# Service difficulty reports: N114SY

A list on [N114SY](https://openairdocs.org/aircraft/N114SY.md).

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

- [SDR SWIA202601080006](https://openairdocs.org/sdr/SWIA202601080006.md): Skin · damaged · Jan 6, 2026 · N114SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING LIGHTNING STRIKE INSPECTION FOUND 1 BURNED RIVET ON FR24 1ST RIVET BELOW STR22L. BURN DAMAGE IS 3/8 L X 3/8 W X 0.073 D AND OUT OF LIMITS PER SRM 53-00-00 REPAIR 03.DAMAGE IS OUT OF LIMITS AND THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR R
- [SDR SWIA2026010700006](https://openairdocs.org/sdr/SWIA2026010700006.md): Skin · damaged · Jan 6, 2026 · N114SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > DURING LIGHTNING STRIKE INSPECTION FOUND 1 BURNED RIVET ON FR24 1ST RIVET BELOW STR22L. BURN DAMAGE IS 3/8 L X 3/8 W X 0.073 D AND OUT OF LIMITS PER SRM 53-00-00 REPAIR 03.DAMAGE IS OUT OF LIMITS AND THE STRUCTURALLY SIGNIFICANT ITEM IS CLISSIFIED AS A MAJOR R
- [SDR SWIA2025122307](https://openairdocs.org/sdr/SWIA2025122307.md): Stay · faulted · Dec 7, 2025 · N114SY · Emb ERJ170200LR · Landing Gear Retraction/Extension System
  > LG LEVER DISAGREE MESSAGE AFTER TAKEOFF AND RETRACTION ATTEMPT.RIGHT MAIN DID NOT RETRACT, COULD HEAR AND FEEL RIGHT MAIN WAS STILL DOWN. QRH PROCEDURE FOLLOWED. GEAR CONFIRMED DOWN AND GREEN AS PER QRH PROCEDURE. (FLIGHT 5367) PERFORMED GEAR SWINGS IAW AMM
- [SDR SWIA2025120800007](https://openairdocs.org/sdr/SWIA2025120800007.md): Warning Message · illuminated · Dec 7, 2025 · N114SY · Emb ERJ170200LR · Landing Gear Selector
  > LG LEVER DISAGREE MESSAGE AFTER TAKEOFF AND RETRACTION ATTEMPT. RIGHT MAIN DID NOT RETRACT, COULD HEAR AND FEEL RIGHT MAIN WAS STILL DOWN. QRH PROCEDURE FOLLOWED. GEAR CONFIRMED DOWN AND GREEN AS PER QRH PROCEDURE. (FLIGHT 5367 - OPEN
- [SDR SWIA20250303206](https://openairdocs.org/sdr/SWIA20250303206.md): Seat Track · gouged · Feb 6, 2025 · N114SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RH I/B SEAT TRACK GOUGED AT FRAMES 46, 48, 50, 53, 55 AS MARKED (C-CHECK RO 3/1/2025) REMOVED AND REPLACED RH I/B SEAT TRACK FR43-59 REF. EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.O.E.M. PART INSTALLED NO CHANGE TO WEIGHT AND BALANCEAVI
- [SDR SWI2025F00277](https://openairdocs.org/sdr/SWI2025F00277.md): Shear Tie · corroded · Feb 4, 2025 · N114SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR CLIP AT FR88 BETWEEN STGR 28R-27R AS MARKED. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED SHEAR CLIP AT FR88 BETWEEN STGR 28R-27R REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. REPLACED DAMAGED SHEAR CLIP WITH OEM REPL
- [SDR SWIA20250303204](https://openairdocs.org/sdr/SWIA20250303204.md): Beam · corroded · Feb 4, 2025 · N114SY · Emb ERJ170200LR · Passenger/Crew Doors
  > AFT PASSENGER DOOR CUTOUT LOWER BEAM HAS CORROSION AT FWD AND AFT GIRT BAR FLOOR FITTING CUTOUTS AND IN THE CENTER OF THE LOWER BEAM IN THE UPPER SURFACE. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED AFT PAX DOOR LOWER BEAM WITH NEW REF. ERJ175 SRM 51-40-
- [SDR SWI2025F00279](https://openairdocs.org/sdr/SWI2025F00279.md): Seat Track · corroded · Feb 3, 2025 · N114SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA RIGHT INBOARD SEAT TRACK HAS CORROSION AT FR 17, 18, 18/19, 19. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED RH INBOARD SEAT TRACK FR 12-20, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. SEE CONTINUA
- [SDR SWI2025F00278](https://openairdocs.org/sdr/SWI2025F00278.md): Beam · corroded · Feb 3, 2025 · N114SY · Emb ERJ170200LR · Passenger/Crew Doors
  > FWD PAX DOOR LOWER BEAM HAS CORROSION AS MARKED BETWEEN FR 16/17 (C-CHECK RO 3/1/2025) REMOVED AND REPLACED THE FWD PAX DOOR LOWER BEAM. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. WEIGHT AND BALANCE WERE NOT EFFECTED BY THIS WORK O.
- [SDR SWIA20250303203](https://openairdocs.org/sdr/SWIA20250303203.md): Beam · corroded · Feb 3, 2025 · N114SY · Emb ERJ170200LR · Service Doors
  > FWD SERVICE DOOR LOWER BEAM HAS CORROSION AT (3) LOCATIONS AS MARKED BETWEEN FR 16/17 (C-CHECK RO 3/1/2025) REMOVED AND REPALCED THE FWD SERVICE DOOR LOWER BEAM. REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. WEIGHT AND BALANCE WAS NOT
- [SDR SWI2025F00276](https://openairdocs.org/sdr/SWI2025F00276.md): Rib · cracked · Feb 2, 2025 · N114SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > RH H-STAB RIBS 11A AND 12A HAVE SUSPECTED CRACKS AT UPPER ATTACH POINTS. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED RH HSTAB RIB 11A AND 12A WITH NEW REF. ERJ175 SRM 51-40-08, ETD2025-170-902006. REPLACED WITH OEM PART NO CHANGE IN WEIGHT AND BALANCE. S
- [SDR SWIA20250303202](https://openairdocs.org/sdr/SWIA20250303202.md): Rib · cracked · Feb 2, 2025 · N114SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/Rib
  > LH H-STAB RIB 12A HAS A SUSPECTED CRACK AT UPPER ATTACH POINT. (C-CHECK RO 3/1/2025) REMOVED AND REPLACED CRACKED LH HSTAB RIB 12A WITH NEW REF. ETD2025-170-902006, ERJ175 SRM 51-40-08. REPLACED WITH OEM PART, NO CHANGE IN WEIGHT AND BALANCE. SEE CONTIN
- [SDR SWIA20250303201](https://openairdocs.org/sdr/SWIA20250303201.md): Doubler · corroded · Feb 1, 2025 · N114SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > WASTE SERVICE DOOR CUTOUT ON FUSELAGE INTERNAL DOUBLER CORRODED INBOARD OF HINGE POINT (C-CHECK RO 3/1/2025) REMOVED AND REPLACED WASTE SERVICE DOOR CUTOUT ON FUSELAGE INTERNAL DOUBLE REF EMB SRM 51-40-08. REPLACED WITH NEW OEM PART NO CHANGE TO WEIGHT
- [SDR SWI202405200414](https://openairdocs.org/sdr/SWI202405200414.md): Skin · punctured · May 14, 2024 · N114SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > HOLE IN FUSELAGE APPROXIMATELY 1 INCH BY 1 INCH APPROXIMATELY THREE FEET TO THE RIGHT OF MCD APPROXIMATELY ONE FOOT ABOVE FLOOR LEVEL. (FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 28236263 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH PEM
- [SDR SWIA202266608](https://openairdocs.org/sdr/SWIA202266608.md): None · none · Oct 12, 2022 · N114SY · Emb EMB110* · Air Conditioning System
  > D; LEFT PACK FAIL MESSAGE. BURNING SMELL FROM PACK WHEN MX TRIED TO TURN ON. / C; MEL 21-51-0A / CAT: "C" DUE 10/22 / AT GATE READY TO PUSH, STARTED TO SMELL SOMETHING BURNING THEN GOT A PACK 1 FAIL. (FLIGHT #5704 FILED CLOSED) OCT 12, 2022 STATION: ORD
- [SDR SWIA202265953](https://openairdocs.org/sdr/SWIA202265953.md): None · corroded · May 27, 2022 · N114SY · Emb EMB110* · Fuselage Main, Frame
  > CORROSION ON SHEAR CLIP AT FRAME 86, STRINGER 18L. (C-CHECK RO 6/16/2022) REMOVED AND REPLACE SHEAR CLIP AT FRAME 86 STRINGER 18L IAW SRM 51-40-08.RESTORED SURFACE PROTECTION REF SRM 51-23-06. REPLACEMENT WITH OEM PART NO WEIGHT CHANGES. SEE CONTINUATI
- [SDR SWIA202265952](https://openairdocs.org/sdr/SWIA202265952.md): None · corroded · May 27, 2022 · N114SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > RH TRACK HAS CORROSION AT FRAME 16 AS MARKED (C-CHECK RO 6/16/2022) REMOVED CORROSION BY CUTOUT AND APPLIED FILLER REPAIR REF EMB SRM 53-10-10/REPAIR01P. WEIGHT OF REPAIR PARTS: 37.5G. SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA202265951](https://openairdocs.org/sdr/SWIA202265951.md): None · gouged · May 26, 2022 · N114SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > GOUGES ON L/H FLOOR SEAT TRACK BETWEEN FR60-74 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 6/16/2022) REMOVED AND REPLACED L/H FLOOR SEAT TRACK BETWEEN FR60-74 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 / NO WEIGHT CHANGE- REMOVED AND REPL
- [SDR SWIA202265950](https://openairdocs.org/sdr/SWIA202265950.md): None · gouged · May 26, 2022 · N114SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR60-74 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 6/16/2022) REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR60-74 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 / NO WEIGHT CHANGE DUE TO REPLACEME
- [SDR SWIA202265949](https://openairdocs.org/sdr/SWIA202265949.md): None · gouged · May 26, 2022 · N114SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR34-60 IN 15 LOCATIONS AS MARKED. (C-CHECK RO 6/16/2022) REMOVED DAMAGE PORTION OF RH INBD SEAT TRACK FROM FR 34-47. FABRICATED, LOCATED, DRILLED AND INSTALLED NEW PORTION OF RH INBD SEAT TRACK FR 34-47. REF EMB S
- [SDR SWIA202265948](https://openairdocs.org/sdr/SWIA202265948.md): None · corroded · May 26, 2022 · N114SY · Emb EMB110* · Fuselage Main, Frame
  > CORRODED SHEAR CLIP FR88 STGR 28R-29R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED SHEAR CLIP AT FR88 STGR28R-29R IAW SRM 51-40-08. REFERENCE CARD FOR WORK PERFORMED.
- [SDR SWIA202265947](https://openairdocs.org/sdr/SWIA202265947.md): None · corroded · May 26, 2022 · N114SY · Emb EMB110* · Fuselage Main, Frame
  > CORRODED SHEAR CLIP FR88 STGR 28R-27R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACE CORRODED SHEAR CLIP AT FR88 STGR 28R-27R IAW SRM 51-40-08. RESTORED SURFACE PROTECTION IAW SRM 51-23-06. REFERENCE CARD FOR WORK PERFORMED. NO CHANGE TO MRB REQUI
- [SDR SWIA202265946](https://openairdocs.org/sdr/SWIA202265946.md): None · corroded · May 26, 2022 · N114SY · Emb EMB110* · Fuselage Main, Frame
  > CORRODED SHEAR CLIP FR87 STGR 28R-27R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR 87 STGR 28R-27R IAW SRM 51-40-08. REFERENCE CARD FOR WORK PERFORMED.
- [SDR SWIA202265945](https://openairdocs.org/sdr/SWIA202265945.md): None · corroded · May 26, 2022 · N114SY · Emb EMB110* · Fuselage Main, Frame
  > CORRODED SHEAR CLIP FR87 STGR 28R-29R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP AT FR87 STGR 28R-29R IAW SRM 51-40-08. REFERENCE CARD FOR WORK PERFORMED.
- [SDR SWIA202265944](https://openairdocs.org/sdr/SWIA202265944.md): None · corroded · May 26, 2022 · N114SY · Emb EMB110* · Fuselage Main, Frame
  > CORRODED SHEAR CLIP FR85 STGR 28R-27R AS MARKED (C-CHECK RO 6/16/2022) REMOVED AND REPLACED SHEAR CLIP FR 85 STGR 28R-27R REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. RESTORED CIC IAW CPM 51-25-00-910-001-A. SEE CONTINUATION CARD FOR
- [SDR SWIA202265943](https://openairdocs.org/sdr/SWIA202265943.md): None · corroded · May 26, 2022 · N114SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > R/H I/B LONGITUDINAL TOP OF SEAT TRACK BETWEEN FR33-34 HAS CORROSION AS MARKED. (C-CHECK RO 6/16/2022) REMOVED AND REPLACED R/H I/B LONGITUDINAL SEAT TRACK BETWEEN FR 23-34 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06. NO WEIGHT CHANG
- [SDR SWIA202265942](https://openairdocs.org/sdr/SWIA202265942.md): None · corroded · May 24, 2022 · N114SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > RH I/B SEAT TRACK CORRODED BETWEEN FRAMES 81-82 (C-CHECK RO 6/16/2022) REMOVED AND REPLACED RH I/B SEAT TRACK BETWEEN FR74-84 REF EMB SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED. SEE CONTINUATION CARD FOR DETAILS OF W
- [SDR SWIA202155903](https://openairdocs.org/sdr/SWIA202155903.md): Skin · dented · Feb 2, 2021 · N114SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 571985: DENT LEFT SIDE FUSELAGE IN LINE WITH AFT OF CA DV WINDOW BELOW GOLD STRIP IS LOCATED ON THE LH SIDE OF THE FUSELAGE BETWEEN FR10 AND FR11. DAMAGE GOES UP TO STR17. THE LENGTH OF THE DENT IS 3.745". THE / WIDTH OF T
- [SDR SWIA202155902](https://openairdocs.org/sdr/SWIA202155902.md): Skin · dented · Feb 2, 2021 · N114SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin
  > TRANSFER FROM EAML 571986: DENT LEFT SIDE FUSELAGE IN LINE WITH STAR ALLIANCE LOGO BELOW GOLD STRIPE IS A COMBINATION OF 1 DENT, 1 CREASE, AND 2 RAISED AREAS. THE DAMAGE IS LOCATED AT FR12 AND STR18. THE CREASE MEASURES 7.0" IN LENGTH. THE WIDTH OF THE CREAS
- [SDR SWIA201946552](https://openairdocs.org/sdr/SWIA201946552.md): Control Module · malfunctioned · Oct 21, 2019 · N114SY · Emb ERJ170200LR · Steering Unit
  > STEER FAIL CAUTION MESSAGE CAME ON WHEN LOWERING LANDING GEAR. HAD NO NOSE WHEEL STEERING WHILE ON THE GROUND. FLT # 5481 CLOSEDREMOVED AND REPLACED STEERING CONTROL MODULE IAW AMM. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA201844135](https://openairdocs.org/sdr/SWIA201844135.md): Engine · shutdown · Jan 11, 2018 · N114SY · Emb ERJ170200LR · Engine Controls
  > LEFT ENGINE SHUTDOWN INFLIGHT. AT FL380, NO TURBULANCE, CREW THROTTLED THE LEFT ENGINE BACK, ITT SPIKED AND WENT RED. ENGINE ROLLED BACK AND SHUTDOWN. CREW DESCENDED TO FL270 AND THE ENGINE AUTO RELIT. WHILE AT FL100 THE CREW INCREASED POWER SLOWLY AND THE
- [SDR SWIA201439883](https://openairdocs.org/sdr/SWIA201439883.md): Warning Light · false activation · Nov 9, 2014 · N114SY · Emb ERJ170200LR · Trailing Edge Flap Control System
  > DURING GO AROUND WITH FLAP SELECTOR AT 2, RECEIVED FLAP OVERSPEED FOR 5 SECONDS, WHILE ENCOUNTERING INTERMITTENT TURBULANCE. NO FAULTS NOTED. ACFT OK FOR SERVICE IAW AMM.

## 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 = 'N114SY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N114SY/reports

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