# Service difficulty reports: N247SY

A list on [N247SY](https://openairdocs.org/aircraft/N247SY.md).

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

- [SDR SWIA2026050275974](https://openairdocs.org/sdr/SWIA2026050275974.md): Control Lever · warning message · May 2, 2026 · N247SY · Emb ERJ170200LR · Trailing Flap Position Indicating System
  > FLAP FAIL CAUTION MESSAGE, RETURNED TO FIELD QRH DID NOT CLEAR MESSAGE. (FLIGHT 3952) INTERROGATED CMC FOUND FAULT CODE 27512014ACE, TROUBLESHOT PER FIM 27-51-00-810-802-A. DETERMINED LH OUTBOARD FLAP ACTUATOR NUMBER #4 CAUSING FAULT. COMPLIED WITH TASK CARD
- [SDR SWIA20250116221](https://openairdocs.org/sdr/SWIA20250116221.md): Seat Track · gouged · Dec 21, 2024 · N247SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH FLOOR SEAT TRACK 74/84 HAS PAINT DAMAGE OR GOUGES ON OR AFT OF FRAMES 74, 76, 78, 79, 80, 81 AND 83. (C-CHECK RO 1/15/2025) REMOVED AND REPLACED PORTION OF R/H FLOOR SEAT TRACK BETWEEN FR 81-84 REF: ETD2022-170-022163-B
- [SDR SWIA202265375](https://openairdocs.org/sdr/SWIA202265375.md): None · corroded · Apr 10, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CORROSION- FRAME 88 STRINGER 28R SHEAR CLIP CORRODED. (C CHECK RO 4/16/22) REMOVED AND REPLACED SHEAR CLIP AT FR 88 STRINGER 27R-28R REF ERJ 175 SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202265384](https://openairdocs.org/sdr/SWIA202265384.md): None · cracked · Apr 3, 2022 · N247SY · Emb ERJ170200LR · Fuselage Floor Panel
  > FR12 CENTERLINE COCKPIT FLOOR SUPPORT BEAM HAS ATTACH ANGLE CRACKED UNDER CANNON PLUGS AS MARKED (C CHECK RO 4/16/22) / REMOVED AND REPLACED FR12 CENTERLINE COCKPIT FLOOR SUPPORT BEAM ATTACH ANGLE REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-2
- [SDR SWIA202265383](https://openairdocs.org/sdr/SWIA202265383.md): None · cracked · Apr 2, 2022 · N247SY · Emb ERJ170200LR · Fuselage Structure (General)
  > LH MLG - FRAME 52 "L" ANGLE CRACKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED LH MLG - FRAME 52 "L" ANGLE REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06
- [SDR SWIA202265388](https://openairdocs.org/sdr/SWIA202265388.md): None · worn · Apr 1, 2022 · N247SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE FITTING # 2 HARDWARE IS WORN. (C CHECK RO 4/16/22) REMOVED AND REPLACED RH ELEVATOR HINGE FITTING # 2 HARDWARE ON RACK REF: ERJ 175 AMM 27-31-05-01-A
- [SDR SWIA202265387](https://openairdocs.org/sdr/SWIA202265387.md): None · worn · Apr 1, 2022 · N247SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE FITTING # 3 HARDWARE IS WORN. (C CHECK RO 4/16/22) REMOVED AND REPLACED RH ELEVATOR HINGE FITTING # 3 HARDWARE ON RACK REF: ERJ 175 AMM 27-31-05-01-A
- [SDR SWIA202265386](https://openairdocs.org/sdr/SWIA202265386.md): None · worn · Apr 1, 2022 · N247SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR HINGE FITTING # 2 HARDWARE IS WORN. (C CHECK RO 4/16/22) REMOVED AND REPLACED HARDWARE FOR LH ELEVATOR #2 HINGE FITTING REF AMM 27-31-05. REFER TO CP 24530014 FOR FINAL INSTALLATION
- [SDR SWIA202265385](https://openairdocs.org/sdr/SWIA202265385.md): None · worn · Apr 1, 2022 · N247SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR HINGE FITTING # 3 HARDWARE IS WORN. (C CHECK RO 4/16/22) REMOVED AND REPLACED HARDWARE FOR LH ELEVATOR #3 HINGE FITTING REF AMM 27-31-05. REFER TO CP 24530014 FOR FINAL INSTALLATION
- [SDR SWIA202265382](https://openairdocs.org/sdr/SWIA202265382.md): None · corroded · Apr 1, 2022 · N247SY · Emb ERJ170200LR · Fuselage Internal Stairs
  > STILL RIGHT FWD WET AREA FRAME 12-14 TWO AREAS OF CORROISION AS MARKED. (C CHECK RO 4/16/22) CORROSION OUT OF LIMITS REF. EMB SRM 53-10-10/AD06. REMOVED AND REPLACED SILL AT RIGHT FWD WET AREA FRAME 12-14 REF. EMB SRM 51-40-08.
- [SDR SWIA202265376](https://openairdocs.org/sdr/SWIA202265376.md): None · cracked · Apr 1, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CRACKED SHEAR CLIP FRAME 12 @ INTERCOSTAL OTBD OF PILOT OTBD SEAT TRACK (C CHECK RO 4/16/22) REMOVED AND REPLACED SHEAR CLIP FRAME 12 @ INTERCOSTAL OTBD OF PILOT OUTBD SEAT TRACK REF SRM 51-40-08. APPLIED SURFACE PROTECTION REF SRM 51-23-06 AND CIC PROTECT
- [SDR SWIA202265381](https://openairdocs.org/sdr/SWIA202265381.md): None · corroded · Mar 31, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > CENTER SHEAR PANEL AT FR87 /FR88 HAS CORROSION AROUND GALLEY BARREL NUT AS MARKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED CENTER SHEAR PANEL AT FR87 /FR88 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202265380](https://openairdocs.org/sdr/SWIA202265380.md): None · corroded · Mar 31, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > R/H I/B SHEAR PANEL HAS CORROSION AS MARKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED R/H I/B SHEAR PANEL REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202265379](https://openairdocs.org/sdr/SWIA202265379.md): None · corroded · Mar 31, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > R/H I/B SPLICE AT FR89 HAS CORROSION AS MARKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED R/H I/B SPLICE AT FR89 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202265378](https://openairdocs.org/sdr/SWIA202265378.md): None · corroded · Mar 31, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > R/H GUSSET PLATE AT FR90 HAS CORROSION AS MARKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED R/H GUSSET PLATE AT FR90 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202265377](https://openairdocs.org/sdr/SWIA202265377.md): None · corroded · Mar 31, 2022 · N247SY · Emb ERJ170200LR · Fuselage Main, Frame
  > R/H PANEL SUPPORT AT FR89 TO FR90 HAS CORROSION AS MARKED. (C CHECK RO 4/16/22) REMOVED AND REPLACED R/H PANEL SUPPORT AT FR89 TO FR90 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2020090852312](https://openairdocs.org/sdr/SWIA2020090852312.md): Skin · damaged · Aug 22, 2020 · N247SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REFERENCE CAMP 21414889 FOR ORIGINAL DISCREPANCY OF OUT OF LIMITS THROUGH DAMAGE TO LEFT AFT FUSELAGE, LOCATED BETWEEN FRAMES 83 AND 85 AND STRINGERS 19 AND 20. PERFORM DAMAGE REMOVAL AND CUTOUT FOR ETD SUBMISSION PER MANUFACTURERS INSTRUCTIONS FOR PREPARATIO
- [SDR SWIA2020090852311](https://openairdocs.org/sdr/SWIA2020090852311.md): Skin · damaged · Aug 21, 2020 · N247SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > REFERENCE CAMPS 21404308 AND 21414879. OUT OF LIMITS THROUGH DAMAGE TO LEFT AFT FUSELAGE, LOCATED BETWEEN FRAMES 83 AND 85 AND STRINGERS 19 AND 20. MEASURES 18 1/2 INCHES LONG AND 5 INCHES WIDE WITH A GOUGE MEASURING 4 3/4 LENGTH 0.025 DEEP AND 0.25 WIDE. R

## 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 = 'N247SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N247SY/reports

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