# Service difficulty reports: N184SY A list on [N184SY](https://openairdocs.org/aircraft/N184SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2026071976827](https://openairdocs.org/sdr/SWIA2026071976827.md): Shear Tie · corroded · Jul 19, 2026 · N184SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT FR 85 BETWEEN STRINGERS 27 - 28R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-08. - [SDR SWIA2026071776832](https://openairdocs.org/sdr/SWIA2026071776832.md): Shear Tie · corroded · Jul 17, 2026 · N184SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT FR 88 BETWEEN STRINGERS 27- 28R. REMOVED AND REPLACED THE SHEAR TIE FR 88 STGRS 27-28R, REF SRM 51-40-08. - [SDR SWIA2026071776825](https://openairdocs.org/sdr/SWIA2026071776825.md): Shear Tie · corroded · Jul 17, 2026 · N184SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION ON SHEAR TIE AT FR 87 BETWEEN STRINGERS 27 - 28R. R & R THE SHEAR TIE IAW SRM 51-40-08. - [SDR SWIA2026071676830](https://openairdocs.org/sdr/SWIA2026071676830.md): Beam · corroded · Jul 16, 2026 · N184SY · Emb ERJ170200LR · Fuselage Main, Structure > AFT WET AREA CORRODED FASTENERS ON RT BEAM AT FR 86. REMOVED AND REPLACED AFT WET AREA RT BEAM FR 86-89, IAW SRM 51-40-08. NEW BEAM REPLACED WITH OEM PART. - [SDR SWIA2026071676828](https://openairdocs.org/sdr/SWIA2026071676828.md): Beam · corroded · Jul 16, 2026 · N184SY · Emb ERJ170200LR · Fuselage Main, Structure > AFT WET AREA LEFT BEAM HAD CORRODED FASTENERS BETWEEN FR 86-87. REMOVED AND REPLACED AFT WET AREA LT BEAM IAW SRM 51-40-08. - [SDR SWIA2026070976831](https://openairdocs.org/sdr/SWIA2026070976831.md): Antenna · out of limits · Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/Structures > COMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR BY INSTALLING A DOUBLER AND FILLER REPAIR AT FR 82-83, STR 27-28L IAW DWG 170-2365-02-RS, AND M-9 - [SDR SWIA2026070976829](https://openairdocs.org/sdr/SWIA2026070976829.md): Antenna · out of limits · Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/Structures > COMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR.IAW DRAWING 170-2365-02-315 APPENDIX B. - [SDR SWIA2026070976826](https://openairdocs.org/sdr/SWIA2026070976826.md): Antenna · out of limits · Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/Structures > COMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44) (C-CHECK RO 08/10/2026)COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR. REF DRAWING 170-2365-02-314 APPENDIX A. - [SDR SWIA2026070976824](https://openairdocs.org/sdr/SWIA2026070976824.md): Antenna · out of limits · Jul 9, 2026 · N184SY · Emb ERJ170200LR · Standard Practices/Structures > COMPLY WITH LT SIDE ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). COMPLIED WITH LT SIDE ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS, AND M-93 ERJ175-53-26-03 (EA ERJ4111A-44). - [SDR SWIA202410210014](https://openairdocs.org/sdr/SWIA202410210014.md): Door · warning message · Oct 14, 2024 · N184SY · Emb ERJ170200LR · Door Warning System > DOOR PAX AFT OPEN WARNING MESSAGE APPEARED FOR APPROXIMATELY 10 SECONDS DURING CLIMB OUT THEN EXTINGUISHED. RAN QRH. PRESSURIZATION WAS NORMAL AND THE FLIGHT ATTENDANT VERIFIED THAT 3 LATCH INDICATORS WERE INDICATING GREEN. MEL 52-70-0CAT: 'C' DUE 10/24/24DOO - [SDR SWIA20241015014](https://openairdocs.org/sdr/SWIA20241015014.md): Warning Message · false activation · Oct 14, 2024 · N184SY · Emb ERJ170200LR · Door Warning System > D: DOOR PAX AFT OPEN WARNING MESSAGE APPEARED FOR APPROXIMATELY 10 SECONDS DURING CLIMB OUT THEN EXTINGUISHED. RAN QRH. PRESSURIZATION WAS NORMAL AND THE FLIGHT ATTENDANT VERIFIED THAT 3 LATCH INDICATORS WERE INDICATING GREENC: MEL 52-70-0CAT: 'C' DUE 10/24/2 - [SDR SWIA20230911819](https://openairdocs.org/sdr/SWIA20230911819.md): Unknown · gouged · Aug 19, 2023 · N184SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN CFI RIGHT FLOOR SEAT TRACK HAS GOUGE MARKS AT FR 23, AFT OF 23, 24, 25, AFT OF 26, AFT OF 27, AFT OF 30, AFT OF 32, AND AFT OF 33. (C-CHECK RO 9/8/2023) REMOVED AND REPLACED RH SEAT TRACK AT FR 23-34. REF EMB SRM 51-40-08. THIS DOES NOT EFFEC - [SDR SWIA2021072759752](https://openairdocs.org/sdr/SWIA2021072759752.md): Support Bracket · cracked · Jul 15, 2021 · N184SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > LH AND RH PANEL SUPPORT BRACKETS CRACKED ON FLOOR BEAM AT FRAME 85. (C-CHECK RO 7/23/2021) REMOVED AND REPLACED LH AND RH PANEL SUPPORT BRACKETS ON FLOOR BEAM AT FRAME 85 REF SRM 51-40-08. USED 7475T61.050 PO# 263514 FOR FABRICATION OF LH AND RH PANEL - [SDR SWIA2021072759751](https://openairdocs.org/sdr/SWIA2021072759751.md): Angle · cracked · Jul 11, 2021 · N184SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > LH LOWER FUSELAGE FRAME 52 L-ANGLE HAS A CRACK EMANATING FROM THE OUTBOARD MOST RIVET. (C-CHECK RO 7/23/2021) REMOVED AND REPLACED L/H LOWER FUSELAGE FR 52 "L" ANGLE REF SRM 51-40-08. - [SDR SWIA2021072759750](https://openairdocs.org/sdr/SWIA2021072759750.md): Doubler · corroded · Jul 11, 2021 · N184SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > CORROSION FORWARD WET AREA - AFT OF FRAME 19 ONE AREA OF CORROSION ON DOUBLER ON LH SIDE. (C-CHECK RO 7/23/2021) REMOVED AND REPLACED DOUBLER AT FRAME 19 LH SIDE REF EMB SRM 51-40-08 AND 51-40-02 - [SDR SWIA2021072759749](https://openairdocs.org/sdr/SWIA2021072759749.md): Crossbeam · corroded · Jul 10, 2021 · N184SY · Emb ERJ170200LR · Fuselage Main, Structure > RH CROSSBEAM CORRODED AT FRAME 84. (C-CHECK RO 7/23/2021) BLENDED AND EVALUATED R/H CROSSBEAM AT FRAME 84 REF SRM 51-10-03. 1 MATERIAL REMOVED 0.032" L-2.792", W-0.927". AREAL 2. MATERIAL REMOVED 0.016" L-1.170", W-0.819". AREA 3 MATERIAL REMOVED 0.024" - [SDR SWIA2020041350118](https://openairdocs.org/sdr/SWIA2020041350118.md): Trim Switch · failed · Apr 13, 2020 · N184SY · Emb ERJ170200LR · Stabilizer Actuator > UPON TAKEOFF, PLANE CONTINUED TO PITCH UP. WHILE AP ON PLANE CONTINUED TO PITCH HIGH WITH AIRSPEED FROZEN TO LOWER NUMBERS. MANUAL SPEED TO RETRACT FLAPS- PLANE CONTINUED TO PITCH HIGH- FOLLOWED MEMORY ITEMS FOR SUSPECTED PITCH TRIM. DISCONNECTED ALL AND HAND ## 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 = 'N184SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N184SY/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.