# Service difficulty reports: N109SY A list on [N109SY](https://openairdocs.org/aircraft/N109SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2025063000004](https://openairdocs.org/sdr/SWIA2025063000004.md): Flap Track · worn · Jun 4, 2025 · N109SY · Emb ERJ170200LR · Trailing Edge Flaps > L/H #1 AFT FLAP TRACK WORN ON ROLLER MATING FACE. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED L/H #1 INBOARD FLAP AFT TRACK PER E175 AMM 57-54-25 SN:220413BNA1 PN: 170-39060-003. TW: MCN-9506 CAL DUE 9/11/25. SEALANT PO:335504 - [SDR SWIA202506300003](https://openairdocs.org/sdr/SWIA202506300003.md): Seat Track · corroded · Jun 3, 2025 · N109SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > RH SEAT TRACK HAS CORROSION AT FR 13 AND Y = + 276 MM. (C-CHECK RO 06/29/2025)REMOVED AND REPLACED RH SEAT TRACK (PN:170-03263-001 PO#:328229)AT FR 13 AND Y= +276MM PER E-175 SRM 51-40-08. - [SDR SWIA202265920](https://openairdocs.org/sdr/SWIA202265920.md): None · damaged · May 31, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > R/H INBOARD SEAT TRACK BEAM REQUIRES SPLICE REPAIR BETWEEN FR.34-48 DUE TO AVAILABILITY OF SPLICE DEVICE. (C-CHECK RO 6/8/2022) REMOVED AND REPLACED RH INBD SEAT TRACK SPLICE REPAIR AND RESTORED SURFACE PROTECTION PER REF SRM 53-00-10/REPAIR01P. NO SIGN - [SDR SWIA202265919](https://openairdocs.org/sdr/SWIA202265919.md): None · gouged · May 10, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > GOUGES ON R/H FLOOR SEAT TRACK BETWEEN FR23-34 IN 10 LOCATIONS AS MARKED. (C-CHECK RO 6/8/2022) REMOVED AND REPLACED R/H FLOOR SEAT TRACK BETWEEN FR 23-34. REF SRM 51-40-08. RESTORED SURFACE PROTECTION AND CIC PROTECTION. REF SRM 51-23-06 AND CPM 51- - [SDR SWIA202265918](https://openairdocs.org/sdr/SWIA202265918.md): None · gouged · May 10, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > GOUGES ON L/H I/B FLOOR SEAT TRACK BETWEEN FR30-34 IN 5 LOCATIONS AS MARKED. (C-CHECK RO 6/8/2022) REMOVED AND REPLACED L/H I/B FLOOR SEAT TRACK BETWEEN FR23-34 REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED. SE - [SDR SWIA202265917](https://openairdocs.org/sdr/SWIA202265917.md): None · gouged · May 10, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > GOUGES ON R/H SIDEWALL SEAT TRACK BETWEEN FR23-34 IN 11 LOCATIONS AS MARKED. (C-CHECK RO 6/8/2022) REMOVED AND REPLACED DAMAGED R/H SIDEWALL SEAT-TRACK FR23-24 WITH NEW SEAT TRACK AS REQUIRED REF EMB175 SRMÂ 51-40-08. PART REPLACED WITH NEW OEM PART, N - [SDR SWIA202265916](https://openairdocs.org/sdr/SWIA202265916.md): None · gouged · May 10, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > GOUGES ON L/H SIDEWALL SEAT TRACK BETWEEN FR23-34 IN 5 LOCATIONS AS MARKED. (C-CHECK RO 6/8/2022) REMOVED AND REPLACED L/H SIDEWALL SEAT TRACK BETWEEN FR23-34 REF SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED - [SDR SWIA202265915](https://openairdocs.org/sdr/SWIA202265915.md): None · gouged · May 10, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > LH I/B SEAT TRACK FR74/84 GOUGED IN 4 LOCATIONS AS MARKED (C-CHECK RO 6/8/2022) REMOVED AND REPLACED LH I/B SEAT TRACK FR74/84 REF EMB SRM 51-40-08. PART REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED - [SDR SWIA202265914](https://openairdocs.org/sdr/SWIA202265914.md): None · corroded · May 9, 2022 · N109SY · Emb EMB110* · Fuselage Main, Longeron/Stringer > AFT DRAIN MAST AFT INTERCOSTAL CORRODED BETWEEN FR86/87 STR27R/28R (C-CHECK RO 6/8/2022) / REMOVED AND REPLACED AFT DRAIN MAST AFT INTERCOSTAL BETWEEN FR86/87 STRG 27R - 28R REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALA - [SDR SWIA202265913](https://openairdocs.org/sdr/SWIA202265913.md): None · corroded · May 9, 2022 · N109SY · Emb EMB110* · Fuselage Main, Frame > CORRODED SHEAR CLIP AT FR88 STR27R/28R (C-CHECK RO 6/8/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 88 STRG 27R - 28R REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202265912](https://openairdocs.org/sdr/SWIA202265912.md): None · corroded · May 9, 2022 · N109SY · Emb EMB110* · Fuselage Main, Frame > CORRODED SHEAR CLIP AT FR87 STR27R/28R (C-CHECK RO 6/8/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 87 STRG 27R - 28R REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202265911](https://openairdocs.org/sdr/SWIA202265911.md): None · corroded · May 9, 2022 · N109SY · Emb EMB110* · Fuselage Main, Frame > CORRODED SHEAR CLIP AT FR86 STR27R/28R (C-CHECK RO 6/8/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 86 STRG 27R - 28R REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202265910](https://openairdocs.org/sdr/SWIA202265910.md): None · corroded · May 9, 2022 · N109SY · Emb EMB110* · Fuselage Main, Frame > CORRODED SHEAR CLIP AT FR85 STR27R/28R (C-CHECK RO 6/8/2022) / REMOVED AND REPLACED SHEAR CLIP AT FR 85 STRG 27R - 28R REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202265909](https://openairdocs.org/sdr/SWIA202265909.md): None · gouged · May 9, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > GOUGES ON L/H SEAT TRACK BETWEEN FR 60-74 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 6/8/2022) REMOVED AND REPLACE SEAT TRACK BEAM BETWEEN FR 60-74 REF EMB 170/175 SRM 51-40-08. REF CONTINUATION CARD FOR CORRECTIVE ACTION DETAILS. PART WAS REPLACED WITH OEM - [SDR SWIA202265908](https://openairdocs.org/sdr/SWIA202265908.md): None · gouged · May 9, 2022 · N109SY · Emb EMB110* · Fuselage, Powerplant Attach Fittings > GOUGES ON L/H SEAT TRACK BETWEEN FR 34-60 IN 15 LOCATIONS AS MARKED. (C-CHECK RO 6/8/2022) REMOVED AND REPLACED L/H SEAT TRACK BETWEEN FR 34-60, REF SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED - [SDR SWIA202265907](https://openairdocs.org/sdr/SWIA202265907.md): None · dented · May 6, 2022 · N109SY · Emb EMB110* · Fuselage Main, Frame > EVALUATE AND REPAIR DENT ON LEFT FORWARD FUSELAGE BELOW CAPTAINS WINDOW BETWEEN FRAMES 12-14 AND STRINGERS 19L AND 20L, DENT MEASURES 9.25" LONG AND.0115 DEEP. SEE ADM 109SY-7735 (C-CHECK RO 6/8/2022) RECONTOURED DENT BETWEEN FRAMES 12-14 AND STRINGERS - [SDR SWIA201904025691](https://openairdocs.org/sdr/SWIA201904025691.md): Warning Message · multiple fail · Apr 1, 2019 · N109SY · Emb ERJ170200LR · Central Warning > IN FLIGHT, RECEIVED MULTIPLE WARNING MESSAGES: QRH COMPLIED WITH FOR ALL MESSAGE. ALL MESSAGES CLEARED AROUND 15 MINUTES AFTER POSTING. (FLT#5433) CLOSED IAW FIM AND PRECAUTIONARY MEASURE BLOCK DIAGRAM COMPLIANCE, DETERMINED FAULT TO BE TRANSITORY CONDITION. N - [SDR SWIA2018082745010](https://openairdocs.org/sdr/SWIA2018082745010.md): Pressure Switch · failed · Aug 27, 2018 · N109SY · Emb ERJ170200LR · Landing Gear Brake System > DURING CLIMB OUT, RECEIVED A CAUTION MESSAGE FOR THE PARKING BRAKE NOT RELEASED. COMPLIED WITH THE QRH, BUT MESSAGED PERSISTED. UNEVENTFUL LANDING AND TAXI. REMOVED AND REPLACED THE EMERGENCY PARKING BRAKE NR 2 PRESSURE SWITCH IAW AMM, OPS AND LEAK CHECK - [SDR SWIA2018070644841](https://openairdocs.org/sdr/SWIA2018070644841.md): Connector · unsecure · Jul 5, 2018 · N109SY · Emb ERJ170200LR · Landing Gear System Wiring > PARKING BRAKE NOT RELEASED CAUTION MSG IN CRUISE. RAN QRH, LANDED UNEVENTFULLY. (FLT 5867) SECURED CONNECTOR AND EMER BRAKE FAULT EXTINGUISHED. PERFORMED OPS CHECK OF EMERGENCY BRAKE SYSTEM ALL CHECKS GOOD AT THIS TIME BOTH PRESSURE SWITCHES OPERATE NORMALLY A - [SDR SWIA201541288](https://openairdocs.org/sdr/SWIA201541288.md): Structure · damaged · Jun 3, 2015 · N109SY · Emb ERJ170200LR · Fuselage Main, Structure > DAMAGE LOCATED UNDER AFT SERVICE DOOR. DAMAGE IS LOCATED BETWEEN FRAMES 85R AND 84R LOCATED BETWEEN STR 23R, STR 24R, AND STR 25R EXTENDING THROUGH AND DISTORTING STR 24R. LENGTH OF DAMAGE IN BAY BETWEEN STR 24R AND STR 25R IS 3.75"? W AND A MAX DEPTH OF.42 ## 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 = 'N109SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N109SY/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.