# Service difficulty reports: N117SY

A list on [N117SY](https://openairdocs.org/aircraft/N117SY.md).

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

- [SDR SWIA2026080676958](https://openairdocs.org/sdr/SWIA2026080676958.md): Seat Track · corroded · Aug 6, 2026 · N117SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FRAMES 17-21, Y + 10 RT SEAT TRACK CORRODED AT MULTIPLE LOCATIONS. R & R THE SEAT TRACK IAW SRM 51-40-08. NO FURTHER ACTION REQUIRED.
- [SDR SWIA2026080676957](https://openairdocs.org/sdr/SWIA2026080676957.md): Seat Track · corroded · Aug 6, 2026 · N117SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA, LT SEAT TRACK AT FR 14-18, Y - 10" CORRODED AT MULTIPLE LOCATIONS. R & R THE FWD WET AREA SEAT TRACK IAW SRM 51-40-08.
- [SDR SWI2025F01075](https://openairdocs.org/sdr/SWI2025F01075.md): Flap Track · out of limits · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Leading Edge Devices
  > RH WING FLAP TRACK 2 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.549INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE RH INBOARD FLAP TRACK #2 O/B REF. AMM 57-54-23. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25,
- [SDR SWI2025F01074](https://openairdocs.org/sdr/SWI2025F01074.md): Flap Track · out of limits · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Leading Edge Devices
  > LH WING FLAP TRACK 2 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.549 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE LH INBOARD FLAP MAIN TRACK #2 O/B REF. AMM 57-54-23. ASSET#: TC1-609 CAL: 03/06/26, ASSET#: TC2-10406 CAL: 06/19
- [SDR SWI2025F01073](https://openairdocs.org/sdr/SWI2025F01073.md): Flap Track · out of limits · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Leading Edge Devices
  > LH WING FLAP TRACK 3 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE LH OUTBOARD FLAP TRACK #3 O/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25,
- [SDR SWI2025F01072](https://openairdocs.org/sdr/SWI2025F01072.md): Flap Track · out of limits · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Leading Edge Devices
  > LH WING FLAP TRACK 3 IB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025) REMOVED AND REPLACED THE LH OUTBOARD FLAP TRACK #3 I/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25
- [SDR SWI2025F01071](https://openairdocs.org/sdr/SWI2025F01071.md): Flap Track · out of limits · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Leading Edge Devices
  > RH WING FLAP TRACK 3 OB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE RH OUTBOARD FLAP TRACK #3 O/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25
- [SDR SWIA2025081200721](https://openairdocs.org/sdr/SWIA2025081200721.md): Flap Track · out of limits · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Aileron Tabs
  > RH WING FLAP TRACK 3 IB HAS DEPTH REDUCTION THAT EXCEEDS 0.578 INCH IN LENGTH AND IS OUT OF LIMITS. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED THE RH OUTBOARD FLAP TRACK #3 I/B REF. AMM 57-57-33. ASSET#: TC1-604 CAL: 03/06/26, ASSET#: TC2-10468 CAL: 10/07/25
- [SDR SWIA2025081100721](https://openairdocs.org/sdr/SWIA2025081100721.md): Seat Track · gouged · Jul 21, 2025 · N117SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN LEFT OUTBOARD SEAT TRACK SECTION 34/43 - 59 HAS GOUGING AT FRS 45, 48, 50, 55, 57 AND 59. (C-CHECK RO 08/09/2025)REMOVED AND REPLACED MAIN CABIN LEFT OUTBOARD (LATERAL) SEAT TRACK SECTION FR43 - 59. REF. EMB SRM 51-40-08. RESTORED SURFACE PROTECTIO
- [SDR SWIA2025081100717](https://openairdocs.org/sdr/SWIA2025081100717.md): Seat Track · gouged · Jul 17, 2025 · N117SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH LATERAL SEAT TRACK HAS MULTIPLE GOUGES AND CORROSION AS MARKED FR 16- FR 20
- [SDR SWIA20240514](https://openairdocs.org/sdr/SWIA20240514.md): Warning Message · multiple fail · May 14, 2024 · N117SY · Emb ERJ170200LR · Central Warning
  > LOSS OF FMS 1 AND 2 ON ARRIVAL. LOSS OF AUTOTHROTTLES. LOSS OF ALL NAVIGATION. LOSS OF ALL FLIGHT PLAN INFO. (FLIGHT 4653 FILED CLOSED)POWERED UP AIRCRAFT AND ALLOWED SYSTEMS TIME TO INITIALIZE. THERE WERE NO CURRENT MESSAGES PERTAINING TO FMS 1, FMS2, AT, IRS
- [SDR SWIA202405150004](https://openairdocs.org/sdr/SWIA202405150004.md): Mau · tripped · May 14, 2024 · N117SY · Emb ERJ170200LR · Flight Management Computing Hardware System
  > LOSS OF FMS 1 AND 2 ON ARRIVAL. LOSS OF AUTOTHROTTLES. LOSS OF ALL NAVIGATION. LOSS OF ALL FLIGHT PLAN INFO. (FLIGHT 4653 FILED OPEN)POWERED UP AIRCRAFT AND ALLOWED SYSTEMS TIME TO INITIALIZE. THERE WERE NO CURRENT MESSAGES PERTAINING TO FMS 1, FMS2, AT, IRS'S
- [SDR SWIA2024012200019](https://openairdocs.org/sdr/SWIA2024012200019.md): Receptacle · sparks · Jan 19, 2024 · N117SY · Emb ERJ170200LR · Electrical Power System
  > RAMP TRIED TO PLUG IN AC POWER AND WE SAW A A FLASH OF LIGHT AND ELECTRICAL SMOKE FILLING THE AIR. WE ALSO HEARD A LOUD SOUND FROM THE PANEL. (FLIGHT 4655 FILED CLOSED)EXTERNAL AC POWER SYSTEM DEFERRAL PREVIOUSLY COMPLIED WITH, PLEASE SEE EAML 1281939 AND 1282
- [SDR SWIA202304240001](https://openairdocs.org/sdr/SWIA202304240001.md): Unknown · warning message · Apr 21, 2023 · N117SY · Emb ERJ170200LR · Pneumatic Distribution System
  > BLEED 1 LEAK IN CRUISE AT FL340. RAN QRH. MESSAGE DID NOT EXTINGUISH; HOWEVER IT FLUCTUATED ON AND OFF THE REMAINDER OF FLIGHT. ASSOCIATED BLEED 2 FAIL CAUTION MESSAGE AFTER QRH ACCOMPLISHED. (FLT 5401 FILED CLOSED)TROUBLESHOOT THE BLEED 1 LEAK CAUTION MESSAGE
- [SDR SWIA202265937](https://openairdocs.org/sdr/SWIA202265937.md): None · corroded · May 23, 2022 · N117SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > CORROSION, ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85. (C-CHECK RO 6/14/2022) PERFORMED SPICE ON END OF RH INBOARD SEAT TRACK BETWEEN FRAME 84 AND 85 REF ETD2022-170-018629. SEE CONTINUATION CARD FOR WORK PERFORMED. REPAIR PART WEIGHT: 222.
- [SDR SWIA202265936](https://openairdocs.org/sdr/SWIA202265936.md): None · corroded · May 23, 2022 · N117SY · Emb EMB110* · Fuselage Internal Mounting 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 6/14/2022) REMOVED AND REPLACED AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 REF SRM 51-40-08. RESTO
- [SDR SWIA202265935](https://openairdocs.org/sdr/SWIA202265935.md): None · corroded · May 22, 2022 · N117SY · Emb EMB110* · Fuselage Main, Frame
  > CORROSION AROUND SCREW HOLE L/H TRACK AT FR 19 (C-CHECK RO 6/14/2022) REMOVED CORROSION FROM AROUND SCREW HOLE L/H TRACK AT FR 19 BY CUTOUT, FILLER AND DOUBLER FABRICATION AND INSTALLATION REF SRM 53-10-10/REPAIR01P. REFERENCE CARD FOR WORK PERFORMED. R
- [SDR SWIA202265934](https://openairdocs.org/sdr/SWIA202265934.md): None · corroded · May 22, 2022 · N117SY · Emb EMB110* · Fuselage Main, Frame
  > CROSS BEAM CORRODED FR 17 CENTER BETWEEN L/H AND R/H TRACK BEAMS (C-CHECK RO 6/14/2022) REMOVED CORROSION ON FR 17 CROSS BEAM BETWEEN L/H AND R/H TRACK BEAMS BY PERFORMING CUTOUT, FILLER AND DOUBLER INSTALLATION REF SRM 53-00-10/REPAIR03P. REPAIR DOUBLE
- [SDR SWIA202265933](https://openairdocs.org/sdr/SWIA202265933.md): None · corroded · May 22, 2022 · N117SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > R/H TRACK BEAM CORRODED FWD END OF SEAT TRACK AT FRAME 17 (C-CHECK RO 6/14/2022) REMOVED AND REPLACED R/H SEAT TRACK BEAM FR12-FR20 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202265932](https://openairdocs.org/sdr/SWIA202265932.md): None · corroded · May 20, 2022 · N117SY · Emb EMB110* · Fuselage Main, Frame
  > SHEAR CLIP AT FRAME 88 BETWEEN STRINGERS 26R-27R CORRODED (C-CHECK RO 6/14/2022) REMOVED AND REPLACED SHEAR CLIP FR 88 STRINGER 26R-27R REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. APPLIED C.I.C. REF CPM 51-25-
- [SDR SWIA202265931](https://openairdocs.org/sdr/SWIA202265931.md): None · corroded · May 20, 2022 · N117SY · Emb EMB110* · Fuselage Main, Keel
  > SHEAR CLIP AT FRAME 85 BETWEEN STRINGERS 26R-27R CORRODED (C-CHECK RO 6/14/2022) REMOVED AND REPLACED SHEAR CLIP FR 85 STRINGER 26R-27R REF EMB SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, 51-23-06. APPLIED C.I.C. REF CPM 51-25-
- [SDR SWIA2020070650921](https://openairdocs.org/sdr/SWIA2020070650921.md): Skin · dented · Apr 27, 2020 · N117SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > TWO DENTS FOUND OUT-OF-LIMITS ON THE LEFT SIDE FORWARD FUSELAGE SKIN PANEL LOCATED AT FRAME 11 AND BETWEEN STRINGERS 17L AND 18L. DENT FORWARD OF FRAME 11 MEASURES 3.84"L X 3.18"W X.060"D WITH A CREASE. DENT AFT OF FRAME 11 MEASURES 2.16"L X 1.45"W X.033"D.
- [SDR SWIA2020060550921](https://openairdocs.org/sdr/SWIA2020060550921.md): Skin Panel · dented · Apr 27, 2020 · N117SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > TWO DENTS FOUND OUT-OF-LIMITS ON THE LEFT SIDE FORWARD FUSELAGE SKIN PANEL LOCATED AT FRAME 11 AND BETWEEN STRINGERS 17L AND 18L. DENT FORWARD OF FRAME 11 MEASURES 3.84"L X 3.18"W X.060"D WITH A CREASE. DENT AFT OF FRAME 11 MEASURES 2.16"L X 1.45"W X.033"D.
- [SDR SWIA2019012145457](https://openairdocs.org/sdr/SWIA2019012145457.md): Pressure Switch · failed · Jan 21, 2019 · N117SY · Emb ERJ170200LR · Landing Gear Brake System
  > WHILE IN CRUISE WE RECEIVED A PRKG BRK NOT RELEASED MESSAGE. PERFORMED QRH, MESSAGE DID NOT CLEAR. DECLARED EMERGENCY. (FLT 5996) CLOSED REMOVED AND REPLACED NR 2 PARKING BRAKE PRESSURE SWITCH. OPS CHECK GOOD. NO FURTHER DEFECTS IAW AMM.
- [SDR SWIA201541403](https://openairdocs.org/sdr/SWIA201541403.md): Retainer · damaged · Aug 13, 2015 · N117SY · Emb ERJ170200LR · Passenger/Crew Doors
  > DAMAGE TO PAX DOOR SEAL RETAINERS. REPAIRED THE SEAL RETAINERS.
- [SDR SWIA201541402](https://openairdocs.org/sdr/SWIA201541402.md): Retainer · damaged · Aug 12, 2015 · N117SY · Emb ERJ170200LR · Passenger/Crew Doors
  > DAMAGE TO PAX DOOR. REPAIRED THE DOOR SEAL RETAINERS.
- [SDR SWIA201440011](https://openairdocs.org/sdr/SWIA201440011.md): Battery Pack · failed · Nov 17, 2014 · N117SY · Emb ERJ170200LR · Emergency Lighting
  > CEILING EMERGENCY LIGHT NR 4 NOT WORKING. R & R NR 4 EMERGENCY LIGHT BATTERY PACK IAW AMM.
- [SDR SWIA201439904](https://openairdocs.org/sdr/SWIA201439904.md): Blade · vibration · Nov 10, 2014 · N117SY · Emb ERJ170200LR · Turbine Engine Compressor Section
  > DURING FLIGHT, THE NR 1 ENGINE LOW PRESSURE VIBRATION REACHED 4.0 CAUTION AND FLUCTUATED BETWEEN 3.7 AND 4.0 ENTIRE FLIGHT. DIVERTED, REMOVED NR 1, 25, 26 FAN BLADES PINS OF LT ENGINE AND CLEANED AND INSPECTED AND LUBRICATED IAW AMM. PERFORMED VIBRATION CHEC

## 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 = 'N117SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N117SY/reports

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