# Service difficulty reports: N116SY

A list on [N116SY](https://openairdocs.org/aircraft/N116SY.md).

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

- [SDR SWI2024F01142](https://openairdocs.org/sdr/SWI2024F01142.md): Seat Track · gouged · Sep 26, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H SIDEWALL SEAT TRACK BETWEEN FR 74-84 IN 11 LOCATIONS AS MARKED. (C-CHECK RO 10/16/2024) REMOVED AND REPLACED RH OUTBD LATERAL SEAT TRACK FR 74-84 PER REF EMB SRM 51-40-08. NEW PART INSTALLED IS OEM, NO CHANGES TO WEIGHT AND BALANCE NOTED. SEE
- [SDR SWI2024F01124](https://openairdocs.org/sdr/SWI2024F01124.md): Seat Track · gouged · Sep 26, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 74-84 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED GOUGES FROM THE R/H FLOOR SEAT TRACK BETWEEN FRAME 74-84, IN 10 LOCATIONS, AS MARKED, BY BLENDING. MEASUREMENTS OF THE WORST OUT OF LIMIT
- [SDR SWIA202410160926](https://openairdocs.org/sdr/SWIA202410160926.md): Seat Track · gouged · Sep 26, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR 74-84 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED GOUGES FROM THE R/H FLOOR SEAT TRACK BETWEEN FRAME 74-84, IN 10 LOCATIONS, AS MARKED, BY BLENDING. MEASUREMENTS OF THE WORST OUT OF LIMIT AR
- [SDR SWI2024F01125](https://openairdocs.org/sdr/SWI2024F01125.md): Floorbeam · corroded · Sep 25, 2024 · N116SY · Emb ERJ170200LR · Fuselage Main, Floor Beam
  > CORROSION ON AFT WET AREA LH BEAM AROUND RIVETS AT FR 87 STGR27L/28L (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED AFT WET AREA LH BEAM AT FR 87 STGR27L/28L. REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. OEM PARTS CHANGE, THIS DOES
- [SDR SWIA20240925](https://openairdocs.org/sdr/SWIA20240925.md): Floorbeam · corroded · Sep 25, 2024 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CORROSION ON AFT WET AREA RH BEAM AROUND RIVETS AT FR 87 STGR27R/28R (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED THE AFT WET AREA RH BEAM AT FR 87 STGR27R/28R. REF EMB SRM 51-40-08. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
- [SDR SWIA2024101600925](https://openairdocs.org/sdr/SWIA2024101600925.md): Beam · corroded · Sep 25, 2024 · N116SY · Emb ERJ170200LR · Fuselage Main, Structure
  > CORROSION ON AFT WET AREA RH BEAM AROUND RIVETS AT FR 87 STGR27R/28R (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED AND REPLACED THE AFT WET AREA RH BEAM AT FR 87 STGR27R/28R. REF EMB SRM 51-40-08. OEM PARTS CHANGE, THIS DOES NOT AFFECT WEIGHT AND BALANCE.
- [SDR SWI2024F01127](https://openairdocs.org/sdr/SWI2024F01127.md): Seat Track · gouged · Sep 24, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH IB SEAT TRACK HAS GOUGING FROM FR 23 TO FR 34 (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED RH IB SEAT TRACK FROM FR 23 TO FR 34 IAW REF EMB SRM 51-40-08. PART INSTALLED WAS OEM. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARDS FOR MA
- [SDR SWIA2024110400924](https://openairdocs.org/sdr/SWIA2024110400924.md): Seat Track · corroded · Sep 24, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA RH SEAT TRACK BETWEEN FRAME 17/18 HAS CORROSION AS MARKED (C-CHECK RO 10/16/2024) (FILED CLOSED)REMOVED AND REPLACED FWD WET AREA RH SEAT TRACK BETWEEN FR 12 TO FR 20 IAW REF EMBSRM 51-40-08. PART WAS REPLACED WITH OEM PART, NO CHANGE TO WEIGHT A
- [SDR SWI2024101600020](https://openairdocs.org/sdr/SWI2024101600020.md): Seat Track · gouged · Sep 24, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH IB SEAT TRACK HAS GOUGING FROM FR 23 TO FR 34 (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED AND REPLACED RH IB SEAT TRACK FROM FR 23 TO FR 34 IAW REF EMB SRM 51-40-08. PART INSTALLED WAS OEM. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARDS FOR MAIN
- [SDR SWIA2024101600924](https://openairdocs.org/sdr/SWIA2024101600924.md): Seat Track · corroded · Sep 24, 2024 · N116SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA RH SEAT TRACK BETWEEN FRAME 17/18 HAS CORROSION AS MARKED (C-CHECK RO 10/16/2024) (FILED OPEN)REMOVED AND REPLACED FWD WET AREA RH SEAT TRACK BETWEEN FR 12 TO FR 20 IAW REF EMBSRM 51-40-08. PART WAS REPLACED WITH OEM PART, NO CHANGE TO WEIGHT AND
- [SDR SWIA202407020625](https://openairdocs.org/sdr/SWIA202407020625.md): Control Handle · warning message · Jun 25, 2024 · N116SY · Emb ERJ170200LR · Landing Gear Selector
  > LG LEVER DISAG WARNING MESSAGE AFTER LANDING GEAR RETRACTION ON TAKEOFF. LANDING GEAR SHOWING ALL 3 DOWN WITH THE LEVER IN THE UP POSITION. CYCLED GEAR PER QRH PROCEDURE AND MESSAGE CLEARED AND GEAR CAME UP. (FLIGHT 4723 - FILED CLOSED) THIS DISCREPANCY WAS
- [SDR SWIA2024062600025](https://openairdocs.org/sdr/SWIA2024062600025.md): Landing Gear · warning message · Jun 25, 2024 · N116SY · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > LG LEVER DISAG WARNING MESSAGE AFTER LANDING GEAR RETRACTION ON TAKEOFF. LANDING GEAR SHOWING ALL 3 DOWN WITH THE LEVER IN THE UP POSITION. CYCLED GEAR PER QRH PROCEDURE AND MESSAGE CLEARED AND GEAR CAME UP. (FLIGHT 4723 - FILED OPEN) THIS IS CURRENTLY A WO
- [SDR SWIA202265540](https://openairdocs.org/sdr/SWIA202265540.md): None · damaged · Apr 27, 2022 · N116SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > THE I/B SEAT TRACK AT SEATS 19B & 19C ARE DAMAGED. (FILED CLOSED) REMOVED AND REPLACED THE I/B SEAT TRACK AT SEATS 19B & 19C IN REF TO AMM 25-21-11.
- [SDR SWIA202264213](https://openairdocs.org/sdr/SWIA202264213.md): None · corroded · Feb 1, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > SHEAR CLIP AT FR.83 STR.29R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR.83 STR.29R, REF SRM 51-40-08, CPM 51-25-00-910-001-AWEIGHT AND BALANCE IS NOT AFFECTED WITH INSTALLATION OF N
- [SDR SWIA202264212](https://openairdocs.org/sdr/SWIA202264212.md): None · corroded · Feb 1, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > SHEAR CLIP AT FR.75 STR.29R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 75 STR 29R AS REQUIRED REF SRM 51-40-08. INSTALLATION ODF SHEAR CLIP WITH SAME PART NUBER AS OLD SHEAR CLIP WI
- [SDR SWIA202264211](https://openairdocs.org/sdr/SWIA202264211.md): None · corroded · Feb 1, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > SHEAR CLIP AT FR.74 STR.29R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR74 STR29 REF SRM 51-40-08, NEW SHEAR CLIP WITH ORIGINAL PART NUMBER AS OLD SHEAR CLIP INSTALLED SO WE
- [SDR SWIA202264210](https://openairdocs.org/sdr/SWIA202264210.md): None · corroded · Jan 31, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > SHEAR CLIP AT FR.83 STR.28R FOUND TO HAVE CORROSION HIDDEN BY WASTE CONTAMINATION. (C-CHECK RO 2/11/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR.83 STR.28R, REF SRM 51-40-08, 51-23-05, 51-23-06, CPM 51-25-00-910-001-A.SHEAR CLIP INSTALLATION DOESN'T E
- [SDR SWIA202264209](https://openairdocs.org/sdr/SWIA202264209.md): None · corroded · Jan 23, 2022 · N116SY · Emb ERJ170200LR · Fuselage Structure (General)
  > WASTE SERVICE DOUBLER HAS MULTIPLE AREAS OF CORROSION INCLUDING DETERIORATED FASTENERS BETWEEN FR.88-89 STR. 28R-27R. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED WASTE SERVICE DOUBLER AT FR 88 - FR 89 REF EMB SRM 51-40-08,WEIGHT AND BALANCE WILL NOT BE
- [SDR SWIA202264208](https://openairdocs.org/sdr/SWIA202264208.md): None · corroded · Jan 23, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > CENTER FUSELAGE III FRAME.88 CORRODED AT STR.28R FORWARD OF THE WASTE BOX. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED CENTER FUSELAGE III BOTTOM SECTION OF FRAME 88 REF EMB SRM 51-40-08,INSTALLATION OF ORIGINAL SHEAR CLIP AND NEW FR 88 WITH SAME PART
- [SDR SWIA202264218](https://openairdocs.org/sdr/SWIA202264218.md): None · corroded · Jan 20, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Longeron/Stringer
  > SHEAR CLIP AT FR.85 BETWEEN STR.28R-29R HAS CORROSION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 85 BETWEEN STR 28R-29R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-04, 51-23-05, AND 51-23-06. APPLIED CORROSION INHIBITI
- [SDR SWIA202264207](https://openairdocs.org/sdr/SWIA202264207.md): None · corroded · Jan 20, 2022 · N116SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > L/H SIDE FLOOR SEAT TRACK CORRODED BETWEEN FR76 AND FR77 AS MARKED. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED L/H SIDE FLOOR SEAT TRACK FR74 AND FR84 AS REQUIRED REF SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE
- [SDR SWIA202264206](https://openairdocs.org/sdr/SWIA202264206.md): None · corroded · Jan 20, 2022 · N116SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings
  > R/H SIDE FLOOR SEAT TRACK CORRODED BETWEEN FR78 AND FR79 AS MARKED. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED R/H SIDE FLOOR SEAT TRACK FR74 AND FR84 AS REQUIRED REF SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE
- [SDR SWIA202264205](https://openairdocs.org/sdr/SWIA202264205.md): None · corroded · Jan 20, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > SHEAR CLIP AT FR.88 BETWEEN STR.28R-29R HAS CORROSION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STR 28R-29R REF EMB SRM 51-40-08,INSTALLATION OF SHEAR CLIP DOESN'T EFFECT WEIGHT AND BALANCE
- [SDR SWIA202264204](https://openairdocs.org/sdr/SWIA202264204.md): None · corroded · Jan 20, 2022 · N116SY · Emb ERJ170200LR · Fuselage Main, Frame
  > SHEAR CLIP AT FR.87 BETWEEN STR.28R-29R HAS CORROSION. (C-CHECK RO 2/11/2022) REMOVED AND REPLACED SHEAR CLIP AT FR.87 BETWEEN STR.28R-29R REF EMB SRM 51-40-08INSTALLATION OF NEW SHEAR CLIP DOESN'T EFFECT WEIGHT AND BALANCE.
- [SDR SWIA202264217](https://openairdocs.org/sdr/SWIA202264217.md): None · cracked · Jan 19, 2022 · N116SY · Emb ERJ170200LR · Fuselage, Door Hinge
  > LH FR 52 FORWARD WEBBING ANGLE, AT LOWER SURFACE OF LH WING STUB, IS CRACKED ON THE OB END AS MARKED (C-CHECK RO 2/11/2022) REMOVED AND REPLACED LH FR 52 FORWARD WEBBING ANGLE, AT LOWER SURFACE OF LH WING STUB REF EMB SRM 51-40-08 REFER TO ATTACHED CONT
- [SDR SWIA202264216](https://openairdocs.org/sdr/SWIA202264216.md): None · worn · Jan 18, 2022 · N116SY · Emb ERJ170200LR · Wing, Landing Gear Attach Fittings
  > R/H WING OUTBOARD UPPER FLAP TRACK #3 HAS THICKNESS REDUCTION OF 0.0035" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) BLENDED RH OUTBOARD UPPER #3 FLAP TRACK WITH FLAPS EXTENDED. NOMINAL 39MM. REMOVED.16MM MATERIAL REMAINING 3
- [SDR SWIA202264215](https://openairdocs.org/sdr/SWIA202264215.md): None · worn · Jan 18, 2022 · N116SY · Emb ERJ170200LR · Wing, Landing Gear Attach Fittings
  > R/H WING FLAP TRACK #1A HAS THICKNESS REDUCTION OF 0.010" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) REMOVED AND REPLACED RH WING #1A FLAP TRACK. TW HG4-50097 DUE 6-24-22. REF AMM 57-54-25.
- [SDR SWIA202264214](https://openairdocs.org/sdr/SWIA202264214.md): None · worn · Jan 18, 2022 · N116SY · Emb ERJ170200LR · Wing, Landing Gear Attach Fittings
  > L/H WING FLAP TRACK #1A HAS THICKNESS REDUCTION OF 0.0095" WITH FLAPS EXTENDED. TC2-7153, CAL DUE 11-18-22 (C-CHECK RO 2/11/2022) REMOVED AND REPLACED LH WING FLAP TRACK #1A. TW HG4-50097 DUE 6-24-22. REF AMM 57-54-25.
- [SDR SWIA2019031945649](https://openairdocs.org/sdr/SWIA2019031945649.md): Sensor · dirty · Mar 18, 2019 · N116SY · Emb ERJ170200LR · Air Distribution System
  > FWD EBAY FANS FAIL MESSAGE RECEIVED IN FLIGHT. (FLT#5478) CLOSED CLEANED FAN FWD AVIONICS BAY FLOW SENSOR IAW AMM AND C/W OPERATIONAL CHECK IAW AMM AND FAULT CLEARED. OK TO CONTINUE SERVICE.
- [SDR SWIA2019031545645](https://openairdocs.org/sdr/SWIA2019031545645.md): Bracket · corroded · Feb 27, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD CARGO CUTOUT TRIM RETAINING BRACKET HAS CORROSION NR 5 FROM THE FRONT. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FWD CARGO CUTOUT TRIM RETAINING BRACKET (NR 5 FROM THE FRONT) IAW SRM.
- [SDR SWIA2019031545644](https://openairdocs.org/sdr/SWIA2019031545644.md): Seal Rest · corroded · Feb 24, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FWD CARGO DOOR CUTOUT FWD SEAL REST HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FWD CARGO DOOR CUTOUT SEAL REST IAW SRM.
- [SDR SWIA2019031545643](https://openairdocs.org/sdr/SWIA2019031545643.md): Beam · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT BEAM FR 89-90 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED CORROSION ON RT BEAM FR 89-90 IAW SRM.
- [SDR SWIA2019031545642](https://openairdocs.org/sdr/SWIA2019031545642.md): Beam · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT BEAM FR 86-89 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED AND REPLACED RT BEAM FR 86-89 IAW SRM.
- [SDR SWIA2019031545641](https://openairdocs.org/sdr/SWIA2019031545641.md): Gusset · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOORBEAM GUSSET FR 89 ON LT BEAM HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED AND REPLACED FLOORBEAM GUSSET FR89 ON LT BEAM IAW SRM.
- [SDR SWIA2019031545640](https://openairdocs.org/sdr/SWIA2019031545640.md): Gusset · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOORBEAM GUSSET FR 90 ON RT BEAM HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FLOORBEAM GUSSET FR 90 ON RT BEAM IAW SRM.
- [SDR SWIA2019031545639](https://openairdocs.org/sdr/SWIA2019031545639.md): Gusset · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOORBEAM GUSSET FR 89 ON RT BEAM HAS CORROSION. (C-CHECK) RO: 03/14/2019 INSTALLED NEW FLOORBEAM GUSSET FR 89 ON RT BEAM AND APPLIED TOPCOAT TO FASTENERS IAW SRM.
- [SDR SWIA2019031545638](https://openairdocs.org/sdr/SWIA2019031545638.md): Gusset · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > FLOOR GUSSET FR 90 OTBD OF RT BEAM (AT BASE OF AVIONICS CABINET) HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED FLOOR GUSSET FR90 OUTBD RT BEAM IAW SRM.
- [SDR SWIA2019031545637](https://openairdocs.org/sdr/SWIA2019031545637.md): Floor Support · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT PANEL SUPPORT FR 87-90 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / INSTALLED NEW RT FLOOR SUPPORT (P/N:170-86181-005) AT FR 87-90 IAW SRM.
- [SDR SWIA2019031545636](https://openairdocs.org/sdr/SWIA2019031545636.md): Shear Panel · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > RT SHEAR PANEL FR 87-88 HAS CORROSION. (C-CHECK) RO: 03/14/2019 REMOVED AND REPLACED RT SHEAR PANEL FR 87-88 IAW SRM.
- [SDR SWIA201945635](https://openairdocs.org/sdr/SWIA201945635.md): Shear Panel · corroded · Feb 23, 2019 · N116SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > CENTER SHEAR PANEL FR 87-88 HAS CORROSION. (C-CHECK) RO: 03/14/2019 / REMOVED CORROSION FROM CENTER SHEAR PANEL AT FR 87 -88 IAW SRM.

## 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 = 'N116SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N116SY/reports

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