# Service difficulty reports: N108SY

A list on [N108SY](https://openairdocs.org/aircraft/N108SY.md).

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

- [SDR SWIA20241017926](https://openairdocs.org/sdr/SWIA20241017926.md): Shear Panel · damaged · Sep 26, 2024 · N108SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > ELONGATED HOLE FOUND AFTER REMOVAL OF PANEL R/H END OF FR88 FOR R/H SHEAR PANEL ATTACHMENT (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED ELONGATED HOLE BY DRILLING TO SPECIFIC DIAMETER TO REMOVE DAMAGE. INSTALLED BUSHING.SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWI2024F01126](https://openairdocs.org/sdr/SWI2024F01126.md): Floorbeam · corroded · Sep 25, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED CLOSED)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 RE
- [SDR SWIA20241017925](https://openairdocs.org/sdr/SWIA20241017925.md): Beam · corroded · Sep 25, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > AFTER REMOVAL OF R/H INBOARD BEAM FR12-20 FOUND CORROSION AT FR17 CROSSBEAM (C-CHECK RO 10/15/2024) (FILED OPEN)WEIGHT OF FR 17 CROSSBEAM REPAIR PARTS AND FASTENERS MEASURE 253.5 G. (TOOLING I.D# HG3-61241 DUE: 08/21/25) PERFORMED CROSSBEAM REPAIR AT FR17 REF:
- [SDR SWI2024F01130](https://openairdocs.org/sdr/SWI2024F01130.md): Beam · corroded · Sep 24, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED
- [SDR SWI2024F01129](https://openairdocs.org/sdr/SWI2024F01129.md): Beam · corroded · Sep 24, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND FR 18. REF SRM 53-10-10/REPAIR 01. REMOVED DAMAGE ON THE L/H I/B BEAM BETWEEN FR 19-20 BY BLENDI
- [SDR SWI2024F01128](https://openairdocs.org/sdr/SWI2024F01128.md): Beam · corroded · Sep 24, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
- [SDR SWIA20241017024](https://openairdocs.org/sdr/SWIA20241017024.md): Beam · corroded · Sep 24, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN R/H BEAM AT FR.87. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H BEAM AT FR.87. REF EMB SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED
- [SDR SWIA20241017023](https://openairdocs.org/sdr/SWIA20241017023.md): Beam · corroded · Sep 24, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN L/H I/B BEAM FR.17-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED DAMAGE ON L/H I/B BEAM BY PERFORMING A CENTER BEAM UPPER CAP REPAIR AT FR 17 AND FR 18. REF SRM 53-10-10/REPAIR 01. REMOVED DAMAGE ON THE L/H I/B BEAM BETWEEN FR 19-20 BY BLENDING
- [SDR SWIA20241017924](https://openairdocs.org/sdr/SWIA20241017924.md): Beam · corroded · Sep 24, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION IN R/H I/B BEAM FR.12-20. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE R/H I/B BEAM FR.12-20. REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.
- [SDR SWI2024F01137](https://openairdocs.org/sdr/SWI2024F01137.md): Seat Track · gouged · Sep 23, 2024 · N108SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED RH IB SEAT TRACK FR 73-FR 84 REF SRM 51-40-08. OEM PARTS CHANGE - WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWI2024F01136](https://openairdocs.org/sdr/SWI2024F01136.md): Seat Track · gouged · Sep 23, 2024 · N108SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
- [SDR SWIA20240923](https://openairdocs.org/sdr/SWIA20240923.md): Seat Track · gouged · Sep 23, 2024 · N108SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 23-34. REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE, THIS DOES
- [SDR SWIA20241017022](https://openairdocs.org/sdr/SWIA20241017022.md): Seat Track · gouged · Sep 23, 2024 · N108SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED RH IB SEAT TRACK FR 73-FR 84 REF SRM 51-40-08. OEM PARTS CHANGE - WEIGHT AND BALANCE NOT AFFECTED.
- [SDR SWIA202410170021](https://openairdocs.org/sdr/SWIA202410170021.md): Seat Track · gouged · Sep 23, 2024 · N108SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LH IB SEAT TRACK HAS GOUGING FROM FR 73 TO FR 84 (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED LH IB SEAT TRACK SEGMENT FR 73 TO FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.
- [SDR SWIA2024101700923](https://openairdocs.org/sdr/SWIA2024101700923.md): Seat Track · gouged · Sep 23, 2024 · N108SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 23-34. REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE, THIS DOES N
- [SDR SWI2024F01141](https://openairdocs.org/sdr/SWI2024F01141.md): Beam · corroded · Sep 22, 2024 · N108SY · Emb ERJ170200LR · Passenger/Crew Doors
  > AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)INSTALLED NEW AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING REF SRM 51-40-08 SEE CONTINUE CARD FOR WORK PERFORME
- [SDR SWIA20240922](https://openairdocs.org/sdr/SWIA20240922.md): Beam · corroded · Sep 22, 2024 · N108SY · Emb ERJ170200LR · Service Doors
  > AFT SERVICE DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED CLOSED)REMOVED AND REPLACED THE AFT SERVICE DOOR LOWER BEAM. REF EMB SRM 51-40-08
- [SDR SWIA202410170025](https://openairdocs.org/sdr/SWIA202410170025.md): Beam · corroded · Sep 22, 2024 · N108SY · Emb ERJ170200LR · Passenger/Crew Doors
  > AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)INSTALLED NEW AFT PAX DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING REF SRM 51-40-08 SEE CONTINUE CARD FOR WORK PERFORMED
- [SDR SWIA202410170922](https://openairdocs.org/sdr/SWIA202410170922.md): Beam · corroded · Sep 22, 2024 · N108SY · Emb ERJ170200LR · Service Doors
  > AFT SERVICE DOOR LOWER BEAM FWD AND AFT EVACUATION SLIDE-FITTING CUTOUTS HAVE CORROSION AS MARKED. (C-CHECK RO 10/15/2024) (FILED OPEN)REMOVED AND REPLACED THE AFT SERVICE DOOR LOWER BEAM. REF EMB SRM 51-40-08
- [SDR SWIA2024110409201](https://openairdocs.org/sdr/SWIA2024110409201.md): Doubler · corroded · Sep 20, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WASTE BOX INTERNAL FLANGE CORRODED ON BOTH SIDES OF HINGE (C-CHECK RO 10/15/2024) (FILED CLOSED).REMOVED AND REPLACE WASTE BOX INTERNAL DOUBLER AND WASTE BOX DOOR ASSY INCLUDING THE HINGE ASSY. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.
- [SDR SWIA20241017920](https://openairdocs.org/sdr/SWIA20241017920.md): Skin · corroded · Sep 20, 2024 · N108SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WASTE BOX INTERNAL FLANGE CORRODED ON BOTH SIDES OF HINGE (C-CHECK RO 10/15/2024) (FILED OPEN).REMOVED AND REPLACE WASTE BOX INTERNAL DOUBLER AND WASTE BOX DOOR ASSY INCLUDING THE HINGE ASSY. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. O
- [SDR SWIA202264783](https://openairdocs.org/sdr/SWIA202264783.md): None · none · Mar 2, 2022 · N108SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > WARRANTY - RIBS 10A, 11A, AND 12A MISLOCATED DURING DRILL UP OF NEW RIBS (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH HORIZONTAL STABILIZER RIBS 10A, 11A, AND 12A, REF EMB175 SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202264792](https://openairdocs.org/sdr/SWIA202264792.md): None · cracked · Feb 27, 2022 · N108SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT AT R/H FR. 86 CRACKED I/B OF AFT SERVICE DOOR. (C CHECK RO 03/07/2022) REMOVED AND REPLACED FLOOR SUPPORT AT R/H FR. 86 I/B OF AFT SERVICE DOOR AND APPLIED TOPCOAT TO FASTENERS REF SRM 51-40-08 AND 51-23-06
- [SDR SWIA202264791](https://openairdocs.org/sdr/SWIA202264791.md): None · cracked · Feb 27, 2022 · N108SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT AT R/H FR. 85 CRACKED I/B OF AFT SERVICE DOOR. (C CHECK RO 03/07/2022) REMOVED AND REPLACED FLOOR SUPPORT AT R/H FR. 85 I/B OF AFT SERVICE DOOR AND APPLIED TOPCOAT TO FASTENERS REF SRM 51-40-08 AND 51-23-06
- [SDR SWIA202264782](https://openairdocs.org/sdr/SWIA202264782.md): None · none · Feb 26, 2022 · N108SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > LH HORIZONTAL STABILIZER UPPER SKIN MIS-DRILLED HOLE AT RIB 14 FWD END (C CHECK RO 03/07/2022) REPAIRED L/H HORIZONTAL STABILIZER UPPER SKIN AT RIB 14 FWD END. REF ETD2022-170-007380. SEE CONTINUATION FOR WORK PERFORMED.
- [SDR SWIA202264790](https://openairdocs.org/sdr/SWIA202264790.md): None · corroded · Feb 23, 2022 · N108SY · Emb ERJ170200LR · Doors
  > AFT CARGO DOOR AFT DOOR SILL REST ( EXTERNAL SIDE) HAS CORROSION AROUND MULTIPLE NUTPLATES AS MARKED (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT CARGO DOOR SILL REST REF EMB SRM 51-40-08.
- [SDR SWIA202264800](https://openairdocs.org/sdr/SWIA202264800.md): None · damaged · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR HINGE #2 INBOARD BUSHING IS DENTED INTO THE INTERNAL DIAMETER AND WILL NOT ALLOW THE BOLT TO BE INSERTED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH ELEVATOR HINGE #2 INBOARD BUSHING. REF EMB 175 AMM 20-10-08
- [SDR SWIA202264799](https://openairdocs.org/sdr/SWIA202264799.md): None · displaced · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > LH ELEVATOR HINGE FITTING #3 INBOARD HAT BUSHING IS MIGRATED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED LH ELEVATOR HINGE FITTING #3 INBOARD HAT BUSHING AS REQUIRED. REF. EMB 175 AMM 20-10-08
- [SDR SWIA202264798](https://openairdocs.org/sdr/SWIA202264798.md): None · damaged · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #2 HARDWARE STACK UP (BOLT/NUT/BUSHING/WASHERS) WAS FOUND SEIZED AND WERE DAMAGED DURING REMOVAL. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #2 HARDWARE AS REQUIRED ON RACK. REF. EMB 175 AMM 27-31-05. SEE CP 24266583
- [SDR SWIA202264797](https://openairdocs.org/sdr/SWIA202264797.md): None · damaged · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #2 INBOARD BUSHING IS DENTED INTO THE INTERNAL DIAMETER AND WILL NOT ALLOW THE BOLT TO BE INSERTED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #2 INBOARD BUSHING. REF EMB 175 AMM 20-10-08
- [SDR SWIA202264796](https://openairdocs.org/sdr/SWIA202264796.md): None · damaged · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #3 BOLT OUTBOARD HAT BUSHINGS (FLOATING AND PRESSED IN) HAVE DENTS/SCORING DAMAGE. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #3 BOLT OUTBOARD HAT BUSHINGS (FLOATING AND PRESSED IN). REF. EMB 175 AMM 20-10-08
- [SDR SWIA202264795](https://openairdocs.org/sdr/SWIA202264795.md): None · damaged · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Elevator Tab, Attach Fittings
  > RH ELEVATOR HINGE #4 BOLT AND NUT HAVE THREAD DAMAGE/NUT WILL NOT THREAD ONTO BOLT. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH ELEVATOR HINGE #4 BOLT AND NUT ON RACK. REF. EMB 175 AMM 27-31-05 SEE CP 24266583 FOR INSTALLATION.
- [SDR SWIA202264794](https://openairdocs.org/sdr/SWIA202264794.md): None · binds · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Horizontal Stabilizer, Attach Fittings
  > RH HORIZONTAL STABILIZER #2 HINGE BEARING IS BINDING/RATCHETING. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH HORIZONTAL STABILIZER #2 HINGE BEARING, REF. EMB 175 AMM 20-10-08
- [SDR SWIA202264793](https://openairdocs.org/sdr/SWIA202264793.md): None · binds · Feb 17, 2022 · N108SY · Emb ERJ170200LR · Horizontal Stabilizer, Attach Fittings
  > RH HORIZONTAL STABILIZER #3 HINGE BEARING IS BINDING/RATCHETING. (C CHECK RO 03/07/2022) REMOVED AND REPLACED RH HORIZONTAL STABILIZER #3 HINGE BEARING. REF. EMB 175 AMM 20-10-08
- [SDR SWIA202264789](https://openairdocs.org/sdr/SWIA202264789.md): None · cracked · Feb 16, 2022 · N108SY · Emb ERJ170200LR · Fuselage Floor Panel
  > CENTER COCKPIT FLOOR CONSOLE SUPPORT ANGLE IS CRACKED ON THE FORWARD SIDE OF FLOOR BEAM AT FRAME 12. (C CHECK RO 03/07/2022) / REMOVED AND REPLACED CENTER COCKPIT FLOOR CONSOLE SUPPORT ANGLE ON THE FORWARD SIDE OF FRAME 12 REF: EMB SM 51-40-08. SEE CONTI
- [SDR SWIA202264781](https://openairdocs.org/sdr/SWIA202264781.md): None · corroded · Feb 16, 2022 · N108SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > UNDER AFT WET AREA, FWD OF WASTE BOX, SHEAR CLIP CORRODED AT FRAME 88 BETWEEN STRINGERS 23R AND 24R (C CHECK RO 03/07/2022) REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STGR 23R AND 24R REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202264788](https://openairdocs.org/sdr/SWIA202264788.md): None · corroded · Feb 15, 2022 · N108SY · Emb ERJ170200LR · Fuselage Internal Stairs
  > AFT WET AREA, RH SIDE, PANEL, SHEAR CORRODED IN 2 PLACES, 2ND AND 4TH BOLT HOLES FROM RH END (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA, RH SIDE, PANEL, SHEAR REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06
- [SDR SWIA202264787](https://openairdocs.org/sdr/SWIA202264787.md): None · corroded · Feb 15, 2022 · N108SY · Emb ERJ170200LR · Fuselage Internal Stairs
  > AFT WET AREA, RH SIDE, PANEL SUPPORT CORRODED IN 2 PLACES, AFT AND CENTER BOLT HOLES (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA RH SIDE PANEL SUPPORT REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 50-23-05, AND 51-23-06.
- [SDR SWIA202264786](https://openairdocs.org/sdr/SWIA202264786.md): None · corroded · Feb 15, 2022 · N108SY · Emb ERJ170200LR · Fuselage Internal Stairs
  > AFT WET AREA, RH SIDE, GUSSET PLATE CORRODED AT INBOARD BOLT HOLE (C CHECK RO 03/07/2022) REMOVED AND REPLACED AFT WET AREA, RH SIDE, GUSSET PLATE AT FR90 REF EMB SRM 51-40-08 RESTORED SURFACE PROTECTION REF SRM 51-23-06 APPLIED CIC REF CPM 51-25-00
- [SDR SWIA202264785](https://openairdocs.org/sdr/SWIA202264785.md): None · corroded · Feb 14, 2022 · N108SY · Emb ERJ170200LR · Aileron Tabs
  > L/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS CORRODED. (C CHECK RO 03/07/2022) REMOVED AND REPLACED L/H AND R/H WING FLAP TRACK SUPPORT #2, #3, AND #4 FWD ATTACHMENT TO WING FITTING SPRING WASHERS. REF E
- [SDR SWIA202264784](https://openairdocs.org/sdr/SWIA202264784.md): None · damaged · Feb 14, 2022 · N108SY · Emb ERJ170200LR · Aileron Tabs
  > L/H WING #2A O/B FLAP TRACK HAS WIDTH REDUCTION DAMAGE OF.031". (C CHECK RO 03/07/2022) LH WING #2A OB FLAP TRACK OUT OF LIMITS. NOMINAL 1.003" REMOVED.44" REMAINING.959" REF ERJ 175 SRM 57-52-03. TC2-8910 DATE11-23-22. REPLACED LH OB #2A FLAP TRACK. R
- [SDR SWIA202264780](https://openairdocs.org/sdr/SWIA202264780.md): None · worn · Feb 13, 2022 · N108SY · Emb ERJ170200LR · Wing, Nacelle/Pylon Attach Fittings
  > LH SLAT #3 O/B TRACK THICKNESS REDUCTION.41MM OUT OF LIMITS. ASSET TC2-7153 DUE 11/18/22 (C CHECK RO 03/07/2022) / COMPLIED WITH PERMANENT REPAIR PER ETD2022-170-006810 / - DETAILED VISUAL INSPECTION (DET) AT REWORKED AREAS, THRESHOLD OF 7,500 FC, INTE
- [SDR SWIA202264779](https://openairdocs.org/sdr/SWIA202264779.md): None · damaged · Jan 5, 2022 · N108SY · Emb ERJ170200LR · Fuselage Structure (General)
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA47357-ETD2019-170-043590-N108SY-PR - DENT AND SCRATCH DAMAGE TO THE FWD FUSE SKIN BTWN FR10-FR11 AND STR14L-15L. PERFORMED TEMP ACTIONS IN REF TO ETD2019-170-043590, REV:/, DTD 03/29/2019. PERFORM PERM REPAIR PER SRM
- [SDR SWIA202158611](https://openairdocs.org/sdr/SWIA202158611.md): Unknown · odor · Jun 3, 2021 · N108SY · Emb ERJ170200LR · Air Distribution System
  > FUME EVENT DURING CRUISE STRONG SULFUR ACIDIC SMELL. EYES AND THROAT IRRITATION. DID NOT GET TO ISOLATE ANY PACKS OR ENG BLEEDS AND NO APU ON TAXI IN. (FLIGHT 5819 - FILED CLOSED) PERFORMED FIM TASK 21-20-00-810-803-A AND FIM TASK 21-20-00-810-801-A.
- [SDR SWIA2019071246056](https://openairdocs.org/sdr/SWIA2019071246056.md): Line · failed · Jul 11, 2019 · N108SY · Emb ERJ170200LR · Hydraulic System, Main
  > RECEIVED HYDRAULIC 2 LOW PRESSURE AND HYD 2 QTY CAUTION MESSAGES IN FLIGHT. PERFORMED QRH. MESSAGES REMAINED. DIVERTED. LANDING GEAR MANUALLY EXTENDED. LANDING WAS UNEVENTFUL. (FLT#5647) FO: 07/12/2019 CLOSED REMOVED AND REPLACED LEFT #2 HYDRAULIC TRAILING EDG
- [SDR SWIA201540630](https://openairdocs.org/sdr/SWIA201540630.md): Antenna · damaged · Jan 20, 2015 · N108SY · Emb ERJ170200LR · Independent Position Determining System
  > FOUND TCAS ANTENNA DAMAGED. R & R THE BOTTOM OMNI DIRECTIONAL TCAS ANTENNA IAW AMM. 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 = 'N108SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N108SY/reports

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