# Service difficulty reports: N178SY

A list on [N178SY](https://openairdocs.org/aircraft/N178SY.md).

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

- [SDR SWIA2026010475093](https://openairdocs.org/sdr/SWIA2026010475093.md): Flap Track · worn · Jan 4, 2026 · N178SY · Emb ERJ170200LR · Trailing Edge Flaps
  > LEFT FLAP TRACK 1A HAS A THICKNESS REDUCTION OF.023 INCH. REMOVED AND REPLACED THE LT FLAP TRACK 1A IAW AMM 57-54-25.
- [SDR SWIA2026012175092](https://openairdocs.org/sdr/SWIA2026012175092.md): Seat Track · damaged · Dec 27, 2025 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CENTER FUSELAGE III RT INBD SEAT TRACK HAS SEVERAL DAMAGES FROM FR 74 TO FR 84. REMOVED AND REPLACED SEAT TRACK FR 74 TO FR 84 IAW SRM 51-40-08. REPLACED WITH NEW OEM PART,
- [SDR SWIA2025122775089](https://openairdocs.org/sdr/SWIA2025122775089.md): Seat Track · damaged · Dec 27, 2025 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CENTER FUSELAGE III LEFT INBD SEAT TRACK HAS SEVERAL DAMAGES FROM FR 74 TO FR 84. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA2025122775087](https://openairdocs.org/sdr/SWIA2025122775087.md): Seat Track · gouged · Dec 27, 2025 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT CENTER SEAT TRACK SEGMENT FR 43-59 HAS NICKS & GOUGES AT FRAMES 45, 47, 50, 52, 53, 56, AND 58. REMOVED AND REPLACED RT CENTER SEAT TRACK SEGMENT FR43-59. IAW SRM 51-40-08.
- [SDR SWIA2020121625091](https://openairdocs.org/sdr/SWIA2020121625091.md): Seat Track · corroded · Dec 26, 2025 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN LT SEAT TRACK FR 87. REMOVED AND REPLACED THE SEAT FR86 - FR 89. IAW SRM 51-40-08.
- [SDR SWIA2026012175090](https://openairdocs.org/sdr/SWIA2026012175090.md): Seat Track · corroded · Dec 26, 2025 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN RIGHT SEAT TRACK FROM FR.12-21. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA2025122475088](https://openairdocs.org/sdr/SWIA2025122475088.md): Mount · cracked · Dec 24, 2025 · N178SY · Emb ERJ170200LR · Fuselage, Equipment Attach Fittings
  > WEATHER RADAR LOWER MOUNTING BRACKET CRACKED. REMOVED AND REPLACED WEATHER RADAR LOWER MOUNTING BRACKET IAW SRM 51-40-08.
- [SDR SWIA2025082700005](https://openairdocs.org/sdr/SWIA2025082700005.md): Door · dented · Aug 25, 2025 · N178SY · Emb ERJ170200LR · Passenger/Crew Doors
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA99531-ETD2025-170-906479 MXCODEID110241-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 99531CATERING HIT THE AIRPLANE TOO HARD AS THEY PULLED UP TO THE AFT PASSENGER DOOR. COMPLY WITH ETD 2025-170-906479 PERMINANT REPAI
- [SDR SWIA20230428](https://openairdocs.org/sdr/SWIA20230428.md): Skin · gouged · Apr 28, 2023 · N178SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF VWS BOX FOUND 4 AREAS OF GOUGES ON EXTERNAL CF III SKIN AROUND FASTENER HOLES, AND 29 HOLES DRILLED OUT OF ROUND BETWEEN FR 88- 89, BETWEEN STGR 28R- 25R AS MARKED. (C-CHECK RO 5/12/2023) REPAIRED 4 AREAS OF GOUGES ON EXTERNAL CF III SKI
- [SDR SWIA2023051500424](https://openairdocs.org/sdr/SWIA2023051500424.md): Seat Track · corroded · Apr 24, 2023 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH INBOARD SEAT TRACK AFT OF THE CROWN TEETH BETWEEN FRAME 84 AND 85. (C-CHECK RO 5/12/2023) PERFORMED SEAT TRACK SPLICE FROM FR 82-85. SEE CONTINUATION FOR ALL WORK PERFORMED. REF ETD2023-170-010683. REPAIR PARTS ADDITIONAL WEIGHT IS 7.86O
- [SDR SWIA202305150002](https://openairdocs.org/sdr/SWIA202305150002.md): Waste Box · delaminated · Apr 24, 2023 · N178SY · Emb ERJ170200LR · Service Doors
  > CF III WASTE SERVICE BOX DELAMINATED AROUND ENTIRE TOP PERIMETER OF COMPOSITE BOX (C-CHECK RO 5/12/2023) REPAIRED CF III WASTE SERVICE BOX. REFERENCE SRM 53-23-60/REPAIR 02P. THIS REPAIR DOES NOT AFFECT THE AIRCRAFT'S WEIGHT AND BALLANCE. REF CONTINUAT
- [SDR SWIA202305150001](https://openairdocs.org/sdr/SWIA202305150001.md): Fitting · chafed · Apr 23, 2023 · N178SY · Emb ERJ170200LR · Cargo/Baggage Doors
  > FWD CARGO DOOR AFT 3 LATCH FITTINGS ON FUSELAGE HAVE MINOR CHAFE DAMAGE TO EDGES (3 EA) (C-CHECK RO 5/12/2023) REMOVED CHAFING AT FWD CARGO DOOR AFT 3 LATCHES ON THE FUSELAGE ORIG..775" LOSS.005" REMAINING.770" FOUND TO BE IN LIMITS REF EMB SRM 53-2
- [SDR SWIA2023051500422](https://openairdocs.org/sdr/SWIA2023051500422.md): Unknown · corroded · Apr 22, 2023 · N178SY · Emb ERJ170200LR · Fuselage Structure (General)
  > FWD WET AREA HAS CORROSION IN 1(EACH) LOCATION ON THE LH AFT FLOOR SILL AT FR 19. (C-CHECK RO 5/12/2023) REMOVED AND REPLACED FWD WET AREA LH AFT FLOOR SILL AT FR 19 REF SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS.
- [SDR SWIA202265279](https://openairdocs.org/sdr/SWIA202265279.md): None · delaminated · Apr 8, 2022 · N178SY · Emb ERJ170200LR · Ailerons
  > RIGHT HAND WING INBD FLAP IS REMOVED. (REF AMM 27-15-06) (FILED - CLOSED) INSTALLED NEW RIGHT HAND WING INBD FLAP IN REFERENCE TO AMM 27-15-06. RIG CHECKED GOOD FLAP OPERATES NORMAL FROM 0-45-0
- [SDR SWIA202264822](https://openairdocs.org/sdr/SWIA202264822.md): None · failed · Mar 13, 2022 · N178SY · Emb ERJ170200LR · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MESSAGE AFTER DEPARTURE. RAN QRH AND PREPARED FOR A NO FLAP LANDING. ON APPROACH, MOVED FLAP LEVER TO 1 TO USE SLATS AND THE EICAS MESSAGE WENT AWAY AND THE FLAPS WORKED FINE. (FLIGHT 3412 - FILED CLOSED) PERFORMED TROUBLESHOOTING OF FLAP
- [SDR SWIA202156086](https://openairdocs.org/sdr/SWIA202156086.md): Floor Support · broken · Jan 26, 2021 · N178SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT AT FR.85 INBOARD OF THE AFT PAX DOOR IS BROKEN. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED FLOOR SUPPORT FRAME 85 REF SRM 51-40-01
- [SDR SWIA202156085](https://openairdocs.org/sdr/SWIA202156085.md): Floor Support · corroded · Jan 24, 2021 · N178SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RH FLOOR SILL AT FR84 CORRODED. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED RH FLOOR SILL AT FR84 REF SRM 51-40-08 RESTORED SURFACE PROTECTION REF SRM 51-23-06
- [SDR SWIA202156084](https://openairdocs.org/sdr/SWIA202156084.md): Nut Plate · corroded · Jan 24, 2021 · N178SY · Emb ERJ170200LR · Cargo/Baggage Doors
  > FORWARD CARGO DOOR LOWER HORIZONTAL BEAM 4 NUT PLATES FROM THE FRONT ON THE SEAL REST HAVE 6 RIVET TAILS THAT ARE CORRODED. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED FORWARD CARGO DOOR LOWER HORIZONTAL BEAM 4 NUT PLATE RIVETS REF SRM 51-40-08
- [SDR SWIA202156079](https://openairdocs.org/sdr/SWIA202156079.md): Support · cracked · Jan 24, 2021 · N178SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > L/H WHEEL WELL FRAME 52 SUPPORT FOR AILERON FUSELAGE SECTOR CRACKED. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED L/H WHEEL WELL FRAME 52 SUPPORT FOR AILERON FUSELAGE SECTOR REF EMB SRM 51-40-08
- [SDR SWIA202156083](https://openairdocs.org/sdr/SWIA202156083.md): Gusset · corroded · Jan 23, 2021 · N178SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION AFT WET AREA - RH GUSSET PLATE AT FRAME 90 AT END OF SEAT TRACK IS CORRODED IN 3 PLACES. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED RH GUSSET PLATE AT FRAME 90 REF EMB SRM 51-40-08, 51-23-06. SEE CONTINUATION CARD FOR ALL WORK ACCOMPLISHED.
- [SDR SWIA202156082](https://openairdocs.org/sdr/SWIA202156082.md): Gusset · corroded · Jan 23, 2021 · N178SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION AFT WET AREA - RH GUSSET PLATE AT FRAME 90 IS CORRODED. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED RH GUSSET PLATE AT FR 90 REF EMB SRM 51-40-08 51-23-06. SEE CONTINUATION CARD FOR ALL WORK ACCOMPLISHED,
- [SDR SWIA202156078](https://openairdocs.org/sdr/SWIA202156078.md): Crossbeam · corroded · Jan 23, 2021 · N178SY · Emb ERJ170200LR · Fuselage Main, Frame
  > AFT WET AREA CORROSION - CORROSION ON FASTENER ON LH BEAM AT FRAME 87. (C-CHECK) RO 2/6/2021 / REMOVED AND REPLACED LH BEAM AT FR 87 REF EMB SRM 51-40-08. FACTORY REPLACEMENT PART HAS NO CHANGE IN WEIGHT
- [SDR SWIA202156081](https://openairdocs.org/sdr/SWIA202156081.md): Doubler · corroded · Jan 22, 2021 · N178SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FWD WET AREA- CORROSION L/H DOUBLER FRAMES 19 TO 20 AS MARKED. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED L-H DOUBLER BETWEEN FR 19-20. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.
- [SDR SWIA202156080](https://openairdocs.org/sdr/SWIA202156080.md): Support · corroded · Jan 22, 2021 · N178SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD WET AREA- CORROSION R/H SILL BETWEEN FRAMES 13 AND 14. (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED FWD WET AREA- R/H SILL BETWEEN FRAMES 12 -14 PER REF: SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.
- [SDR SWIA202156077](https://openairdocs.org/sdr/SWIA202156077.md): Seat Track · corroded · Jan 22, 2021 · N178SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA- CORROSION R/H INBSD SEAT TRACK LEADING EDGE TEETH BETWEEN FRAMES 17 AND 18 AS MARKED (C-CHECK) RO 2/6/2021 REMOVED AND REPLACED R-H I/B SEAT TRACK FR 12-20. REF EMB SRM 51-40-08. NO CHANGE IN WEIGHT. SEE CONTINUATION CARD FOR WORK ACCOMPLISHE

## 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 = 'N178SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N178SY/reports

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