# Service difficulty reports: N149SY

A list on [N149SY](https://openairdocs.org/aircraft/N149SY.md).

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

- [SDR SWIA2026070676706](https://openairdocs.org/sdr/SWIA2026070676706.md): Floorbeam · corroded · Jul 6, 2026 · N149SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > CORROSION ON LT FLOORBEAM AT FR 87, Y= -10". REMOVED AND REPLACED LH FLOORBEAM AT FR 87, Y= -10" PER SRM 51-40-08.
- [SDR SWIA2026070676705](https://openairdocs.org/sdr/SWIA2026070676705.md): Seat Track · corroded · Jul 6, 2026 · N149SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD FUSELAGE PASSENGER CABIN FLOOR STRUCTURE WET AREA RH TRACK AT FRAMES 16-19 AT Y+10IN TO Y+14IN HAVE SIGNS OF CORROSION AND BUBBLING PAINT. REMOVED AND REPLACED FORWARD FUSELAGE PASSENGER CABIN FLOOR STRUCTURE WET AREA RT TRACK AT FRAMES 16-19 AT Y+10I
- [SDR SWIA2026070676704](https://openairdocs.org/sdr/SWIA2026070676704.md): Seat Track · worn · Jul 6, 2026 · N149SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT TRACK HAS WEAR BETWEEN FRAMES 78 AND 79, FRAMES 80 AND 81, AND FRAMES 82 AND 83. REMOVED AND REPLACED LEFT-HAND FLOOR SEAT TRACK FR 74-84 PER E175 SRM 51-40-08.
- [SDR SWIA20230713622](https://openairdocs.org/sdr/SWIA20230713622.md): Unknown · nicked · Jun 22, 2023 · N149SY · Emb ERJ170200LR · Cargo/Baggage Doors
  > AFT CARGO DOOR (2) FUSELAGE FORWARD LATCH FITTINGS HAS NICK DAMAGE. (C-CHECK RO 7/12/2023) COMPLIED WITH BLEND OF AFT CARGO DOOR LATCH FITTINGS AS MARKED. FOUND TO BE WITHIN LMITS PER SRM 53-23-29/AD02. REPAIR INSPECTION INTERVAL 3133FC TME LIMIT N/A SS
- [SDR SWI2023F00133](https://openairdocs.org/sdr/SWI2023F00133.md): Unknown · corroded · Jun 21, 2023 · N149SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH IB SEAT TRACK HAS CORROSION AND CHAFFING AS MARKED FR 21- FR 34 (C-CHECK RO 7/12/2023) REMOVED AND REPLACED RH IB SEAT TRACK FR23-34. PART REPLACED WITH NEW OEM PART. THIS ACTION DOES NOT AFFECT THE AIRCRAFT WEIGHT AND BALANCE. SEE CONTINUATION FOR D
- [SDR SWI2023F00132](https://openairdocs.org/sdr/SWI2023F00132.md): Unknown · corroded · Jun 21, 2023 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 7/12/2023) REMOVED AND REPLACED RH LONGITUDINAL FLOOR BEAM AT FR 87. REF EMB SRM 51-40-08. THIS ACTION DOES NOT
- [SDR SWI2023F00131](https://openairdocs.org/sdr/SWI2023F00131.md): Unknown · corroded · Jun 21, 2023 · N149SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH CENTER SEAT TRACK AT FR 75, 76, 76.5, 77, 78, 80, 81, 82, 83, 84. (C-CHECK RO 7/12/2023) REMOVED AND REPLACED RH CENTER SEAT TRACK BETWEEN FR 74 -84, REF EMB 175 SRM 51-40-08. PART REPLACED WITH NEW OEM PART. THIS ACTION DOES NOT AFFECT
- [SDR SWIA20230713621](https://openairdocs.org/sdr/SWIA20230713621.md): Unknown · corroded · Jun 21, 2023 · N149SY · Emb ERJ170200LR · Fuselage Structure (General)
  > CORROSION, AFT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LH AND CENTER SHEAR PANELS. (C-CHECK RO 7/12/2023) REMOVED AND REPLACED LH LONGITUDINAL BEAM AT FR 87. REF EMB SRM 51-40-08. THIS REPAIR DOES NOT AFFECT
- [SDR SWIA202306050004](https://openairdocs.org/sdr/SWIA202306050004.md): Unknown · cracked · Jun 4, 2023 · N149SY · Emb ERJ170200LR · Flight Compartment Windows
  > FOS SIDE WINDSHIELD HAS MULTIPLE CRACKS. (FILED CLOSED)REMOVED AND REPLACED FOS SIDE WINDSHIELD IN REFERENCE TO ERJ 175 AMM 56-11-00. TORQUE WRENCH SERIAL NUMBER 0906300068 USED FOR WINDOW TORQUE.PERFORMED WINDSHIELD HEATING SYSTEM OPS CHECK IN REFERENCE TO A
- [SDR SWIA202053227](https://openairdocs.org/sdr/SWIA202053227.md): Web · cracked · Oct 3, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FRAME 52 WEBBING CRACKED BELOW SUPPORT ANGLE IN A RADIUS, AS MARKED. C-CHECK RO 10/12/2020. REMOVED AND REPLACE CRACKED WEB WITH NEW WEB AT FR 52 LT MLG WHEEL WELL, AS REQUIRED REF SRM.
- [SDR SWIA202053223](https://openairdocs.org/sdr/SWIA202053223.md): Beam · corroded · Oct 2, 2020 · N149SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION ON FWD PAX DOOR THRESHOLD BEAM AFT GIRT BAR FITTING CUTOUT. C-CHECK RO 10/12/2020. REMOVED AND REPLACED FWD PAX DOOR THRESHOLD BEAM WITH NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE IN WEIGHT AND BALANCE, REF EMB175 SRM.
- [SDR SWIA202053234](https://openairdocs.org/sdr/SWIA202053234.md): Intercostal · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, INTERCOSTAL AT FR 89-90 Y=11". C-CHECK RO 10/12/2020. REMOVED AND REPLACED INTERCOSTAL AT FR 89-90 Y=11", REF SRM.
- [SDR SWIA202053233](https://openairdocs.org/sdr/SWIA202053233.md): Splice · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, FLOOR SPLICE AT FR 90 Y=11". C-CHECK RO 10/12/2020. REMOVED AND REPLACED FLOOR SPLICE AT FR 90 Y=11", REF SRM.
- [SDR SWIA202053232](https://openairdocs.org/sdr/SWIA202053232.md): Splice · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, FLOOR SPLICE AT FR 90 Y=0. C-CHECK RO 10/12/2020. REMOVED AND REPLACED FLOOR SPLICE AT FR 90 Y=0, REF SRM.
- [SDR SWIA202053231](https://openairdocs.org/sdr/SWIA202053231.md): Splice · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, FLOOR SPLICE AT FR 90 Y= -11". C-CHECK RO 10/12/2020. REMOVED AND REPLACED FLOOR SPLICE AT FR 90 Y= -11". PRE-TREATED BARE METAL AND APPLIED PRIMER, REF SRM PO 256693.
- [SDR SWIA202053230](https://openairdocs.org/sdr/SWIA202053230.md): Splice · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, FLOOR SPLICE AT FR 89 Y=11". C-CHECK RO 10/12/2020. REMOVED AND REPLACED FLOOR SPLICE AT FR 89 Y=11", REF SRM.
- [SDR SWIA202053229](https://openairdocs.org/sdr/SWIA202053229.md): Floor Support · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, LT FLOOR PANEL SUPPORT AT FR 88-90. C-CHECK RO 10/12/2020. REMOVED AND REPLACED LT FLOOR PANEL SUPPORT AT FR 88-90 DUE TO OUT OF LIMITS MATERIAL LOSS, REF SRM.
- [SDR SWIA202053228](https://openairdocs.org/sdr/SWIA202053228.md): Floor Support · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, LT FLOOR SPLICE OUTBOARD OF SHEAR PANEL AT FR 87-88. C-CHECK RO 10/12/2020. REMOVED AND REPLACED LT FLOOR SPLICE OUTBOARD OF SHEAR PANEL AT FR 87-88, REF EMB SRM.
- [SDR SWIA202053222](https://openairdocs.org/sdr/SWIA202053222.md): Floor Support · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, RT CENTER FLOOR BEAM AT FR 87-89. C-CHECK RO 10/12/2020. REMOVED AND REPLACED RT CENTER FLOOR BEAM BETWEEN FRAMES 87-89 WITH NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF SRM.
- [SDR SWIA202053221](https://openairdocs.org/sdr/SWIA202053221.md): Floor Support · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION, LT CENTER FLOOR BEAM AT FR 87-89. C-CHECK RO 10/12/2020. REMOVED AND REPLACED THE LT CENTER FLOOR BEAM AT FRAME 87-89 WITH NEW BEAM FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF EMBS RM.
- [SDR SWIA202053220](https://openairdocs.org/sdr/SWIA202053220.md): Seat Track · corroded · Sep 28, 2020 · N149SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION STRUCTURE CENTER FUSELAGE 1 DRY AREA 53-21 RT SEAT TRACK FRAME 12/20 Y= -10.748" BETWEEN FRAME 12 & 13, 14 &15 AND FRAME17. C-CHECK RO 10/12/2020. REMOVED AND REPLACED RT SEAT TRACK BETWEEN FR 12/20 Y= -10.748" WITH NEW SEAT TRACK FROM FACTORY. NO
- [SDR SWIA202053226](https://openairdocs.org/sdr/SWIA202053226.md): Support Angle · cracked · Sep 27, 2020 · N149SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FR 52 SUPPORT ANGLE IS CRACKED THROUGH THE OUTBOARD FASTENER FWD OF THE LT MLG WHEEL WELL AREA, AS MARKED. C-CHECK RO 10/12/2020. REMOVED AND REPLACED FR 52 CRACKED SUPPORT ANGLE LT MLG WHEEL WELL WITH NEW L-ANGLE, AS REQUIRED REF SRM.
- [SDR SWIA202053225](https://openairdocs.org/sdr/SWIA202053225.md): Floorbeam · cracked · Sep 27, 2020 · N149SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA, FRAME 86 FLOOR BEAM RIGHT SIDE FLOOR SUPPORT IS CRACKED/BROKE OFF, AS MARKED. C-CHECK RO 10/12/2020. REMOVED AND REPLACED FLOOR SUPPORT ON RT FLOOR BEAM AT FR 86, REF SRM.
- [SDR SWIA202053224](https://openairdocs.org/sdr/SWIA202053224.md): Floorbeam · cracked · Sep 27, 2020 · N149SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA, FRAME 86 FLOOR BEAM LEFT SIDE FLOOR SUPPORT IS CRACKED/BROKE OFF, AS MARKED. C-CHECK RO 10/12/2020. REMOVED AND REPLACED FLOOR SUPPORT ON LT FLOOR BEAM AT FR 86, REF 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 = 'N149SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N149SY/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.