# Service difficulty reports: N151SY A list on [N151SY](https://openairdocs.org/aircraft/N151SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2026083177282](https://openairdocs.org/sdr/SWIA2026083177282.md): Seat Track · corroded · Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > FWD WET AREA CENTER SEAT TRACK HAS CORROSION ON CROWN AT FR 20-21 AND Y-10. REPAIRED TRIMMED OUT FWD WET AREA CENTER SEAT TRACK CROWN TEETH AT FR 20-21 AND Y-10 PER SRM 53-00-10REPAIR 02P AND ETD2026-170-015024 REV A. - [SDR SWIA2026083177281](https://openairdocs.org/sdr/SWIA2026083177281.md): Floorbeam · corroded · Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > FWD WET AREA HAS CORROSION ON LONGITUDINAL FLOORBEAM AT FR 17, Y-10. REMOVED AND REPLACED THE FLOORBEAM AT FR 17 AND Y-10 IAW SRM 51-40-08. - [SDR SWIA2026083177280](https://openairdocs.org/sdr/SWIA2026083177280.md): Beam · corroded · Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > AFT WET AREA LH UPPER BEAM HAD CORROSION BTWN FR 87-88, Y-10 - Y-12. REMOVED AND REPLACED AFT WET AREA LH UPPER BEAM IAW SRM 51-40-08. - [SDR SWIA2026083177279](https://openairdocs.org/sdr/SWIA2026083177279.md): Floorbeam · corroded · Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > FWD WET AREA FLOORBEAM WAS CORRODED, FR 17, Y-10. REPAIRED FLOORBEAM IAW SRM 53-00-10,REPAIR 3P. NO FURTHER ACTION REQUIRED - [SDR SWIA2026083177278](https://openairdocs.org/sdr/SWIA2026083177278.md): Seat Track · corroded · Aug 31, 2026 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > FWD WET AREA RT SEAT TRACK WAS CORRODED ON THE CROWN, BTWN FR 18-19, Y105. R & R THE SEAT TRACK IAW SRM 51-40-08. - [SDR SWIA202311280016](https://openairdocs.org/sdr/SWIA202311280016.md): Unknown · warning message · Nov 26, 2023 · N151SY · Emb ERJ170200LR · Fire Protection System > ENG 2 FIRE DET FAIL CAUTION MSG WHILE CLIMBING OUT OF BNA ABOVE 13,000. MSG GOT CLEARED ON ITS OWN; FOLLOWED QRH - NO INDICATION OF FIRE FOUND ON ENG 2 (FLIGHT 5738 FILED CLOSED)**** REPEATER **** REMOVED AND REPLACED GENERIC I/O MODULE (MAU 1 SLOT 11,12) IN R - [SDR SWI2023F00525](https://openairdocs.org/sdr/SWI2023F00525.md): Unknown · warning message · Nov 26, 2023 · N151SY · Emb ERJ170200LR · Detection System > ENG 2 FIRE DET FAIL CAUTION MSG WHILE CLIMBING OUT OF BNA ABOVE 13,000. MSG GOT CLEARED ON ITS OWN; FOLLOWED QRH - NO INDICATION OF FIRE FOUND ON ENG 2 (FLIGHT 5738 FILED OPEN)**** REPEATER **** - [SDR SWIA20230714622](https://openairdocs.org/sdr/SWIA20230714622.md): Unknown · corroded · Jun 22, 2023 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > LH FLOOR SEAT TRACK FLANGE HAS CORROSION AT FR 19-20 AT BASE OF CROWN TEETH TRANSITION. (C-CHECK RO 7/13/2023) L/H INBD SEAT TRACK WAS REMOVED AND REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED. REF EMB SRM 51-40-08 - [SDR SWI202307140134](https://openairdocs.org/sdr/SWI202307140134.md): Unknown · gouged · Jun 21, 2023 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > LH O/B SEAT TRACK FR74/84 GOUGED IN THREE LOCATIONS AS MARKED (C-CHECK RO 7/13/2023) REMOVED AND REPLACED LH O/B SEAT TRACK FR74/84 REF SRM 51-40-08. LH O/B SEAT TRACK FR74/84 WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED - [SDR SWIA20230714621](https://openairdocs.org/sdr/SWIA20230714621.md): Unknown · corroded · Jun 21, 2023 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CORROSION - RH I/B SEAT TRACK BETWEEN FR83/84 (C-CHECK RO 7/13/2023) REMOVED CORROSION FROM RH IB SEAT TRACK BY CUTTING OUT DAMAGE AND SPLICING IN ANEW SECTION OF SEAT TRACK REF ETD2022-170-022163. WEIGHT OF REPAIR PARTS IS 4 OZ ASSET NUMBER TC2-02 CAL - [SDR SWIA202052788](https://openairdocs.org/sdr/SWIA202052788.md): Support Rod · cracked · Sep 13, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Structure > FUELING PANEL SUPPORT ROD IS CRACKED AND GOUGED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED FUEL PANEL SUPPORT ROD, REF E175 AMM. - [SDR SWIA202052787](https://openairdocs.org/sdr/SWIA202052787.md): Rib · cracked · Sep 13, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Structure > PANEL 345 AR INNER RIB CRACKED, AS MARKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED CRACKED RIB ON PANEL 345AR, REF EMB SRM. - [SDR SWIA202052786](https://openairdocs.org/sdr/SWIA202052786.md): Guide · cracked · Sep 12, 2020 · N151SY · Emb ERJ170200LR · Trailing Edge Flaps > RT WING NR 2 MAIN FLAP CARRIAGE INBOARD AFT TRACK GUIDE CRACKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED RT NR 2 MAIN FLAP CARRIAGE INBOARD AFT TRACK GUIDE, REF E-175 AMM. RIGGING AND OPERATIONAL TEST CHECKS GOOD. - [SDR SWIA202052785](https://openairdocs.org/sdr/SWIA202052785.md): Guide · cracked · Sep 12, 2020 · N151SY · Emb ERJ170200LR · Trailing Edge Flaps > LT WING NR 4 AFT FLAP CARRIAGE INBOARD FWD TRACK GUIDE CRACKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED LT NR 4 AFT FLAP CARRIAGE INBOARD FWD TRACK GUIDE, REF E-175 AMM. - [SDR SWIA202052784](https://openairdocs.org/sdr/SWIA202052784.md): Rod · chafed · Sep 11, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Structure > CHAFE LOWER ROD ASSEMBLY AS MARKED ON CO-PILOTS DV WINDOW. C-CHECK RO 9/24/2020. BLENDED CHAFFED AREA ON LOWER ROD ASSEMBLY, IAW EMB-175 AMM. ROD DIAMETER BEFORE BLEND WAS: 18.05MM. ROD DIAMETER AFTER BLEND: 17.82MM. AMM MIN ALLOWABLE DIAMETER 17.69MM. - [SDR SWIA202052783](https://openairdocs.org/sdr/SWIA202052783.md): Rod · chafed · Sep 11, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Structure > CHAFE LOWER ROD ASSEMBLY AS MARKED ON PILOTS DV WINDOW. C-CHECK RO 9/24/2020. BLENDED CHAFED AREA ON LOWER ROD ASSEMBLY, IAW EMB-175 AMM. ROD DIAMETER BEFORE BLENDING WAS 18.03MM AND ROD DIAMETER AFTER BLENDING: 17:86MM. AMM MINIMUM ALLOWED DIAMETER 17.69M - [SDR SWIA202052782](https://openairdocs.org/sdr/SWIA202052782.md): Angle · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORRODED 3 EA LOWER ANGLES AND 1 EA CRACK RECEPTACLE ON PANEL 1441FR. C-CHECK RO 9/24/2020. REMOVED AND REPLACED 2 EA LOWER ANGLES. PERFORMED BLENDOUT ON (1) ANGLE, FOUND TO BE WITHIN LIMITS. REPLACED DAMAGED RECEPTABLE ON PANEL 1441FR, REF EMB SRM. RESTO - [SDR SWIA202052781](https://openairdocs.org/sdr/SWIA202052781.md): Splice · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Floor Panel > CORROSION ON SPLICE PLATE INSTALLED AT FWD FLANGE OF PANEL 192DL. C-CHECK RO 9/24/2020. REMOVED SPLICE PLATE FWD FLANGE OF PANEL 192 DL AND INSTALLED NEW SPLICE PLATE, REF EMB SRM AMM. - [SDR SWIA202052780](https://openairdocs.org/sdr/SWIA202052780.md): Seat Track · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CORROSION, AFT WET AREA RT FLOOR SEAT TRACK END CORRODED, AS MARKED FR 84-85. C-CHECK RO 9/24/2020. PERFORMED SEAT TRACK SPLICE REPAIR AT AFT WET AREA RT FLOOR SEAT TRACK FR 84-85, PER SRM. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. - [SDR SWIA202052779](https://openairdocs.org/sdr/SWIA202052779.md): Seat Track · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CORROSION, AFT WET AREA LT FLOOR SEAT TRACK END CORRODED, AS MARKED FR 84-85. C-CHECK RO 9/24/2020. REMOVED COROSION, REF EMB SRM. PERFROMED PERNANENT REPAIR STEPS, IAW ETD. - [SDR SWIA202052778](https://openairdocs.org/sdr/SWIA202052778.md): Floorbeam · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > CORROSION, AFT WET AREA LT FLOOR BEAM HAS CORROSION, AS MARKED AT FR 87. C-CHECK RO 9/24/2020. REMOVED DAMAGED AFT WET AREA LT FLOOR BEAM. LOCATED, DRILLED, AND INSTALLED NEW AFT WET AREA LT FLOOR BEAM, REF EMB SRM 51-40-08. APPLIED FINISH, REF EMB SRM & C - [SDR SWIA202052777](https://openairdocs.org/sdr/SWIA202052777.md): Floor Support · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION, AFT WET AREA RT FLOOR BEAM UPPER SHEET HAS CORROSION AS MARKED FR 85-86. C-CHECK RO 9/24/2020. REMOVED AND REPLACED AFT WET AREA RT FLOOR BEAM UPPER SHEET FR 85-86, REF EMB SRM. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202052776](https://openairdocs.org/sdr/SWIA202052776.md): Floorbeam · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > CORROSION, AFT WET AREA RT FLOOR BEAM CORRODED AROUND FASTENER, AS MARKED AT FR 87. C-CHECK RO 9/24/2020. REMOVED AND REPLACED AFT WET AREA RT FLOOR BEAM FR 86-89 WITH NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE. APPLIED FINISH, REF - [SDR SWIA202052775](https://openairdocs.org/sdr/SWIA202052775.md): Floor Support · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION, AFT WET AREA FR 87 PANEL SUPPORT FWD OF RT SHEAR PANEL CORRODED, AS MARKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED AFT WET AREA FR 87 PANEL SUPPORT FORWARD OF RT SHEAR PANEL, REF EMB SRM. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202052774](https://openairdocs.org/sdr/SWIA202052774.md): Floor Support · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION, AFT WET AREA RT PANEL SUPPORT HAS CORROSION AT FR 90, AS MARKED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED RT PANEL SUPPORT AT FRAME 90, REF SRM. - [SDR SWIA202052773](https://openairdocs.org/sdr/SWIA202052773.md): Floor Support · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION, AFT WET AREA RT PANEL SUPPORT HAS CORROSION AT FR 90, AS MARKED. C-CHECK RO 9/24/2020. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE BEYOND ANY SRM LIMITS. REMOVAL AND REPLACEMENT OF AFT WET AREA RH PANEL SUPPORT AT FR90, REF EMB175 SRM. - [SDR SWIA202052772](https://openairdocs.org/sdr/SWIA202052772.md): Crossbeam · broken · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Structure > FRAME 86 CROSSBEAM LT AND RT PANEL SUPPORTS BROKEN OFF. C-CHECK RO 9/24/2020. REMOVED AND REPLACED FR 86 CROSSBEAM LT AND RT PANEL SUPPORTS, PER SRM. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202052771](https://openairdocs.org/sdr/SWIA202052771.md): Structure · chafed · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Engine (Turbine/Turboprop) > RT ENGINE, INBOARD AND OUTBOARD CHEVRON TURKEY FEATHERS ARE CHAFED. C-CHECK RO 9/24/2020. REMOVED AND REPLACED RT ENGINE, INBOARD AND OUTBOARD CHEVRON TURKEY FEATHERS. SEE CONTINUATION CARD FOR STEPS PERFORMED, REF SRM. - [SDR SWIA202052770](https://openairdocs.org/sdr/SWIA202052770.md): Seat Track · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > CORROSION FWD WET AREA LT FLOOR TRACK CORRODED AS MARKED AT FR 17. C-CHECK RO 9/24/2020. PERFORMED CUTOUT OF CORROSION ON FRAME 17 LT FLOOR TRACK. FABRICATED AND INSTALLED FILLER AND DOUBLER, REF EMB SRM. ADDED WEIGHT DOES NOT CHANGE WEIGHT AND BALANCE. - [SDR SWIA202052769](https://openairdocs.org/sdr/SWIA202052769.md): Crossbeam · corroded · Sep 10, 2020 · N151SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION FWD WET AREA FR 17 CROSSBEAM AS MARKED IN BETWEEN LT AND RT FLOOR TRACKS. C-CHECK RO 9/24/2020. PERFORMED CUTOUT OF CORROSION ON FRAME 17 CROSSBEAM. FABRICATED AND INSTALLED FILLER AND DOUBLER, REF EMB SRM. ADDED WEIGHT DOES NOT CHANGE WEIGHT AND - [SDR SWIA2019120946835](https://openairdocs.org/sdr/SWIA2019120946835.md): Brake · failed · Dec 9, 2019 · N151SY · Emb ERJ170200LR · Landing Gear Brake System > WHILE IN FLIGHT WE HAD INTERMITTENT BRK LH/RH FAIL MESSAGES. WE COORDINATED WITH DISPATCH, DECLARED AN EMERGENCY AND LANDED AFTER ALL APPLICABLE CHECKLIST AND BRIEFINGS WERE COMPLETE. LANDING UNEVENTFUL, HOWEVER UPON LANDING BRK LH RH FAIL MESSAGES REMAINED. D ## 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 = 'N151SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N151SY/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.