# Service difficulty reports: N118SY

A list on [N118SY](https://openairdocs.org/aircraft/N118SY.md).

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

- [SDR SWIA2026093077334](https://openairdocs.org/sdr/SWIA2026093077334.md): Unknown · odor · Sep 30, 2026 · N118SY · Emb ERJ170200LR · Air Distribution System
  > ON CLIMB OUT FAS REPORTED A ODOR THAT WAS SWEETSMOKY ODOR WITH NO SMOKE VISIBLE WAS REPORTED AS SIMILAR TO DEUCE FLUID SMELL BUT NOT QUITE THE SAME THE ODOR FADED ON CLIMB OUT AND THEN RETURNED NEARING TOP OF CLIMB AFTER A FEW MINUTES AT TOP OF CLIMB THE ODOR
- [SDR SWIA2026081976951](https://openairdocs.org/sdr/SWIA2026081976951.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND LIGHTNING STRIKE ENTRANCE POINT ON RIVET AT STGR27L NEXT TO FRAME 18 (FILED CLOSED)REPLACED 1 DAMAGED RIVET ON LH SKIN @ STGR27L NEXT TO FRAME 18 IN REFERENCE TO ERJ 175 SRM 51-41-02**SEE CP 32576138 FOR LEAK/PRESSURE CHECK SIGN-OFF
- [SDR SWIA2026081976950](https://openairdocs.org/sdr/SWIA2026081976950.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND MELTED RIVET ON FR12 1 IN UP OFF 26L 1/2 RADIUS DUE TO LIGHTING STRIKE€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ FR12 AND STR 26L IN REFERENCE TO SRM 53-0
- [SDR SWIA2026081976949](https://openairdocs.org/sdr/SWIA2026081976949.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND 3 BURN MELTED SPOTS ABOVE 25L BY 1/2 IN BETWEEN FR12 AND FR13 ONE IS 1/4 RADIUS ONE IS 1/2 IN RADIUS AND ONE IS 3/4 RADIUS ALL GROUPED TOGETHER IN 1 IN 1/4" LONG DUE TO LIGHTING STRIKE€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIR
- [SDR SWIA2026081976948](https://openairdocs.org/sdr/SWIA2026081976948.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND A RIVET ON FR13 JUST ABOVE 25L MELTED DUE TO LIGHTING STRIKE 1/2 RADIUS €ŒSEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ FR13 JUST ABOVE STR 25L IN REFERENCE TO E
- [SDR SWIA2026081976947](https://openairdocs.org/sdr/SWIA2026081976947.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND AN ENTRANCE POINT OF LIGHTING STRIKE, LOOKS WELDED AT 2"BELOW 25L JUST OFF FR13 1/2 IN RADIUS€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. (FILED CLOSED)COMPLIED WITH PERMANENT BLENDING REPAIR OF "
- [SDR SWIA2026081976946](https://openairdocs.org/sdr/SWIA2026081976946.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND RIVET BURNT AT 26L AND FR14 DUE TO LIGHTING STRIKE€? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ STR 26L AND FR14 IN REFERENCE TO ERJ 175 SRM 51-43-04.
- [SDR SWIA2026081976945](https://openairdocs.org/sdr/SWIA2026081976945.md): Skin · damaged · Aug 19, 2026 · N118SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FOUND RIVET AT 26L AND FR15 BURNT AND DEFORMED DUE TO LIGHTING STRIKE.? SEE ETD 2026-170-014053 FOR ADDITIONAL INFORMATION. DAMAGE REQUIRES EVALUATION AND DISPOSITION. REPLACED 1 FASTENER ON FUSELAGE SKIN @ 26L AND FR15 IN REFERENCE TO ERJ 175 SRM 51-43-04
- [SDR SWIA2025090200012](https://openairdocs.org/sdr/SWIA2025090200012.md): Slat Track · chafed · Aug 12, 2025 · N118SY · Emb ERJ170200LR · Leading Edge Devices
  > RIGHT SLAT NR 4 TRACK RIB 8, INTERNAL OF SLAT CHAFED. REMOVED AND REPLACED RT SLAT PANEL NR 4 IAW AMM 27-81-08 & 30-11-06.
- [SDR SWI2025F01140](https://openairdocs.org/sdr/SWI2025F01140.md): Crossbeam · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > FRAME 19 CROSSBEAM CORRODED OUTBOARD OF LH SEAT TRACK. PERFORMED PERMANTENT DOUBLER REPAIR ON THE CROSSBEAM IAW ETD2025-170-926443.
- [SDR SWI2025F01139](https://openairdocs.org/sdr/SWI2025F01139.md): Shear Tie · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION AT AFT CARGO SHEAR CLIP AT FR 89 STGR 29R-29L REMOVED AND REPLACED AFT CARGO SHEAR CLIP AT FR 89 STGR 29R-29L REF: SRM 51-40-08.
- [SDR SWI2025F01138](https://openairdocs.org/sdr/SWI2025F01138.md): Seat Track · chafed · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT LATERAL SEAT TRACK HAS CHAFING DAMAGE AT FR 84/83, 82/83, 81/82, 80/81, 79/80, 78/79, 77/78, 76/77, 75/76, 74/75. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08. REPLACED WITH NEW OEM PART,
- [SDR SWI2025F01137](https://openairdocs.org/sdr/SWI2025F01137.md): Seat Track · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > AFT WET AREA RT SEAT TRACK HAS CORROSION AT FR 87. REMOVED AND REPLACED AFT WET AREA RT SEAT TRACK BETWEEN FR86 - FR89 REF: SRM 51-40-08.
- [SDR SWI2025F01136](https://openairdocs.org/sdr/SWI2025F01136.md): Seat Track · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR, LT INBD SEAT TRACK CORRODED BETWEEN FRS 19-20. REMOVED AND REPLACED THE SEAT TRACK BETWEEN FR 12-20 IAW SRM 51-40-08.
- [SDR SWI2025F01135](https://openairdocs.org/sdr/SWI2025F01135.md): Seat Track · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > PAX FLOOR, RT SEAT TRACK CORRODED AT FR17. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
- [SDR SWI2025F01134](https://openairdocs.org/sdr/SWI2025F01134.md): Seat Track · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK HAS CORROSION AT FR 84, 84/83, 82/83, 81/82, 80/81, 79/80, 78/79, 77/78, 76/77, 75/76, 74/75. REMOVED DAMAGED SECTION OF THE LT CENTER SEAT TRACK AT FRAME 84 AND INSTALLED A FABRICATED FILLER AND DOUBLER TO REPAIR REF ETD2025-170-926606 AND RE
- [SDR SWI2025F01133](https://openairdocs.org/sdr/SWI2025F01133.md): Seat Track · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK HAS CORROSION AT FR 84, 84/83, 82/83, 81/82, 80/81, 79/80, 78/79, 77/78, 76/77, 75/76, 74/75. REMOVED AND REPLACED RT INBD SEAT TRACK FR74-84 REF SRM 51-40-08.
- [SDR SWI2025F01132](https://openairdocs.org/sdr/SWI2025F01132.md): Floorbeam · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > PAX FLOOR, FR 14 CROSSBEAM CORRODED AT RH TRACK/ BEAM. PERFORMED SRM DOUBLER REPAIR AT PAX FLOOR, FR 14 CROSSBEAM AT RH TRACK REF SRM 53-00-10/REPAIR 03P. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06.CPM 51-25-00 (PO:331184)NO CHANGE TO WEI
- [SDR SWIA2025090200806](https://openairdocs.org/sdr/SWIA2025090200806.md): Beam · corroded · Aug 6, 2025 · N118SY · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT WET AREA LH BEAM HAS CORROSION AT FR 87. INSTALLED AFT WET AREA LH BEAM BETWEEN FR86 - FR89 IAW SRM 51-40-08.
- [SDR SWIA2025090200803](https://openairdocs.org/sdr/SWIA2025090200803.md): Rib · cracked · Aug 3, 2025 · N118SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > RH HORIZONTAL STAB RIB 12 HAS SUSPECTED CRACK ON UPPER SIDE 4TH RIVET FROM THE FRONT BETWEEN FRONT SPAR AND UPPER SKIN STRINGER 2. REMOVED AND REPLACED RH HORIZONTAL STAB RIB 12 REF: SRM 51-40-08 ETD2025-170-926732 (P.O# 325561).
- [SDR SWI2024F00289](https://openairdocs.org/sdr/SWI2024F00289.md): Seat Track · cracked · Apr 17, 2024 · N118SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT FLOOR TRACK AT SEAT 19C IS CRACKED. (FILED CLOSED)REMOVED AND REPLACED THE SEAT FLOOR TRACK AT SEAT 19C IN REF TO AMM 25-21-11
- [SDR SWIA202265981](https://openairdocs.org/sdr/SWIA202265981.md): None · worn · Jun 12, 2022 · N118SY · Emb EMB110* · Aileron Tabs
  > LH WING FLAP TRACK 2A OB HAS WIDTH REDUCTION OF 1.0 MM DEEPEST LOCATION ENTIRE LENGTH. FOUND TO BE OUT OF LIMITS. ASST # QA-50384 DUE 2-21-23. (C-CHECK RO 7/1/2022) REMOVED AND REPLACED LH WING FLAP TRACK 2A OB IN REF WITH EMB 175 AMM 57-54-25 HG2-5000
- [SDR SWIA202265980](https://openairdocs.org/sdr/SWIA202265980.md): None · worn · Jun 12, 2022 · N118SY · Emb EMB110* · Aileron Tabs
  > RH WING FLAP TRACK 2A OB HAS WIDTH REDUCTION OF 1.1 MM DEEPEST LOCATION ENTIRE LENGTH. FOUND TO BE OUT LIMITS. ASST # QA-50384 DUE 2-21-23. (C-CHECK RO 7/1/2022) REMOVED AND REPLACED RH WING FLAP TRACK 2A OB IN REF WITH EMB 175 AMM 57-54-25 HG2-50002 DU
- [SDR SWIA202265979](https://openairdocs.org/sdr/SWIA202265979.md): None · corroded · Jun 12, 2022 · N118SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT SHEAR CLIP IS CORRODED AT FR 82 STGR 27R. (C-CHECK RO 7/1/2022) REMOVED AND REPLCED AFT CARGO COMPARTMENT SHEAR CLIP AT FR 82 STGR 27R REF EMB SRM 51-40-08. THE PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWIA202265978](https://openairdocs.org/sdr/SWIA202265978.md): None · corroded · Jun 12, 2022 · N118SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT SHEAR CLIP IS CORRODED AT FR 83 STGR 27R. (C-CHECK RO 7/1/2022) REMOVED AND REPLCED AFT CARGO COMPARTMENT SHEAR CLIP AT FR 83 STGR 27R REF EMB SRM 51-40-08. THE PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWIA202265977](https://openairdocs.org/sdr/SWIA202265977.md): None · corroded · Jun 12, 2022 · N118SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT SHEAR CLIP IS CORRODED AT FR 85 STGR 26R. (C-CHECK RO 7/1/2022) REMOVED AND REPLCED AFT CARGO COMPARTMENT SHEAR CLIP AT FR 85 STGR 26R REF EMB SRM 51-40-08. THE PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED
- [SDR SWIA201743073](https://openairdocs.org/sdr/SWIA201743073.md): Doubler · damaged · Feb 14, 2017 · N118SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT DOUBLER DAMAGED. REPAIRED IAW ETD.
- [SDR SWIA201743072](https://openairdocs.org/sdr/SWIA201743072.md): Doubler · damaged · Feb 14, 2017 · N118SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD DOUBLER DAMAGED. REPAIRED IAW ETD.

## 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 = 'N118SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N118SY/reports

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