# Service difficulty reports: N183SY

A list on [N183SY](https://openairdocs.org/aircraft/N183SY.md).

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

- [SDR SWIA2026082476959](https://openairdocs.org/sdr/SWIA2026082476959.md): Rib · out of limits · Aug 24, 2026 · N183SY · Emb ERJ170200LR · Horizontal Stabilizer Structure
  > COMPLY WITH SB 170-55-0014, HORIZONTAL STAB CENTER BOX AT RIBS 10A, 11A, & 12A REPLACEMENT REV 01 PART 0. COMPLIED WITH SB 170-55-0014 STABILIZERS - HORIZONTAL STABILIZER CENTER BOX €“ RIBS 10A, 11A AND 12A REPLACEMENT REV 01 PART(S) 0.
- [SDR SWIA2026082077109](https://openairdocs.org/sdr/SWIA2026082077109.md): Flap Track · worn · Aug 20, 2026 · N183SY · Emb ERJ170200LR · Trailing Edge Flaps
  > RH WING FLAP TRACK 2A OUTBOARD HAS WIDTH REDUCTION WEAR OF 1.13MM MAX ALONG ENTIRE LENGTH. REMOVED AND REPLACED RH WING FLAP TRACK 2A OUTBOARD.REF. EMB AMM. 57-54-25.ASSET. TC2-50254 DUE. 9-24-26
- [SDR SWIA2026081777107](https://openairdocs.org/sdr/SWIA2026081777107.md): Seat Track · gouged · Aug 17, 2026 · N183SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBOARD FIRST CLASS SEAT TRACK SEGMENT FR22/23 - 34/43 HAS 7 LOCATIONS WITH GOUGES BETWEEN FR23-29. REMOVED AND REPLACED LH INBOARD FIRST CLASS SEAT TRACK SEGMENT FR22/23 - 34/43. REF SRM 51-40-08. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD
- [SDR SWIA2026081777103](https://openairdocs.org/sdr/SWIA2026081777103.md): Beam · corroded · Aug 17, 2026 · N183SY · Emb ERJ170200LR · Fuselage Main, Structure
  > FORWARD PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION DAMAGE AT UPPER EDGE OF BOTH FORWARD AND AFT GIRT BAR FLOOR FITTING CUTOUTS AND UPPER SURFACE OF THE BEAM AT AFT GIRT BAR FITTING SERRATED PLATE CUTOUTS. REMOVED AND REPLACED FORWARD PASSENGER DOOR CUTOUT
- [SDR SWIA2026081477106](https://openairdocs.org/sdr/SWIA2026081477106.md): Seat Track · corroded · Aug 14, 2026 · N183SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FWD WET AREA R/H SEAT TRACK BETWEEN FR12-21 IN 9 LOCATIONS AS MARKED. REMOVED AND REPLACED R/H SEAT TRACK BETWEEN FR12-21, REF SRM 51-40-08.SEE CONTINUATION CARD FOR ADDITIONAL WORK PERFORMED. NO CHANGE TO WEIGHT AND BALANCE.
- [SDR SWIA2026080477108](https://openairdocs.org/sdr/SWIA2026080477108.md): Antenna · demodification · Aug 4, 2026 · N183SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > COMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PAR
- [SDR SWIA2026080477105](https://openairdocs.org/sdr/SWIA2026080477105.md): Antenna · demodification · Aug 4, 2026 · N183SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > COMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PA
- [SDR SWIA2026080477104](https://openairdocs.org/sdr/SWIA2026080477104.md): Antenna · demodification · Aug 4, 2026 · N183SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > COMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93. REPAIR PARTS WEIGH 330.1 GRAMS NO CHANGE TO WEIGHT AND BALA
- [SDR SWIA2026080477102](https://openairdocs.org/sdr/SWIA2026080477102.md): Antenna · demodification · Aug 4, 2026 · N183SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > COMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PARTS LESS THAN
- [SDR SWI2025F01741](https://openairdocs.org/sdr/SWI2025F01741.md): Indicator · sheared · Dec 6, 2025 · N183SY · Emb ERJ170200LR · Door Warning System
  > DOOR PAX AFT OPEN - WARNING RECEIVED CLIMBING THRU 16000 FEET. QRH PROCEDURE COMPLETE. (FLIGHT 3191) INTERROGATED CMC FUND PAX DOOR MESSAGE WITH NO CORRELATIONS. TROUBLESHOT IN REFERENCE TO FIM 52-72-00. CHECKED -W- MEASUREMENT BETWEEN POSITION INDICATOR TA
- [SDR SWIA2023100528](https://openairdocs.org/sdr/SWIA2023100528.md): Unknown · cracked · Sep 28, 2023 · N183SY · Emb ERJ170200LR · Aerodynamic Fairings
  > AFT BELLY FAIRING R/H CTR UPPER ATTACH FLANGE HAS CRACK THROUGH FASTENER HOLE AT SUPPORT BRACKET FWD OF FR 58 BETWEEN STGR 19R- STGR 17R AS MARKED. (C-CHECK RO 10/3/2023) PERFORMED PERMANENT REPAIR TO AFT BELLY FAIRING R/H CTR UPPER ATTACH FLANGE REF EMB 1
- [SDR SWIA20231005915](https://openairdocs.org/sdr/SWIA20231005915.md): Unknown · gouged · Sep 15, 2023 · N183SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES/ EXPOSED METAL /CORROSION ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 11 LOCATIONS (3 IN FLOOR OF TRACK) AS MARKED. (C-CHECK RO 10/3/2023) REMOVED AND REPLACED RH IB SEAT TRACK AT FR23-34. REF EMB SRM 51-40-08. THIS DOES NOT EFFECT WEIGHT AND BALANC
- [SDR SWIA20231005914](https://openairdocs.org/sdr/SWIA20231005914.md): Shear Tie · corroded · Sep 14, 2023 · N183SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR CLIP AT FR85 BETWEEN STGR 27R-28R AS MARKED. (C-CHECK RO 10/3/2023) REMOVED AND REPLACED SHEAR CLIP AT FR85 BETWEEN STGR 27R-28R REF SRM 51-40-08. SEE CONTINUATION CARD FOR DETAILED STEPS PERFORMED. REPLACEMENT OF THIS SHEAR CLIP DOES NO
- [SDR SWIA20231005913](https://openairdocs.org/sdr/SWIA20231005913.md): Unknown · gouged · Sep 13, 2023 · N183SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR74-84 IN 11 LOCATIONS AS MARKED. (C-CHECK RO 10/3/2023) REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR74-84 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR DETAILED STEPS PERFORMED. REPLACEMENT OF THIS SEAT TR
- [SDR SWIA202161545](https://openairdocs.org/sdr/SWIA202161545.md): None · missing · Oct 4, 2021 · N183SY · Emb ERJ170200LR · Tire
  > BRK OVERHEAT, LG NO DISPATCH MESSAGES AFTER LANDING. LEFT OB BRAKE TEMP 450 AND IB 21. DURING POST FLT. WALK AROUND, FO FOUND LEFT GEAR IB LANDING GEAR WHEEL MISSING. (FLIGHT 3359 - FILED CLOSED) REMOVED AND REPLACED THE LH MLG SLIDING TUBE ASSEMBLY IN A
- [SDR SWIA202158827](https://openairdocs.org/sdr/SWIA202158827.md): Floor Panel · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- FWD WET AREA, RH SILL PANEL HAS 2EA AREAS OF CORROSION BETWEEN FR 18-19 AS MARKED. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED RH SILL PANEL BETWEEN FR 18-19 AS MARKED. REF EMB SRM 51-40-08 APLLIED SURFCE PROTECTION PER SRM 51-23-06
- [SDR SWIA202158826](https://openairdocs.org/sdr/SWIA202158826.md): Floor Panel · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Floor Panel
  > CORROSION- FWD WET AREA, RH STILL PANEL HAS 2EA AREAS OF CORROSION AS MARKED. FR12-14. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED FWD WET AREA, RH STILL PANEL AT FRAME 12-14 PER SRM 51-40-08 APLLIED TOP COAT PER SRM 51-23-06
- [SDR SWIA202158825](https://openairdocs.org/sdr/SWIA202158825.md): Support Bracket · broken · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA- 2EA PANEL SUPPORT BRACKETS BROKEN OFF ON FR 86 ON RH & LH SIDE AS MARKED. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED AFT WET AREA- 2EA PANEL SUPPORT BRACKETS ON FR 86 ON RH & LH SIDE AS MARKED.REF: EMB SRM 51-40-08 APPLIED SURFACE PROTECT
- [SDR SWIA202158824](https://openairdocs.org/sdr/SWIA202158824.md): Gusset · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- AFT WET AREA, RH INBD GUSSET PLATE HAS CORROSION ON FR 89 AS MARKED. (C-CHECK RO 6/18/2021) / REMOAVED AND REPLACED RH INBD GUSSET PLATE FR 89 REF SRM 51-40-08
- [SDR SWIA202158823](https://openairdocs.org/sdr/SWIA202158823.md): Gusset · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- AFT WET AREA, RH INBD GUSSET PLATE HAS CORROSION ON FR 90 AS MARKED. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED RH INBD GUSSET PLATE FR 90 REF SRM 51-40-08
- [SDR SWIA202158822](https://openairdocs.org/sdr/SWIA202158822.md): Gusset · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- AFT WET AREA, RH OUTBD GUSSET PLATE HAS CORROSION ON FR 90 AS MARKED. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED RH OUTBD GUSSET PLATE FR 90 REF SRM 51-40-08
- [SDR SWIA202158821](https://openairdocs.org/sdr/SWIA202158821.md): Floor Support · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- AFT WET AREA, RH OUTBD PANEL SUPPORT(FR88-90) HAS AREAS OF CORROSION AS MARKED. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED RH OUTBD PANEL SUPPORT(FR88-90 REF SRM 51-40-08
- [SDR SWIA202158820](https://openairdocs.org/sdr/SWIA202158820.md): Support · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- AFT WET AREA, LH OUTBD PANEL SUPPORT(FR88-90) HAS CORROSION ON FWD END AS MARKED. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED LH OUTBD PANEL SUPPORT(FR88-90) REF SRM 51-40-08
- [SDR SWIA202158819](https://openairdocs.org/sdr/SWIA202158819.md): Shear Panel · corroded · May 27, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION- AFT WET AREA, RH SHEAR PANEL HAS AREAS OF CORROSION AS MARKED. FR-87-88. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED RH SHEAR PANEL AFT WET AREA FR 87-FR 88 REF SRM 51-40-08
- [SDR SWIA202158818](https://openairdocs.org/sdr/SWIA202158818.md): Floorbeam · cracked · May 25, 2021 · N183SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > COCKPIT FLOOR SUPPORT BRACKET CRACKED AT FRAME 12 ON PILOTS SIDE. / (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED CKPT FLOOR SUPPORT BRACKET AT FR12 ON PILOT'S SIDE REF EMB SRM 51-40-08 AND 51-41-01, 51-40-02, 51-23-04, 51-23-05 AND 51-23-06 AND CPM 51-25
- [SDR SWIA202158817](https://openairdocs.org/sdr/SWIA202158817.md): Floor Support · cracked · May 25, 2021 · N183SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > COCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED ANGLE. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED CKPT FLOOR ANGLE BETWEEN FR 11-12 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202158816](https://openairdocs.org/sdr/SWIA202158816.md): Bulkhead · cracked · May 24, 2021 · N183SY · Emb ERJ170200LR · Fuselage Main, Structure
  > FRAME 52 LH WING STUB VAPOR BARRIER, ANGLE CRACKED OUT OF FASTENER HOLE. (C-CHECK RO 6/18/2021) / REMOVED AND REPLACED FRAME 52 LH WING STUB VAPOR BARRIER ANGEL REF SRM 51-23-06, 51-40-08. BACK SEALED FASTENERS INSIDE FUEL TANK REF SRM 51-21-05. APPLIED
- [SDR SWIA202158815](https://openairdocs.org/sdr/SWIA202158815.md): Panel · corroded · May 24, 2021 · N183SY · Emb ERJ170200LR · Standard Practices/Structures
  > PANEL 192CR HAS CORROSION ON INSIDE FLANGE. (C-CHECK RO 6/18/2021)BLENDED FLANGE INSIDE PANEL 192CR. CORROSION REMAINS. REMOVED AND REPLACED FLANGE REF EMB SRM 51-10-03, 51-40-08, 51-40-04, 51-41-02, 51-23-04, 51-23-05, 51-23-06.

## 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 = 'N183SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N183SY/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.