AFT RIVET LOCATION. REMOVED AND REPLACED R/H HORIZONTAL STAB RIB 12A. REF SRM 51-40-08 AND ETD2025-170-930708. - [SDR SWIA202304240002](https://openairdocs.org/sdr/SWIA202304240002.md): Pressure Switch · warning message · Apr 22, 2023 · N175SY · Emb ERJ170200LR · Landing Gear Brake System > PARKING BRAKE NOT RELEASED CAUTION MESSAGE DURING CRUISE. RAN QRH MESSAGE PERSISTED INTERMITTENTLY. NO ISSUES UPON LANDING. (FLT 3486 FILED CLOSED)PERFORMED T/S TO PARKING BRAKE NOT RELEASED CAUTION MESSAGE PER ERJ175 FIM 32-41-00, FOUND PRK BRK PR SW 2 FAULT - [SDR SWIA20230129](https://openairdocs.org/sdr/SWIA20230129.md): Unknown · damaged · Jan 29, 2023 · N175SY · Emb ERJ170200LR · Empennage Structure > LH ELEVATOR HINGE FITTING #3- UPON REMOVAL OF BUSHINGS, FOUND INBD HINGE LUG INNER BORE DAMAGED. (C-CHECK RO 2/8/2023) REMOVED DAMAGE FROM LEFT HAND ELEVATOR HINGE FITTING #3 LUG AND INSTALLED FABRICATED BUSHING. REF EMB, SRM 51-29-00, 55-21-00REP01P. - [SDR SWIA20230126](https://openairdocs.org/sdr/SWIA20230126.md): Unknown · corroded · Jan 26, 2023 · N175SY · Emb ERJ170200LR · Fuselage Structure (General) > CORROSION ON LH FLOOR LH SEAT TRACK 20/23 ON FORWARD END. (C-CHECK RO 2/8/2023) REMOVED AND REPLACED LH SEAT TRACK FR12 - FR20 REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA20230121](https://openairdocs.org/sdr/SWIA20230121.md): Unknown · gouged · Jan 21, 2023 · N175SY · Emb ERJ170200LR · Fuselage Structure (General) > CF I RH INBD (FLOOR) SEAT TRACK HAS DAMAGE/GOUGE FR 28-29 (C-CHECK RO 2/8/2023) REMOVED AND REPLACED CF I RH INBD FLOOR SEAT TRACK BETWEEN FR23-43 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 PO# 291261 CPM 51-25-00-910-001-A PO# 29430 - [SDR SWIA2020091452490](https://openairdocs.org/sdr/SWIA2020091452490.md): Bracket · cracked · Sep 2, 2020 · N175SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings > CRACK IN LT ANGLE BRACKET AT FR52 AS MARKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED LT ANGLE BRACKET AT FR52, REF SRM. RESTORED SURFACE PROTECTION, REF SRM. - [SDR SWIA2020091452487](https://openairdocs.org/sdr/SWIA2020091452487.md): Beam · corroded · Aug 30, 2020 · N175SY · Emb ERJ170200LR · Fuselage Main, Structure > FWD PAX DOOR LOWER BEAM, AFT ESCAPE FITTING FWD SIDE OF MOUNT POCKET HAS CORROSION ON EDGE OF POCKET, MARKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED FWD PAX DOOR LOWER BEAM WITH A NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF E - [SDR SWIA2020091452493](https://openairdocs.org/sdr/SWIA2020091452493.md): Support · corroded · Aug 28, 2020 · N175SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > SURFACE CORROSION FOUND FORWARD RT SILL FRAME 12-14, RBL 36-49, AS MARKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED RT SILL FR 12-14 (FWD WET AREA), REF SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. - [SDR SWIA2020091452492](https://openairdocs.org/sdr/SWIA2020091452492.md): Support · corroded · Aug 28, 2020 · N175SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION IN RT OUTBOARD SILL FR 88-90. C-CHECK RO 9/12/2020. REMOVED AND REPLACED RT OUTBOARD SILL FR 88-90, REF EMB SRM. - [SDR SWIA2020091452491](https://openairdocs.org/sdr/SWIA2020091452491.md): Beam · corroded · Aug 28, 2020 · N175SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION IN RT BEAM BETWEEN FR 89-90. C-CHECK RO 9/12/2020. REMOVED AND REPLACED RT BEAM BETWEEN FR 89-90 REF SRM. - [SDR SWIA2020091452486](https://openairdocs.org/sdr/SWIA2020091452486.md): Beam · corroded · Aug 28, 2020 · N175SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION IN LT BEAM FR 86-89. C-CHECK RO 9/12/2020. REMOVED AND REPLACED LT BEAM WITH NEW PART FROM FACTORY AT FR 86-89. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF SRM. - [SDR SWIA2020091452494](https://openairdocs.org/sdr/SWIA2020091452494.md): Finger Doubler · chafed · Aug 27, 2020 · N175SY · Emb ERJ170200LR · Fuselage Main, Structure > FORWARD CARGO DOOR SURROUND LOWER HORIZONTAL BEAM FINGER PLATE IS CHAFED IN CENTER AREA. C-CHECK RO 9/12/2020. REMOVED AND REPLACED FWD CARGO DOOR SURROUND LOWER HORIZONTAL BEAM FINGER PLATE, REF EMB 175 AMM. - [SDR SWIA2020091452489](https://openairdocs.org/sdr/SWIA2020091452489.md): Angle · cracked · Aug 27, 2020 · N175SY · Emb ERJ170200LR · APU Cowling/Containment > PANEL 351BZ (APU BULKHEAD PANEL) ANGLE IS CRACKED AT THE BOTTOM. C-CHECK RO 9/12/2020. REMOVED DAMAGE FROM PANEL 351BZ. FABRICATED AND INSTALLED NEW FILLER AND DOUBLER, REF EMB SRM. - [SDR SWIA2020091452488](https://openairdocs.org/sdr/SWIA2020091452488.md): Spar · cracked · Aug 27, 2020 · N175SY · Emb ERJ170200LR · Wing Spar > LT WINGLET, FRONT SPAR CRACKED IN TWO LOCATIONS, AS MARKED. C-CHECK RO 9/12/2020. THIS DISCREPANCY WILL BE CORRECTED DURING ACCOMPLISHMENT OF SB-WINGS-WING TIP-SPAR 1 REPLACEMENT REV 01 PART(S) 1, 2, 3, 4 TASK CARD. SEE CAMP NR 21326596 FOR SB ACCOMPLISHMEN ## 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 = 'N175SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N175SY/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.