# Service difficulty reports: N124SY

A list on [N124SY](https://openairdocs.org/aircraft/N124SY.md).

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

- [SDR SWIA2025102400002](https://openairdocs.org/sdr/SWIA2025102400002.md): Shear Tie · corroded · Oct 2, 2025 · N124SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT WET AREA SHEAR CLIP IS CORRODED AT FRAME 88-89 BETWEEN STRINGERS 20L-21L. (C-CHECK RO 10/23/2025)REMOVED AND REPLACED AFT WET AREA SHEAR CLIP AT FRAME 88-89 BETWEEN STRINGERS 20L-21L REF EMB SRM 51-40-08. REPLACED WITH OEM PART AND DOES NOT EFFECT WEIGHT
- [SDR SWI2025F01458](https://openairdocs.org/sdr/SWI2025F01458.md): Flap Track · out of limits · Oct 1, 2025 · N124SY · Emb ERJ170200LR · Leading Edge Devices
  > RH AFT FLAP TRACK 2A OB HAS A WIDTH REDUCTION OF 1.4 MM THAT IS OUT OF LIMITS (C-CHECK RO 10/23/2025)REMOVED AND REPLACED RH AFT FLAP TRACK 2A OB. REF AMB 175 AMM 57-54-25. ASSET# TC1-604, CDD 3-6-26. TC2-10241, CDD 3-20-26.
- [SDR SWIA202510240001](https://openairdocs.org/sdr/SWIA202510240001.md): Flap Track · out of limits · Oct 1, 2025 · N124SY · Emb ERJ170200LR · Leading Edge Devices
  > RH FLAP TRACK 2 IB MAIN HAS A WIDTH REDUCTION OF 1.06MM THAT IS OUT OF LIMITS (C-CHECK RO 10/23/2025)REMOVED AND REPLACED RH FLAP TRACK 2 IB MAIN. REF AMB 175 AMM 57-54-23. ASSET# TC1-604, CDD 3-6-26. TC2-10241, CDD 3-20-26.
- [SDR SWIA2025102400930](https://openairdocs.org/sdr/SWIA2025102400930.md): Seat Track · gouged · Sep 30, 2025 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > R/H LATERAL SEAT TRACK SEGMENT FR 59/73 IS GOUGED 59/60 AND 60/73.)REMOVED AND REPLACED R/H LATERAL SEAT TRACK SEGMENT BETWEEN FR 59/73. REF: SRM 51-40-08. FACTORY REOLACEMENT PART INSTALLED NO CHANGE TO AIRCRAFT WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR
- [SDR SWI2025F01457](https://openairdocs.org/sdr/SWI2025F01457.md): Seat Track · corroded · Sep 29, 2025 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD FUSELAGE FLOOR STRUCTURE SEAT TRACK, RIGHT UPPER SURFACE HAS CORROSION ON UPPER SURFACE AT FR 16. REPAIRED FORWARD FUSELAGE FLOOR STRUCTURE SEAT TRACK, RIGHT UPPER SURFACE AT FR 16. BY REMOVING DAMAGE AND INSTALLING A FABRICATED FILLER PLUG/DOUBLER RE
- [SDR SWIA2025102400929](https://openairdocs.org/sdr/SWIA2025102400929.md): Floorbeam · corroded · Sep 29, 2025 · N124SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > FORWARD FUSELAGE FLOOR STRUCTURE CROSSBEAM FR 17 CENTER HAS TWO AREAS OF CORROSION ON THE UPPER SURFACE. (C-CHECK RO 10/23/2025)REPAIRED FR17 RH CROSSBEAM REF EMB SRM 53-00-10 REPAIR 03P
- [SDR SWIA2025102400927](https://openairdocs.org/sdr/SWIA2025102400927.md): Rib · cracked · Sep 27, 2025 · N124SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > CRACK LH HORIZONTAL RIB 12 UPPER FWD FLANGE AFT RIVET AND AFT FLANGE FWD RIVET. (C-CHECK RO 10/23/2025)REMOVED AND REPLACED LH HORIZONTAL RIB 12A REF ETD2025-170-929972. REPLACED WITH OEM PART AND THERE IS NO CHANGE TO WEIGHT AND BALANCE,
- [SDR SWIA2025F01339](https://openairdocs.org/sdr/SWIA2025F01339.md): Skin · scratched · Sep 12, 2025 · N124SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > UPON INSPECTION, FOUND THE DAMAGED AREA BETWEEN THE AFT CARGO DOOR AND AFT LAV SERVICE PANEL TO BE 15.5"L X 2.5" W WITH A SCRATCH 1/16" DEEP. DAMAGE IS OUT OF LIMITS PER SRM 53-23-01 (FLIGHT 4653 - FILED CLOSED)TRANSFERED FROM EAML 1702353: REF AML# 1702303
- [SDR SWIA2022120266959](https://openairdocs.org/sdr/SWIA2022120266959.md): Floorbeam · mechanic error · Nov 20, 2022 · N124SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > FWD FUSELAGE R/H CENTER FLOOR BEAM HAS A MISS DRILLED HOLE AT FR 14. WHERE THE LOWER STRAP ATTACHES TO THE BOTTOM OF THE FLOOR BEAM. PERFORMED PERMANENT REPAIR TO FWD FUSELAGE R/H CENTER FLOOR BEAM HAS A MISS DRILLED HOLE AT FR 14 WHERE THE LOWER STRAP ATTACH
- [SDR SWIA2022120266958](https://openairdocs.org/sdr/SWIA2022120266958.md): Beam · corroded · Nov 14, 2022 · N124SY · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT CARGO COMPARTMENT LOWER BEAM HAS CORROSION AT FR77 - FR78. REMOVED AND REPLACED AFT CARGO COMPARTMENT LOWER BEAM IAW SRM 51-40-08.
- [SDR SWIA202266957](https://openairdocs.org/sdr/SWIA202266957.md): Seat Track · gouged · Nov 12, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFTOTBD SEAT TRACK HAD GOUGES AND EXPOSED METAL FROM FR74 TO FR84. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08,. SRM 51-23-04, 51-23-05, 51-23-06 AND CPM 51-25-00-910-001A.
- [SDR SWIA202266956](https://openairdocs.org/sdr/SWIA202266956.md): Seat Track · gouged · Nov 12, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT OTBD SEAT TRACK HAS GOUGES AND EXPOSED METAL FROM FR74 TO FR84. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA202266955](https://openairdocs.org/sdr/SWIA202266955.md): Seat Track · corroded · Nov 12, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RT INBD SEAT TRACK HAS CORROSION AT SEAT MOUNT LUGS AND ON FLOOR OF TRACK, GOUGES, AND EXPOSED METAL FROM FR74 TO FR84. REMOVED AND REPLACED RT INBD SEAT TRACK FROM FR74 TO FR84 REF EMB 175 SRM 51-40-08.
- [SDR SWIA202266954](https://openairdocs.org/sdr/SWIA202266954.md): Seat Track · gouged · Nov 11, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON RT INBOARD SEAT TRACK, BETWEEN FRMS 20-21. REMOVED AND REPLACED RT INBD SEAT TRACK FRMS 12-21 IAW SRM 51-40-08.
- [SDR SWIA202266953](https://openairdocs.org/sdr/SWIA202266953.md): Beam · corroded · Nov 11, 2022 · N124SY · Emb ERJ170200LR · Service Doors
  > AFT SERVICE DOOR BEAM HAS CORROSION. BETWEEN FR.85-86 AT STR. 17R. REMOVED AND REPLACED AFT SERVICE DOOR BEAM BETWEEN FR 85-86 AT STGR 17R. REF SRM 51-40-08.
- [SDR SWIA202266952](https://openairdocs.org/sdr/SWIA202266952.md): Floor Support · corroded · Nov 11, 2022 · N124SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION IN AFT WET AREA, ON CENTER LT FLOOR SUPPORT AT FR 87. REMOVED AND REPLACED CENTER LT FLOOR SUPPORT FRAMES 86-89, IAW SRM 51-40-08. PART REPLACED WITH NEW.
- [SDR SWIA2022120266951](https://openairdocs.org/sdr/SWIA2022120266951.md): Seat Track · gouged · Nov 10, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 11 LOCATIONS. (C-CHECK) REMOVED AND REPLACED RT FLOOR SEAT TRACK BETWEEN FR 23-34 IAW SRM 51-40-08 AND REWORKED SEAT TRACK BEAN BACK TO ORIGINAL CONTOUR IAW ETD2022-170-034585.
- [SDR SWIA2022120266950](https://openairdocs.org/sdr/SWIA2022120266950.md): Seat Track · gouged · Nov 10, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 21-23 IN 2 LOCATIONS. (C-CHECK) PERFORMED PERMENANT REPAIR TO RT FLOOR SEAT TRACK BETWEEN FR 21-23 IN 2 LOCATIONS IAW ETD2022-170-035282.
- [SDR SWIA2022120266949](https://openairdocs.org/sdr/SWIA2022120266949.md): Seat Track · gouged · Nov 10, 2022 · N124SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON L/H O/B FLOOR SEAT TRACK BETWEEN FR 23-34 IN 8 LOCATIONS AS MARKED. (C-CHECK RO) REMOVED AND REPLACED L/H O/B FLOOR SEAT TRACK BETWEEN FR 23-34 REF EMB 175 SRM 51-40-08.
- [SDR SWIA202266948](https://openairdocs.org/sdr/SWIA202266948.md): Waste Box · corroded · Nov 8, 2022 · N124SY · Emb ERJ170200LR · Fuselage Main, Structure
  > WASTE BOX FWD INNER CORNER HAS CORROSION. (C-CHECK RO 12/1/2022) REMOVED AND REPLACED WASTE BOX INNER DOUBLER BETWEEN FRAMES 89-88. / SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 51-40-08 / THIS ACTION DOES NOT EFFECT THE AIRCRAFT WEIGHT AND BALLA
- [SDR SWIA202156723](https://openairdocs.org/sdr/SWIA202156723.md): Skin · damaged · Mar 4, 2021 · N124SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REPORT OF AIRCRAFT MAJOR REPAIR" FOR DAMAGE TO FUSELAGE LOCATED UNDER 3RD PASSANGER WINDOW ON LH STGR 21 & STGR 23 AND FR25 & FR27 FILED CLOSED REVIEWED AND SIGNED FORM M-337
- [SDR SWIA202052765](https://openairdocs.org/sdr/SWIA202052765.md): Latch · broken · Sep 25, 2020 · N124SY · Emb ERJ170200LR · Fixed Inner Doors
  > EMERGENCY GEAR EXTENSION DOOR COVER LATCH BROKEN. FILED CLOSED (9/24/2020). REMOVED AND REPLACED THE EMERGENCY GEAR EXTENSION DOOR, PER AMM. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA2019120646827](https://openairdocs.org/sdr/SWIA2019120646827.md): Floor Support · corroded · Aug 27, 2019 · N124SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA- FR88/FR90 R/H PANEL SUPPORT CORRODED. (C-CHECK) RO 9/11/2019 REMOVED CORROSION ON R/H PANEL SUPPORT IN AFT WET AREA- FR88/FR90. R/H PANEL SUPPORT NOMINAL: 0.050". MAX. MATERIAL REMOVED: 0.018". REMAINING MATERIAL:.032". NON SIGNIFICANT ALLOWABL
- [SDR SWIA2019120646826](https://openairdocs.org/sdr/SWIA2019120646826.md): Shear Panel · corroded · Aug 27, 2019 · N124SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA- FR87/FR88 CENTER SHEAR PANEL CORRODED. (C-CHECK) RO 9/11/2019 REMOVED CORROSION ON CENTER SHEAR PANEL IN AFT WET AREA- FR87/FR88. CENTER SHEAR PANEL NOMINAL: 0.050". MAX. MATERIAL REMOVED: 0.018". REMAINING MATERIAL: 0.032". ALLOWABLE DAMAGE: 0.
- [SDR SWIA2019120646824](https://openairdocs.org/sdr/SWIA2019120646824.md): Floor Support · corroded · Aug 27, 2019 · N124SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CORROSION ON RH FLOOR SILL @ FR.12-14 (C-CHECK) RO 9/11/2019 REMOVED AND REPLACED OUT OF LIMITS RH FLOOR SILL @ FR.12-14. REF SRM. THIS SDR IS BEING REPORTED AS PART OF THE CORRECTIVE ACTION PLAN FOR VDR REGARDING SDRS OVER DUE.
- [SDR SWIA2019120646823](https://openairdocs.org/sdr/SWIA2019120646823.md): Floorbeam · corroded · Aug 27, 2019 · N124SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFT WET AREA- FR88 Y=+273 BEAM CORRODED. (C-CHECK) RO 9/11/2019 REMOVED CORROSION ON FR88 Y=+273 BEAM IN AFT WET AREA. FR88 Y=+273 BEAM CAP NOMINAL: 0.070". MAX. MATERIAL REMOVED: 0.022". REMAINING MATERIAL: 0.048" ALLOWABLE DAMAGE: 0.017". FR88 Y=+273 BEA
- [SDR SWIA2019120646825](https://openairdocs.org/sdr/SWIA2019120646825.md): Beam · corroded · Aug 26, 2019 · N124SY · Emb ERJ170200LR · Fuselage Main, Structure
  > FORWARD CARGO BAY LOWER HORIZONTAL BEAM CLOSEOUT PANEL CORRODED AS MARKED. (C-CHECK) RO 9/11/2019 REMOVED DAMAGE TO LOWER HORIZONTAL BEAM CLOSEOUT PANEL BY BLENDING. NOMINAL THICKNESS IS.047".MAX MATERIAL LOSS IS.008" WITH.039" REMANING AND IS OUT OF LIM
- [SDR SWIA201540600](https://openairdocs.org/sdr/SWIA201540600.md): Potable Water · leaking · Jan 14, 2015 · N124SY · Emb ERJ170200LR · Potable Water System
  > DURING APPROACH, LEFT AILERONS JAMMED. DISCONNECTED THE AILERON CONTROLS AND LANDED WITHOUT INCIDENT, NO EMERGENCY DECLARED. FORWARD POTABLE WATER SYSTEM HAD LEAKED, FLOODING THE BELLY UNDER THE FWD CARGO BAY. THE WATER HAD ENCAPSULATED THE CAPTAIN`S AILERON
- [SDR SWIA201541377](https://openairdocs.org/sdr/SWIA201541377.md): Control Column · failed · Jan 11, 2015 · N124SY · Emb ERJ170200LR · Control Column Section
  > AUTOPILOT KICKED OFFLINE. FOUND THE AILERONS TO BE UNMOVABLE. NO OTHER MESSAGES POSTED. FOLLOWED QRH AND LT AILERON REMAINED UNMOVABLE WHILE RT AILERON MOVED FREELY. CONTINUED TO DESTINATION. CONNECTED THE CONTROL YOKE. R & R THE AILERON FEEL UNIT. ALL

## 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 = 'N124SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N124SY/reports

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