# Service difficulty reports: N176SY

A list on [N176SY](https://openairdocs.org/aircraft/N176SY.md).

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

- [SDR SWIA20260107230](https://openairdocs.org/sdr/SWIA20260107230.md): Pump · failed · Dec 30, 2025 · N176SY · Emb ERJ170200LR · Fuel Boost Pump
  > FUEL 1 LO LEVEL WARNING MESSAGE DURING FLIGHT. QRH COMPLIED WITH AND DIVERSION REQUIRED. (FLIGHT 3102) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31453918. TROUBLESHOOT FUEL 1 LO LEVEL WARNING MESSAGE IN REFERENCE TO ERJ175 FIM 28-44-00. PERFORMED OPS TE
- [SDR SWI2026F00000](https://openairdocs.org/sdr/SWI2026F00000.md): Warning Message · illuminated · Dec 30, 2025 · N176SY · Emb ERJ170200LR · Fuel Indicating System
  > FUEL 1 LO LEVEL WARNING MESSAGE DURING FLIGHT. QRH COMPLIED WITH AND DIVERSION REQUIRED. (FLIGHT 3102) OPEN.
- [SDR SWIA2025122400010](https://openairdocs.org/sdr/SWIA2025122400010.md): Shim · worn · Dec 10, 2025 · N176SY · Emb ERJ170200LR · Passenger/Crew Doors
  > FWD PASSENGER DOOR FWD SERRATED SLIDE SHIM IS WORN. REMOVED AND REPLACED FWD PASSENGER DOOR FWD SERRATED SLIDE SHIM. REF EMB 175 AMM 53-10-21.
- [SDR SWI2025F01868](https://openairdocs.org/sdr/SWI2025F01868.md): Flap Track · worn · Dec 4, 2025 · N176SY · Emb ERJ170200LR · Trailing Edge Flaps
  > RIGHT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF.87MM MAX ALONG FWD SIDE. REMOVED AND REPLACED RT WING FLAP TRACK 1A IAW AMM 57-54-25.
- [SDR SWIA2025122300004](https://openairdocs.org/sdr/SWIA2025122300004.md): Flap Track · worn · Dec 4, 2025 · N176SY · Emb ERJ170200LR · Trailing Edge Flaps
  > LEFT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF.25MM MAX ALONG FWD SIDE. REMOVED AND REPLACED LH WING FLAP TRACK 1A REF AMM 57-54-25.
- [SDR SWIA20230619002](https://openairdocs.org/sdr/SWIA20230619002.md): Unknown · warning message · Jun 17, 2023 · N176SY · Emb ERJ170200LR · Landing Gear Door Actuator
  > ON TAKE OFF I CALLED FOR GEAR UP-WE RECEIVED A CAUTION MESSAGE. MESSAGE WAS ONLY VISIBLE FOR A FEW SECONDS THEN IT CLEARED. THE GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND PUSHED THE DN LOCK REL BUTTON-GEAR RETRACTED WITH NO ISSUES. IT OCCURRED DURING A CR
- [SDR SWIA20230217](https://openairdocs.org/sdr/SWIA20230217.md): None · corroded · Feb 17, 2023 · N176SY · Emb ERJ170200LR · Fuselage Main, Frame
  > FWD FUSELAGE HAS LIGHTNING STRIKE ABOVE STGR 19R AFT OF FR 04 AS MARKED (C-CHECK RO 3/6/2023) REPAIRED DAMAGE AT STGR 19R AFT OF FR 04, BY DRILLING HOLE AND INSTALLING REPAIR FASTENER AND WASHER. REF EMB ETD2023-170-004756 REV.A NO WEIGHT INCREASE DUE T
- [SDR SWIA20230216](https://openairdocs.org/sdr/SWIA20230216.md): None · corroded · Feb 16, 2023 · N176SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > CORROSION/GOUGING FOUND AT RH IB SEAT TRACK FROM FR 75 TO 85 ALONG ENTIRE LENGTH. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED RH IB SEAT TRACK FR 75-85 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 PO# 291216 AND APPLIED CIC REF CPM 51-2
- [SDR SWIA20230215](https://openairdocs.org/sdr/SWIA20230215.md): None · gouged · Feb 15, 2023 · N176SY · Emb ERJ170200LR · Fuselage Structure (General)
  > FORWARD FUSELAGE R/H INBOARD SEAT TRACK HAS GOUGE BETWEEN FRAMES 21-22. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED FORWARD FUSELAGE R/H INBOARD SEAT TRACK BETWEEN FRAMES 20-23. REF: SRM 51-40-08. SEAT TRACK REPLACED WITH FACTORY PART, NO CHANGE TO WEIGH
- [SDR SWIA2023020014](https://openairdocs.org/sdr/SWIA2023020014.md): None · cracked · Feb 14, 2023 · N176SY · Emb ERJ170200LR · Fuselage Floor Panel
  > CRACKED FR 12 COCKPIT FLOOR STRUCTURE CENTER CONNECTOR SUPPORT ANGLE. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED CENTER CONNECTOR SUPPORT ANGLE AT FR 12 COCKPIT FLOOR. REF SRM 51-40-08 PO#279119 PO#291158
- [SDR SWIA2023020013](https://openairdocs.org/sdr/SWIA2023020013.md): None · gouged · Feb 13, 2023 · N176SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > RH LATERAL SEAT TRACK HAS GOUGES AS MARKED FR59-73. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED RH LATERAL SEAT TRACK LOCATED AT FR59-73 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. SEAT TRACK REPLACED WITH FACTORY PART, NO CHANGE TO W
- [SDR SWIA20230213](https://openairdocs.org/sdr/SWIA20230213.md): None · corroded · Feb 13, 2023 · N176SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > CORROSION AS MARKED ON 7 AREAS AS MARKED ON THE RH FLOOR BEAM SEAT TRACK FRAMES 23 THROUGH 34. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED RH FLOOR BEAM SEAT TRACK FRAMES 23 THROUGH 34. REF: SRM 51-40-08. SEAT TRACK REPLACED WITH FACTORY PART, NO CHANGE
- [SDR SWIA202265568](https://openairdocs.org/sdr/SWIA202265568.md): None · cracked · Apr 25, 2022 · N176SY · Emb ERJ170200LR · Fuselage Main, Frame
  > LH GEAR BAY SHOWS SIGNS OF A FRAME 52 CRACK. (FILED CLOSED) REPAIRED THE CRACK ON FRAME 52 IN THE LH WHEEL WELL AREA IN REFERENCE TO SRM 53-22-04/REPAIR 04P
- [SDR SWIA202052900](https://openairdocs.org/sdr/SWIA202052900.md): Threshold · corroded · Sep 19, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > L2 DOOR LOWER THRESHOLD BEAM HAS CORROSION ON EDGES OF FWD AND AFT GIRT BAR FITTING RECESSES. C-CHECK RO 9/29/2020. BLENDED AND REPAIRED L2 DOOR LOWER THRESHOLD BEAM FWD AND AFT GIRT BAR FITTING RECESSES (HOUSING CORNERS), IAW EMB SRM. APPLIED ALODINE, REF
- [SDR SWIA202052899](https://openairdocs.org/sdr/SWIA202052899.md): Threshold · corroded · Sep 19, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > R2 DOOR LOWER THRESHOLD BEAM HAS CORROSION ON EDGES OF FWD AND AFT GIRT BAR FITTING RECESSES. C-CHECK RO 9/29/2020. BLENDED AND REPAIRED R2 DOOR LOWER THRESHOLD BEAM FWD AND AFT GIRT BAR FITTING RECESSES (HOUSING CORNERS), IAW EMB SRM. APPLIED ALODINE, REF
- [SDR SWIA202052897](https://openairdocs.org/sdr/SWIA202052897.md): Stop Fitting · worn · Sep 16, 2020 · N176SY · Emb ERJ170200LR · Fuselage Main, Structure
  > L2 DOOR, TOP FORWARD AND AFT LOWER DOOR STOPS ON FRAME WORN. C-CHECK RO 9/29/2020. REMOVED AND REPLACED L2 DOOR, TOP FORWARD AND AFT LOWER DOOR STOPS ON FRAME, REF AMM.
- [SDR SWIA202052891](https://openairdocs.org/sdr/SWIA202052891.md): Intercostal · corroded · Sep 16, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT FR 88-FR 89 INTERCOSTAL HAS CORROSION, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED RT INTERCOSTAL BEAM AT FR 88-89 WITH NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF EMB 175 SRM.
- [SDR SWIA202052890](https://openairdocs.org/sdr/SWIA202052890.md): Firewall · cracked · Sep 16, 2020 · N176SY · Emb ERJ170200LR · APU Cowling/Containment
  > APU FIREWALL PANEL 351BZ CRACKED, AS MARKED. C-CHECK RO 9/29/2020. PERFORMED PERMANENT REPAIR OF CRACK ON PANEL 351BZ BY TRIMMING OUT THE CRACKED SPT WELDS AND INSTALLING A DOUBLER, REF SRM REPAIR02P REF TABLE 206 FOR REURRENT EXT DET AT 10,000 FC.
- [SDR SWIA202052896](https://openairdocs.org/sdr/SWIA202052896.md): Floor Support · corroded · Sep 15, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION FORWARD WET AREA ON FLOOR SUPPORT ON RIGHT SIDE OF FRAME 16 FLOOR BEAM, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED NEW FLOOR SUPPORT BRACKET ON FR 16 RT, REF SRM.
- [SDR SWIA202052895](https://openairdocs.org/sdr/SWIA202052895.md): Floor Support · corroded · Sep 15, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION FORWARD WET AREA ON RIGHT FORWARD SILL IN 3 LOCATIONS BETWEEN FRAMES 13 AND 14, AS MARKED. C-CHECK RO 9/29/2020. FOUND RT SILL FR 13-14 TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FORWARD SILL AND APPLIED FINISH, REF EMB SRM. SEE CONTINUATION CA
- [SDR SWIA202052894](https://openairdocs.org/sdr/SWIA202052894.md): Bracket · cracked · Sep 15, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR SUPPORT BRACKET CRACKED AT FRAME 12 ON PILOTS SIDE, AS MARKED. C-CHECK RO 9/29/2020. LOCATED, DRILLED AND INSTALLLED COCKPIT FLOOR SUPPORT BRACKET AT FRAME 12 ON PILOTS SIDE, REF EMB 175 SRM.
- [SDR SWIA202052893](https://openairdocs.org/sdr/SWIA202052893.md): Shear Tie · cracked · Sep 15, 2020 · N176SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED SHEAR CLIP, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED SUPPORT ANGLE BETWEEN FR 11 AND 12, REF SRM.
- [SDR SWIA202052892](https://openairdocs.org/sdr/SWIA202052892.md): Skin · chafed · Sep 14, 2020 · N176SY · Emb ERJ170200LR · Electrical/Electronic Compartment Doors
  > MID AVIONICS BAY ACCESS DOOR CUTOUT EXTERNAL SKIN HAS 1 CHAFED RIVET HEADS, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED FASTENER (1) AT MID AVIONICS BAY ACCESS DOOR CUTOUT, EXTERNAL SKIN, REF SRM.
- [SDR SWIA2019120246805](https://openairdocs.org/sdr/SWIA2019120246805.md): Unknown · odor · Dec 2, 2019 · N176SY · Emb ERJ170200LR · Air Distribution System
  > STRONG SMELL OF BURNING OIL AFTER TAKEOFF THROUGH 15,000 FEET. FLIGHT 3329 CLOSED COMPLIED WITH APPLICABLE STEPS IN REFERENCE WITH GE LMM, FAULT ISOLATION 003, NO DEFECTS NOTED. PERFORMED ENGINES RUN IN REFERENCE WITH AMM, NO BURNING OIL SMELL IN COCKPIT AN

## 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 = 'N176SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N176SY/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.