# Service difficulty reports: N125SY

A list on [N125SY](https://openairdocs.org/aircraft/N125SY.md).

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

- [SDR SWIA2024052100001](https://openairdocs.org/sdr/SWIA2024052100001.md): Fms · out of sequence · May 20, 2024 · N125SY · Emb ERJ170200LR · Flight Management Computing Hardware System
  > FMS WOULD NOT SEQUENCE APPROACH PROPERLY GOING INTO OKC. WOULD ONLY LOAD BACK COURSE, TRIED MULTIPLE TIMES WITH MULTIPLE APPROACHES AND FMS WOULD ONLY LOAD BACK COURSE WHEN APPROACH WAS ARMED. DIVERTED BACK TO DIRECT TO DFW AND ARMED LNAV ABOUT 30MILES AWAY AN
- [SDR SWIA20230530028](https://openairdocs.org/sdr/SWIA20230530028.md): Unknown · missing · May 28, 2023 · N125SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK AT SEAT 2A IS MISSING. (FILED CLOSED)REPLACED THE MISSING SEAT TRACK AT SEAT 2A IN REF TO AMM 25-21-11
- [SDR SWIA2023012367161](https://openairdocs.org/sdr/SWIA2023012367161.md): Actuator · failed · Jan 20, 2023 · N125SY · Emb ERJ170200LR · Leading Edge Slat Actuator
  > SLAT FAIL IN FLIGHT, ARRIVED AT AIRCRAFT AND ATTEMPTED TO OPS CHECK SLAT SYSTEM. SLATS WOULD NOT MOVE. INTERROGATED MDC AND FOUND MULTIPLE INSTANCES OF FSACE 2 WRG FAULTS. REMOVED AND REPLACED FSACE 2 PER E175 AMM 27-53-02-000-801-A AND 27-53-02-400-801-A.
- [SDR SWIA202266710](https://openairdocs.org/sdr/SWIA202266710.md): Beam · corroded · Oct 18, 2022 · N125SY · Emb ERJ170200LR · Fuselage Main, Structure
  > AFT CARGO DOOR CUTOUT LOWER BEAM HAS CORROSION AT FR 77/78 JUST BELOW THE FWD LATCH FITTING MOUNT AREA. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED AFT CARGO DOOR CUTOUT LOWER BEAM, REF EMB175 SRM 51-40-08. PART REPLACED WITH NEW OEM PART, NO WEIGHT
- [SDR SWIA202266709](https://openairdocs.org/sdr/SWIA202266709.md): Shear Tie · corroded · Oct 17, 2022 · N125SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA BELOW FLOOR STRUCTURE ON SHEAR CLIP AT FR 84 BETWEEN STRINGERS 27R-28R. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 84 STR 27R - 28R REF EMB 175 SRM 51-40-08. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT WEIGHT AND
- [SDR SWIA202266708](https://openairdocs.org/sdr/SWIA202266708.md): Shear Tie · corroded · Oct 17, 2022 · N125SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION, AFT WET AREA BELOW FLOOR STRUCTURE ON SHEAR CLIP AT FR 85 BETWEEN STRINGERS 27R-28R. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 85, BETWEEN STGR 27-28R.REF SRM 51-40-08. NO WEIGHT CHANGE REPLACED WITH PMA PART.
- [SDR SWIA202266707](https://openairdocs.org/sdr/SWIA202266707.md): Seat Track · gouged · Oct 13, 2022 · N125SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > CF III L/H INBOARD SEAT TRACK HAS MULTIPLE GOUGES FROM FWD OF FR74 TO FR 81 AS MARKED (C-CHECK RO 10/31/2022) PERFORMED SPLICE REPAIR TO CF III LH INBOARD SEAT TRACK FR 81-85 ON LH IB SEAT TRACK REF ETD2022-170-031776 REV B. THIS REPAIR DOES NOT EFFECT
- [SDR SWIA202266721](https://openairdocs.org/sdr/SWIA202266721.md): Flap Track · damaged · Oct 12, 2022 · N125SY · Emb ERJ170200LR · Trailing Edge Flaps
  > LH WING FLAP TRACK 1A HAS DEPTH REDUCTION DAMAGE MEASURING.033". REQUIRES 200 FC REINSPECT IF NOT REPLACED, REF EMB175 SRM 57-52-03/AD01 TABLE 101. ASSET: TC2-7153 CAL DUE: 11-18-22. (C-CHECK RO 10/31/2022) / REPLACED LH WING FLAP TRACK 1A. REF ERJ 17
- [SDR SWIA202266720](https://openairdocs.org/sdr/SWIA202266720.md): Flap Track · damaged · Oct 12, 2022 · N125SY · Emb ERJ170200LR · Trailing Edge Flaps
  > LH WING FLAP TRACK 2A HAS WIDTH REDUCTION DAMAGE TO THE OUTBOARD SIDE RAIL WITH THE FLAPS EXTENDED AND RETRACTED THAT IS OUT OF LIMITS. MAX DEPTH OF DAMAGE IS.01.043". ASSET# TC2-8909 CAL DUE: 12-7-22. (C-CHECK RO 10/31/2022) / REPLACED LH WING FLAP T
- [SDR SWIA202266719](https://openairdocs.org/sdr/SWIA202266719.md): Pcu · scored · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Elevator Structure
  > RH ELEVATOR INBD AND OTBD PCU HARDWARE IS SCORED. (C-CHECK) REPLACED RH ELEVATOR INBD AND OTBD PCU HARDWARE ON RACK. REF CAMP #25527485 FOR INSTALL.
- [SDR SWIA202266718](https://openairdocs.org/sdr/SWIA202266718.md): Hinge · scored · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Elevator Structure
  > RH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE IS SCORED. (C-CHECK RO 10/31/2022) / REPLACED RH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE ON RACK. REF CAMP #25527485 FOR INSTALL.
- [SDR SWIA202266717](https://openairdocs.org/sdr/SWIA202266717.md): Pcu · scored · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Elevator Structure
  > LH ELEVATOR INBD AND OTBD PCU HARDWARE IS SCORED. (C-CHECK RO 10/31/2022) / REPLACED LH ELEVATOR INBD AND OTBD PCU HARDWARE ON RACK. REF CAMP #25574992 FOR INSTALL.
- [SDR SWIA202266716](https://openairdocs.org/sdr/SWIA202266716.md): Hinge · scored · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Elevator Structure
  > LH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE IS SCORED. (C-CHECK RO 10/31/2022) / REPLACED LH ELEVATOR HINGE 2, AND HINGE 3 HARDWARE ON RACK. REF CAMP #25574992 FOR INSTALL.
- [SDR SWIA202266706](https://openairdocs.org/sdr/SWIA202266706.md): Shear Tie · corroded · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT WET AREA HAS 1(EACH) CORRODED SHEAR CLIP AT FR 88, STGR 27R-28R. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 88, STGR 27-28R. REF SRM 51-40-08. DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT.
- [SDR SWIA202266705](https://openairdocs.org/sdr/SWIA202266705.md): Shear Tie · corroded · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > AFT WET AREA HAS 1(EACH) CORRODED SHEAR CLIP AT FR 87, STGR 27R-28R. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 87, STGR 27-28R. REF SRM 51-40-08. DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT.
- [SDR SWIA202266704](https://openairdocs.org/sdr/SWIA202266704.md): Intercostal · corroded · Oct 11, 2022 · N125SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > AFT WET AREA FR 86-87, STGR 27R-28R HAS 1(EACH) CORRODED INTERCOSTAL FWD OF AFT HOT DRAIN MAST. (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED INTERCOSTAL BETWEEN FR 86-87, STGR 27-28R. REF SRM 51-40-08. DOES NOT EFFECT WEIGHT AND BALANCE OF AIRCRAFT.
- [SDR SWIA202266715](https://openairdocs.org/sdr/SWIA202266715.md): Rod · gouged · Oct 10, 2022 · N125SY · Emb ERJ170200LR · Fuselage Main, Structure
  > PILOT DV WINDOW LOWER ROD IS GOUGED. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED PIOT DV WINDOW LOWER ROD. ADJUSTMENT CHECK GOOD. REF EMB 175 AMM 56-12-00.
- [SDR SWIA202266703](https://openairdocs.org/sdr/SWIA202266703.md): Seat Track · gouged · Oct 10, 2022 · N125SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH OB SEAT TRACK IS GOUGED AT FR 23-34. SEE CONTINUATION. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED R/H O/B SEAT TRACK FR 23 - 34 REF EMB 175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT'
- [SDR SWIA202266702](https://openairdocs.org/sdr/SWIA202266702.md): Seat Track · gouged · Oct 10, 2022 · N125SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH OB SEAT TRACK IS GOUGED AT FR 23-34. SEE CONTINUATION. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED L/H O/B SEAT TRACK FR 23 - 34 REF EMB 175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. THIS REPAIR DOES NOT EFFECT THE AIRCRAFT'
- [SDR SWIA202266701](https://openairdocs.org/sdr/SWIA202266701.md): Seat Track · gouged · Oct 10, 2022 · N125SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH OB SEAT TRACK IS GOUGED AT FR 20/21. (C-CHECK RO 10/31/2022) REMOVED AND REPLACED RH OB SEAT TRACK AT FR 20/21. REF EMB SRM 51-40-08. PART REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
- [SDR SWIA202266700](https://openairdocs.org/sdr/SWIA202266700.md): Seat Track · gouged · Oct 10, 2022 · N125SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > LH OB SEAT TRACK IS GOUGED AT FR 20/21. (C-CHECK) REMOVED AND REPLACED L/H O/B SEAT TRACK FR20/21. REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED. THIS ACTION DOES NOT EFFECT THE SIRCRAFTS WEIGHT AND BALLANCE.
- [SDR SWIA202266714](https://openairdocs.org/sdr/SWIA202266714.md): Bracket · damaged · Oct 8, 2022 · N125SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > R/H AFT WINDSCREEN UPPER OTBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED R/H AFT WINDSCREEN UPPER OTBD SHUTE BOLT BRACKET AT FRAME 84 HOLE REF EMB SRM 51-40-08 AND RETORED SURFACE PROTECTION REF SRM 51-
- [SDR SWIA202266713](https://openairdocs.org/sdr/SWIA202266713.md): Brace · damaged · Oct 8, 2022 · N125SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > R/H AFT WINDSCREEN UPPER INBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED RH AFT WINDSCREEN GROMMET AT FRME 84 PER ETD2022-170-032175. THIS TEMPORARY REPAIR IS VALID FOR 7500FC AS OF OCTOBER 20, 2022.
- [SDR SWIA202266712](https://openairdocs.org/sdr/SWIA202266712.md): Brace · elongated · Oct 8, 2022 · N125SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > L/H AFT WINDSCREEN UPPER OTBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED LH AFT WINDSCREEN UPPER OUTBD SHUTE BOLT BRACKET AT FRAME 84 REF SRM 51-40-08. APPLIED SURFACE PROTECTION AND CIC PROTECTION REF
- [SDR SWIA202266711](https://openairdocs.org/sdr/SWIA202266711.md): Bracket · damaged · Oct 8, 2022 · N125SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings
  > L/H AFT WINDSCREEN UPPER INBD SHUTE BOLT BRACKET AT FRAME 84 HOLE ELONGATED (C-CHECK RO 10/31/2022) / REMOVED AND REPLACED L/H AFT WINDSCREEN UPPER INBD SHUTE BOLT BRACKET AT FRAME 84 REF EMB SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF SRM 51-23-0
- [SDR SWIA2019120646828](https://openairdocs.org/sdr/SWIA2019120646828.md): Seat Track · out of limits · Oct 3, 2019 · N125SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT HAND SEAT TRACK BEAM IN (3 EACH) AREAS AT FRAME 16 NUTPLATE CUTOUT, FORWARD EDGE OF SEAT TRACK, AND ON THE SEAT TRACK AFT EDGE OF BEAM BETWEEN FRAMES 20-23 AS MARKED (C-CHECK) RO 10/14/2019 REMOVED AND REPLACED OUT OF LIMITS RH SEAT TRACK AT FR 12-23, R
- [SDR SWIA201642064](https://openairdocs.org/sdr/SWIA201642064.md): Skin · dented · Apr 12, 2016 · N125SY · Emb ERJ170200LR · Leading Edge Devices
  > BIRDSTRIKE ON RT INBD OF L/E WING BETWEEN FUSELAGE AND RT ENGINE. DENT FOUND ON INBD SLAT L/E SURFACE. PERMANENTLY REPAIRED RT NR 1 SLAT NOSE SKIN BETWEEN TRACK RIB 1 & TRACK RIB 2 IAW SRM.
- [SDR SWIA201541290](https://openairdocs.org/sdr/SWIA201541290.md): Control Valve · failed · Jun 10, 2015 · N125SY · Emb ERJ170200LR · Landing Gear Brake System
  > RIGHT AND LEFT BRAKE FAULT MESSAGES DURING APPROACH, AUTO BRAKE FELL OFFLINE. AFTER LANDING EXCESSIVE BRAKING REQUIRED TO STOP ACFT. REPLACED THE BRAKE CONTROL VALVE. OPS CHECKED GOOD.

## 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 = 'N125SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N125SY/reports

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