# Service difficulty reports: N119SY

A list on [N119SY](https://openairdocs.org/aircraft/N119SY.md).

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

- [SDR SWI2025F01314](https://openairdocs.org/sdr/SWI2025F01314.md): Seat Track · gouged · Aug 22, 2025 · N119SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH LOWER SEAT TRACK FROM FR 73 TO FR 84 HAS MULTIPLE GOUGES (MARKED) (C-CHECK RO 09/14/2025)REMOVED AND REPLACED LH LOWER SEAT TRACK FROM FR 73 TO FR 84 REF EMB 175 SRM 51-40-08. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRED.
- [SDR SWI2025F01313](https://openairdocs.org/sdr/SWI2025F01313.md): Seat Track · gouged · Aug 22, 2025 · N119SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH LOWER SEAT TRACK FROM FR73 TO FR 84 HAS GOUGES AT MULTIPLE LOCATIONS (MARKED) (C-CHECK RO 09/14/2025)REMOVED AND REPLACED RH LOWER SEAT TRACK FROM FR73 TO FR 84 REF EMB 175 SRM 51-40-08. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION
- [SDR SWIA2025091500822](https://openairdocs.org/sdr/SWIA2025091500822.md): Shear Tie · corroded · Aug 22, 2025 · N119SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION BETWEEN STGR 28R - 27R AND FR 90 (C-CHECK RO 09/14/2025)REMOVED AND REPLACED SHEAR CLIP AT FR 90 STGR 28R-27R REF EMB 175 SRM 51-40-08.THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRED.
- [SDR SWI2025F01319](https://openairdocs.org/sdr/SWI2025F01319.md): Floorbeam · corroded · Aug 21, 2025 · N119SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > RT FLOOR BEAM AT FS 17, Y+23, HAS MULTIPLE AREAS OF CORROSION, MARKED. (C-CHECK RO 09/14/2025)REPAIRED CROSSBEAM AT FR 17 Y+23" REF EMB 175 SRM 53-00-10/REPAIR 03P. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRED.
- [SDR SWI2025F01318](https://openairdocs.org/sdr/SWI2025F01318.md): Skin · corroded · Aug 21, 2025 · N119SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > CORROSION ON INTERNAL SKIN AT STGR 23L-21L FR 88- 89 (C-CHECK RO 09/14/2025)REPAIRED SKIN AT FR 88-89 STGR 21L-23L REF EMB ETD2025-170-926997 REV:/. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. THIS REPAIR IS A TEMP REPAIR AND IS VALID UNTILL AUGUST 21
- [SDR SWI2025F01317](https://openairdocs.org/sdr/SWI2025F01317.md): Floorbeam · corroded · Aug 21, 2025 · N119SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > RH FLOOR BEAM AT FS 14, Y+23, HAS MULTIPLE AREAS OF CORROSION, MARKED. (C-CHECK RO 09/14/2025)REPAIRED CROSSBEAM AT FR 14 Y+23" REF EMB 175 SRM 53-00-10/REPAIR 03P. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRED.
- [SDR SWI2025F01316](https://openairdocs.org/sdr/SWI2025F01316.md): Floor Support · corroded · Aug 21, 2025 · N119SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RH FLOOR SUPPORT AT FS 12-19, Y+10, HAS MULTIPLE AREAS OF CORROSION, MARKED. (C-CHECK RO 09/14/2025)REMOVED AND REPLACED R/H SEAT TRASK AT FR 12-20 Y+10.5" REF EMB 175 SRM 51-40-08. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRED
- [SDR SWI2025F01315](https://openairdocs.org/sdr/SWI2025F01315.md): Floor Support · corroded · Aug 21, 2025 · N119SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT AT FS 20, Y-10, HAS CORROSION, MARKED. (C-CHECK RO 09/14/2025)REPAIRED L/H SEAT TRACK AT FR20 Y-10" REF EMB 175 SRM 53-10-10/REPAIR 01P. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTION REQUIRED.
- [SDR SWIA2025091500821](https://openairdocs.org/sdr/SWIA2025091500821.md): Floor Support · corroded · Aug 21, 2025 · N119SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > LH FLOOR SUPPORT AT FS 13-15, Y-11, HAS MULTIPLE AREAS OF CORROSION, MARKED. (C-CHECK RO 09/14/2025)REPAIRED L/H SEAT TRACK 2EA AREAS BETWEEN FR 13-15 Y-11"REF EMB 175 SRM 53-10-10/REPAIR 03P.THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. NO FURTHER ACTIO
- [SDR SWIA20250820](https://openairdocs.org/sdr/SWIA20250820.md): Stringer · corroded · Aug 20, 2025 · N119SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 23L BETWEEN FR 88 AND FR 89 (C-CHECK RO 09/14/2025)REPAIRED STRINGER AT FR 86-91 STGR 23L REF EMB ETD2025-170-926997 REV:/. THIS REPAIR DOESN'T EFFECT THE WEIGHT AND BALANCE. THIS REPAIR IS A TEMP REPAIR AND IS VALID UNTILL AUGUST 21, 2026.
- [SDR SWIA202266338](https://openairdocs.org/sdr/SWIA202266338.md): None · corroded · Aug 6, 2022 · N119SY · Emb EMB110* · Fuselage Structure (General)
  > AFT WING TO FUSELAGE FAIRING LOWER ATTACH FLANGE SPLICE IS CORRODED. (C-CHECK RO 8/18/2022) / REMOVED AND REPLACEDAFT WING TO FUSELAGE FAIRING LOWER ATTACH FLANGE SPLICE IS CORRODED. REF EMB 170/175 SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE AIRCRAF
- [SDR SWIA202266337](https://openairdocs.org/sdr/SWIA202266337.md): None · corroded · Aug 6, 2022 · N119SY · Emb EMB110* · Fuselage Structure (General)
  > AFT WING TO FUSELAGE FAIRING L/H LOWER ATTACH FLANGE IS CORRODED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED AFT WING TO FUSELAGE FAIRING L/H LOWER ATTACH FLANGE REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS DO
- [SDR SWIA202266336](https://openairdocs.org/sdr/SWIA202266336.md): None · corroded · Aug 6, 2022 · N119SY · Emb EMB110* · Fuselage Structure (General)
  > AFT WING TO FUSELAGE FAIRING R/H LOWER ATTACH FLANGEIS CORRODED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED AFT WING TO FUSELAGE FAIRING R/H LOWER ATTACH FLANGE REF EMB 170/175 SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT WEIGHT AND BALLANCE.
- [SDR SWIA202266335](https://openairdocs.org/sdr/SWIA202266335.md): None · damaged · Aug 4, 2022 · N119SY · Emb EMB110* · Fuselage Main, Frame
  > REAR-FUSELAGE DRAIN-TUBE FAIRING SUPPORTS FOR "MID 2" DRAIN FAIRING NEED REMOVED TO FOM. (C-CHECK RO 8/18/2022) INSTALLED RH REAR FUSELAGE DRAIN TUBE FAIRING SUPPORTS FOR MID 2 DRAIN FAIRING REF SRM 51-40-08
- [SDR SWIA202266334](https://openairdocs.org/sdr/SWIA202266334.md): None · corroded · Aug 1, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1 (EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR83, STGR 29R-28R AS MARKED (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AT FR83 STGR 29R-28R REF SRM 51-40-08. THIS DOES NOT EFFECT THE WEIGHT AND BALANCE OF THE AIRCRAFT. SEE CONTIN
- [SDR SWIA202266333](https://openairdocs.org/sdr/SWIA202266333.md): None · corroded · Aug 1, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1 (EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR82, STGR 29R-28R (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 82 STGR 29R-28R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, AND 51-23-06, CPM 51-25-
- [SDR SWIA202266332](https://openairdocs.org/sdr/SWIA202266332.md): None · corroded · Aug 1, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1 (EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR81 STGR 28R-29R AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED 1 (EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR81 STGR 28R-29R REF EMB 170/175 SRM 51-40-08. THIS ACTION DOES NOT EFFECT
- [SDR SWIA202266331](https://openairdocs.org/sdr/SWIA202266331.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Keel
  > AFT CARGO HAS 1(EACH) CORRODED STGR, AND HARDWARE AT FR76-82, STGR 29RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED STGR 29R FROM 73-84 REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS REPAIR DOES NOT EF
- [SDR SWIA202266330](https://openairdocs.org/sdr/SWIA202266330.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AT FR75, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AT CORRECT LOCATION OG FR 75 STGR 29R-28R REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. T
- [SDR SWIA202266329](https://openairdocs.org/sdr/SWIA202266329.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT WET AREA HAS 1(EACH) CORRODED SHEAR CLIP AT FR87, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED SHEAR CLIP, EVALUATED POSSIBLE CORROSIONAND DETERMINED THAT THERE WAS NO MATERIAL LOSS TO THE DISCREPANT PART. REINSTALLED SHEAR CLIP. REF EMB 170/
- [SDR SWIA202266328](https://openairdocs.org/sdr/SWIA202266328.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AT FR88, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED SHEAR CLIP, EVALUATED POSSIBLE CORROSIONAND DETERMINED THAT THERE WAS NO MATERIAL LOSS TO THE DISCREPANT PART. REINSTALLED SHEAR CLIP. REF EMB 170/175
- [SDR SWIA202266327](https://openairdocs.org/sdr/SWIA202266327.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR81, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP (1) AT AFT CARGO FRAME 81. STGRS 27R. REF SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE WEIGHT AND BALLANCE OF TH
- [SDR SWIA202266326](https://openairdocs.org/sdr/SWIA202266326.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR82, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AT FR82 STGR 27R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 21-23-04, 51-23-05, AND 51-23-06 AND CPM 5
- [SDR SWIA202266325](https://openairdocs.org/sdr/SWIA202266325.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR83, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AT FR83 STGR 28R-27R REF SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS ACTION DOES NOT
- [SDR SWIA202266324](https://openairdocs.org/sdr/SWIA202266324.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR84, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AND HARDWARE AT FR84, STGR 27RH REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS
- [SDR SWIA202266323](https://openairdocs.org/sdr/SWIA202266323.md): None · corroded · Jul 30, 2022 · N119SY · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO HAS 1(EACH) CORRODED SHEAR CLIP AND HARDWARE AT FR85, STGR 27RH AS MARKED. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED SHEAR CLIP AND HARDWARE AT FR85, STGR 27RH REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS
- [SDR SWIA202266343](https://openairdocs.org/sdr/SWIA202266343.md): None · worn · Jul 27, 2022 · N119SY · Emb EMB110* · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #1, 2, & 3 AND IB PCU HARDWARE WORN/CORRODED (C-CHECK RO 8/18/2022) / REMOVED AND REPLACED RH ELEVATOR HINGE #1, 2, & 3 AND IB PCU HARDWARE SEE WP# H8669 CAMP # CP 24946712 FOR FINAL INSTALL
- [SDR SWIA202266342](https://openairdocs.org/sdr/SWIA202266342.md): None · worn · Jul 27, 2022 · N119SY · Emb EMB110* · Elevator Tab, Attach Fittings
  > LH ELEVATOR HINGE #2 & 3 AND IB & OB PCU HARDWARE WORN/CORRODED (C-CHECK RO 8/18/2022) / REMOVED AND REPLACED LH ELEVATOR HINGE #2 & 3 AND IB & OB PCU HARDWARE ON RACK SEE WP# H8669 CAMP# 24946711 FOR FINAL INSTALL
- [SDR SWIA202266341](https://openairdocs.org/sdr/SWIA202266341.md): None · cracked · Jul 27, 2022 · N119SY · Emb EMB110* · Fuselage Structure (General)
  > L/H FRAME 52 L-ANGLE IS CRACKED THROUGH THE FASTENERS FWD OF THE L/H MLG WHEEL WELL. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED L/H FRAME 52 L-ANGLE REF SRM 51-40-08
- [SDR SWIA202266340](https://openairdocs.org/sdr/SWIA202266340.md): None · damaged · Jul 27, 2022 · N119SY · Emb EMB110* · Aileron Tabs
  > LH FLAP TRACK 2A OUTBOARD HAS WIDTH REDUCTION DAMAGE AT FORWARD AND AFT SECTIONS MEASURING 1.2 MM (ASSET TC2-7514, DUE 2-16-23). OUTSIDE OF ALLOWABLE LIMITS. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED LH FLAP TRACK 2A OB AS PER E175 AMM 57-54-25. TW 69
- [SDR SWIA202266339](https://openairdocs.org/sdr/SWIA202266339.md): None · damaged · Jul 27, 2022 · N119SY · Emb EMB110* · Aileron Tabs
  > RH FLAP TRACK 2A OUTBOARD HAS WIDTH REDUCTION DAMAGE AT FORWARD AND AFT SECTIONS MEASURING 1.5 MM. OUTSIDE OF ALLOWABLE LIMITS (ASSET TC2-7514, DUE 2-16-23). (C-CHECK RO 8/18/2022) REPLACED RH FLAP TRACK 2A OUTBOARD. REF ERJ 175 AMM 57-54-25. HG2-694 DA
- [SDR SWIA202266322](https://openairdocs.org/sdr/SWIA202266322.md): None · corroded · Jul 27, 2022 · N119SY · Emb EMB110* · Fuselage Structure (General)
  > 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 8/18/2022) / REMOVED AND REPLACED AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 86 TO FRAME 89, REF SRM
- [SDR SWIA2019082246197](https://openairdocs.org/sdr/SWIA2019082246197.md): Rub Strip · worn · Aug 7, 2019 · N119SY · Emb ERJ170200LR · APU Core Engine
  > APU EXHAUST SILENCER LINER WEAR/RUB STRIP NEAR THE UNFLANGED END IS WORN. (C-CHECK) RO: 08/21/2019 REMOVED AND REPLACED APU EXHAUST LINER IAW AMM.
- [SDR SWIA2019082246198](https://openairdocs.org/sdr/SWIA2019082246198.md): Frame · gouged · Aug 4, 2019 · N119SY · Emb ERJ170200LR · Nacelle/Pylon, Main Frame
  > RH AFT PYLON FAIRING FWD FRAME I/B LUG IS GOUGED. (C-CHECK) RO: 08/21/2019 REMOVED AND REPLACED R/H AFT PYLON FAIRING FWD FRAME1 IAW SRM.
- [SDR SWIA201541370](https://openairdocs.org/sdr/SWIA201541370.md): Battery Pack · inoperative · Jul 21, 2015 · N119SY · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT BATTERY FAULT ADVISORY MESSAGE APPEARS WHEN LIGHTS ARE SELECTED ON. REPLACED LT FORWARD EMERGENCY LIGHT BATTERY. OPS CHECKED GOOD.
- [SDR SWIA2015012740637](https://openairdocs.org/sdr/SWIA2015012740637.md): Smoke Detector · false indication · Jan 22, 2015 · N119SY · Cndair CL6002C10 · Smoke Detection
  > AFTER LEVELING OFF AT FL350, THE CREW RECEIVED A LAVATORY SMOKE WARNING MESSAGE. AFTER 10 SECONDS, THE MESSAGES EXTINGUISHED. HAD THE F/A CHECK THE LAVATORIES FOR FIRE OR SMOKE. NO FAULTS NOTED. MX INSPECTED THE SMOKE DETECTOR SYSTEM. NO FAULTS FOUND. P

## 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 = 'N119SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N119SY/reports

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