# Service difficulty reports: N171SY

A list on [N171SY](https://openairdocs.org/aircraft/N171SY.md).

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

- [SDR SWIA2026021775292](https://openairdocs.org/sdr/SWIA2026021775292.md): Bleed Air Sys · warning message · Feb 17, 2026 · N171SY · Emb ERJ170200LR · Pneumatic Distribution System
  > ON CLIMBOUT. BLEED 1 OVERPRESSURE MESSAGE ON CLIMBOUT. RAN QRH. MESSAGE DID NOT EXTINGUISH AFTER FIRST STEP. AFTER 2ND STEPS OF PROCEDURE MESSAGE EXTINGUISHED. (FLIGHT 3439). MX ACTION CW IAW AMM 36-11-03-040-801-A. INTERROGATED CMC, FOUND FAULT 36111210AM
- [SDR SWIA2025100600929](https://openairdocs.org/sdr/SWIA2025100600929.md): Skin · dented · Sep 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DUE TO BIRD STRIKE, FOUND DENT ON FWD FUSELAGE LOWER LH SIDE SKIN. THE DENT IS LOCATED BETWEEN FR01 AND FR02, AND BETWEEN STGR 25L AND STGR 26L. IT MEASURES 3.3 INCHES LONG, 2.75 INCHES WIDE, AND 0.077 INCHES DEEP. THERE IS A CREASE AND OIL CANNING PRESENT. (
- [SDR SWIA202509300029](https://openairdocs.org/sdr/SWIA202509300029.md): Skin · dented · Sep 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DUE TO BIRD STRIKE, FOUND DENT ON FWD FUSELAGE LOWER LH SIDE SKIN. THE DENT IS LOCATED BETWEEN FR01 AND FR02, AND BETWEEN STGR 25L AND STGR 26L. IT MEASURES 3.3 INCHES LONG, 2.75 INCHES WIDE, AND 0.077 INCHES DEEP. THERE IS A CREASE AND OIL CANNING PRESENT. (
- [SDR SWIA2025070100629](https://openairdocs.org/sdr/SWIA2025070100629.md): Skin · damaged · Jun 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY MAJOR REPAIR, COMPLIED WITH PERMANENT REPAIR OF RT AFT SIDE OF FUSELAGE SKIN, BETWEEN HYDRAULIC SYSTEM
- [SDR SWIA2025063000029](https://openairdocs.org/sdr/SWIA2025063000029.md): Skin · ground damage · Jun 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > FUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWI2025F00632](https://openairdocs.org/sdr/SWI2025F00632.md): Seat Track · gouged · Apr 21, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > R/H PASSENGER CABIN FLOOR O/B LATERAL SEAT TRACK AT FR20 TO FR21 HAS GOUGE (C-CHECK RO 05/11/2025)REMOVED AND REPLACED R/H PASSENGER CABIN FLOOR O/B LATERAL SEAT TRACK BETWEEN FR16 TO FR20. REF: SRM 51-40-08. SEAT TRACK REPLACE WITH OEM PART NO CHANGE TO WEIG
- [SDR SWI2025F00631](https://openairdocs.org/sdr/SWI2025F00631.md): Seat Track · corroded · Apr 21, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > R/H PASSENGER CABIN FLOOR AT FR17 R/H SEAT TRACK HAS SURFACE CORROSION (C-CHECK RO 05/11/2025)REPAIRED R/H PASSENGER CABIN FLOOR AT FR17 R/H SEAT TRACK IN ACCORDANCE WITH REF EMB SRM 53-10-10/REPAIR 01.
- [SDR SWIA202505120421](https://openairdocs.org/sdr/SWIA202505120421.md): Seat Track · corroded · Apr 21, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > L/H PASSENGER CABIN FLOOR AT FR17 L/H SEAT TRACK HAS SURFACE CORROSION (C-CHECK RO 05/11/2025)REMOVED AND REPLACED L/H PASSENGER CABIN FLOOR BTW FR12-FR20 L/H SEAT TRACK. REF: EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.
- [SDR SWIA20250512419](https://openairdocs.org/sdr/SWIA20250512419.md): Seat Track · corroded · Apr 19, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH FLOOR SEAT TRACK AT FR 76 AND 80. (C-CHECK RO 05/11/2025)REMOVED AND REPLACED RH FLOOR SEAT TRACK AT FR 76-80 IN ACCODANCE WITH ETD2022-170-022163-C. REPLACED WITH NEW OEM PART. NO CHANGE TO WEIGHT AND BALANCE REQUIRED.
- [SDR SWI2025F00630](https://openairdocs.org/sdr/SWI2025F00630.md): Rib · cracked · Apr 18, 2025 · N171SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > CRACK RH HORIZONTAL RIB 12 LOWER FWD FLANGE AT AFT RIVET. (C-CHECK RO 05/11/2025)REMOVED AND REPLACED RH HORIZONATL RIB 12 REF. EMB SRM 51-40-08, AND ETD2025-170-906827.
- [SDR SWIA20250512418](https://openairdocs.org/sdr/SWIA20250512418.md): Rib · cracked · Apr 18, 2025 · N171SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > SUSPECTED CRACK LH HORIZONTAL RIB 12 LOWER FWD FLANGE AT AFT RIVET. (C-CHECK RO 05/11/2025)REMOVED AND REPLACED HORIZONTAL RIB 12 REF. EMB SRM 51-40-08, AND ETD2025-170-906827.
- [SDR SWIA202266588](https://openairdocs.org/sdr/SWIA202266588.md): None · corroded · Sep 23, 2022 · N171SY · Emb EMB110* · Fuselage Main, Frame
  > AFT WET AREA R/H LONGITUDINAL BEAM HAS CORROSION ON THE TOP SURFACE AT FR. 88. (C-CHECK RO 10/4/2022) / REMOVED AND REPLACED AFT WET AREA R/H LONGITUDINAL BEAM AT FR 88 REF SRM 51-40-08. APPLIED SURFACE PROTECTION REF SRM 51-23-06. NO CHANGE TO WEIGHT
- [SDR SWIA202266587](https://openairdocs.org/sdr/SWIA202266587.md): None · gouged · Sep 15, 2022 · N171SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > CF I L/H INBOARD SEAT TRACK HAS MULTIPLE AREAS OF GOUGES FROM FR 22 TO FR 29 AS MARKED (C-CHECK RO 10/4/2022) CORRECT LOCATION OF SEAT TRACK REPAIR IS FR 23- 27. SPLICED IN SEAT TRACK FILLER PN PE11056-F3A INTO CFI L/H INBOARD SEAT TRACK FROM FR23 TO FR
- [SDR SWIA202266586](https://openairdocs.org/sdr/SWIA202266586.md): None · gouged · Sep 15, 2022 · N171SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > CF I R/H INBOARD SEAT TRACK HAS MULTIPLE GOUGES FROM FWD OF FR23 TO FR34 AS MARKED (C-CHECK RO 10/4/2022) REMOVED AND REPLACED CFI R/H INBOARD SEAT TRACK FR23 TO FR34 REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
- [SDR SWIA2020022748854](https://openairdocs.org/sdr/SWIA2020022748854.md): Doubler · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > CORROSION IN L/H O/B DOUBLER BETWEEN FR.87-88. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED CORRODED LH O/B DOUBLER BETWEEN FR87-88 REF SRM. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2020022748853](https://openairdocs.org/sdr/SWIA2020022748853.md): Floor Support · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN R/H FLOOR SUPPORT BETWEEN FR.90-90A. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H FLOOR SUPPORT BETWEEN FR.90-90A PER REF: SRM APPLIED SURFACE PROTECTION PER REF: SRM, APPLIED CIC PER REF: CPM SEE CONTINUATION CARD FOR WORK PREFORMED
- [SDR SWIA2020022748852](https://openairdocs.org/sdr/SWIA2020022748852.md): Seat Track · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN L/H SEAT TRACK FR.84. (C-CHECK) RO 2/22/2020 REMOVED CORROSION ON AFT END OF OTBD CROWN CORNER ON L/H SEAT TRACK AT FR.84. DAMAGE AREA: L = 0.296" X W = 0.093" X D = 0.100". CROWN NOMINAL: 0.354". REMAINING MATERIAL: 0.344". REF EMB SRM. CALI
- [SDR SWIA2020022748851](https://openairdocs.org/sdr/SWIA2020022748851.md): Floor Support · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN R/H O/B SILL FROM FR.88-90. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H O/B SILL FROM FR.88-90. PER REF: SRM SEE CONTINUATION CARD FOR WORK PREFORMED
- [SDR SWIA2020022748850](https://openairdocs.org/sdr/SWIA2020022748850.md): Structure · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN R/H O/B SILL FR.84. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H O/B SILL FR.84. PER REF: SRM SEE CONTUINUATION CARD FOR WORK PREFORMED
- [SDR SWIA2020022748849](https://openairdocs.org/sdr/SWIA2020022748849.md): Floor Support · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN L/H FLOOR SUPPORT FR.87. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED L/H FLOOR SUPPORT FR.87. PER REF: SRM SEE CONTINUATION CARD FOR WORK PREFORMED
- [SDR SWIA2020022748848](https://openairdocs.org/sdr/SWIA2020022748848.md): Structure · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN R/H O/B SILL FR.17. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED ON R/H O/B SILL FR 17-21, REF. SRM AND RESTORED SURFACE PROTECTION RIVETS HEAD, REF. SRM.
- [SDR SWIA2020022748847](https://openairdocs.org/sdr/SWIA2020022748847.md): Structure · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN R/H O/B SILL FR.14. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H O/B SILL FR.14. REF SRM.
- [SDR SWIA2020022748846](https://openairdocs.org/sdr/SWIA2020022748846.md): Floor Support · cracked · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CRACK IN R/H FLOOR SUPPORT FR.86. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H FLOOR SUPPORT FR.86 PER REF SRM. APPLIED SURFACE PROTECTION PER REF SRM APPLIED CIC PER CPM.
- [SDR SWIA2020022748845](https://openairdocs.org/sdr/SWIA2020022748845.md): Angle · cracked · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CRACK IN ANGLE FR.12 LBL 38". (C-CHECK) RO 2/22/2020 REMOVED, LOCATED, DRILLED AND INSTALLED FR 12 ANGLE AT LBL 38 PER SRM AND SRM.
- [SDR SWIA2020022748844](https://openairdocs.org/sdr/SWIA2020022748844.md): Angle · cracked · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CRACK IN ANGLE FR.12 AT BL 0". (C-CHECK) RO 2/22/2020 REMOVED, LOCATED, DRILLED AND INSTALLED FR 12 ANGLE AT BL0 PER SRM AND SRM.
- [SDR SWIA2020022748842](https://openairdocs.org/sdr/SWIA2020022748842.md): Skin · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > CORROSION IN FR.84 RBL 27". (C-CHECK) RO 2/22/2020 REMOVED CORROSION AT FR 84 RBL 27". INSTALLED DOUBLER AND FILLER REF ETD.
- [SDR SWIA2020022748841](https://openairdocs.org/sdr/SWIA2020022748841.md): Frame · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION IN FR.84 LBL 32". (C-CHECK) RO 2/22/2020 COMPLIED WITH INSTALL OF OUTER DOUBLER AND REINFORECEMNT L ANGLE ON FR 84 LBL 32" PER ETD- SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. THIS REPAIR DOES NOT ADVERSELY AFFECT A FATIGUE CRITICAL STR
- [SDR SWIA2020022748840](https://openairdocs.org/sdr/SWIA2020022748840.md): Seat Track · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN R/H SEAT TRACK FR.84. (C-CHECK) RO 2/22/2020 SPLICE IN NEW R/H SEAT TRACK FR.84 REF ETD.
- [SDR SWIA2020022748839](https://openairdocs.org/sdr/SWIA2020022748839.md): Seat Track · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN L/H BEAM FR.18-20 LBL 10". (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED LH SEAT TRACK BEAM FR 12-FR20 REF EMB SRM.
- [SDR SWIA2020022748838](https://openairdocs.org/sdr/SWIA2020022748838.md): Seat Track · corroded · Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION IN R/H BEAM FR.16-20 RBL 10". (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H BEAM FR.16-20 RBL 10". REF EMB SRM.
- [SDR SWIA2020022748843](https://openairdocs.org/sdr/SWIA2020022748843.md): Attach Angle · cracked · Feb 6, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > LH ATTACH ANGLE AT FRAME 52 CRACKED (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED LH ATTACH ANGLE AT FRAME 52 REF EMB SRM

## 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 = 'N171SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N171SY/reports

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