# Service difficulty reports: N105SY A list on [N105SY](https://openairdocs.org/aircraft/N105SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWI2024092000011](https://openairdocs.org/sdr/SWI2024092000011.md): Floorbeam · corroded · Aug 22, 2024 · N105SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > 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 9/19/2024) REMOVED AND REPLACED RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER - [SDR SWIA2024092000010](https://openairdocs.org/sdr/SWIA2024092000010.md): Beam · corroded · Aug 22, 2024 · N105SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FORWARD PASSENGER DOOR CUTOUT HAS CORROSION AT FORWARD CUTOUT FOR GIRTBAR FITTING AS MARKED. (C-CHECK RO 9/19/2024) REMOVED AND REPLACED FORWARD PASSENGER DOOR THRESHOLD BEAM REF SRM 51-40-08 SEE CONTINUATION CARD FOR WORK PERFORMED NO CHANGE TO WEIGHT - [SDR SWIA202409200009](https://openairdocs.org/sdr/SWIA202409200009.md): Skin · damaged · Aug 16, 2024 · N105SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA92805-ETD2024-170-021422 MXCODEID76852-PR - AT 2500 FT BIRD STRIKE, NOSE RADOME AND WINDSHIELD FIRST OFFICER WAS IMPACTED. PERFORMED BIRD STRIKE INSPECTION PER AMM05-50-02-200-801-A. DAMAGE FOUND ON SKIN AT FRAME 4 STR - [SDR SWIA20230211](https://openairdocs.org/sdr/SWIA20230211.md): None · damaged · Feb 11, 2023 · N105SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings > THE SEAT TRACK AT SEAT 23C IS DAMAGED. (FILED CLOSED)REMOVED AND REPLACED SEAT TRACK AT SEAT 23C IN REF TO AMM 25-21-11. - [SDR SWIA202264088](https://openairdocs.org/sdr/SWIA202264088.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Life Jacket > FORWARD PAX DOOR EVACUATION-SLIDE-MECHANISM CABLE LOWER ATTACHING HARDWARE CORRODED. (C CHECK RO 01/28/2022) REMOVED AND REPLACED FORWARD PAX DOOR EVACUATION-SLIDE-MECHANISM CABLE LOWER ATTACHING HARDWARE REF EMB175 AMM 20-10-01 ASSETT #456 DUE CAL 5-3-2 - [SDR SWIA202264087](https://openairdocs.org/sdr/SWIA202264087.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Life Jacket > FORWARD PAX DOOR 2 EACH ESCAPE SLIDE MOUNT BRACKET BOLTS CORRODED (C CHECK RO 01/28/2022) REMOVED AND REPLACED FORWARD PAX DOOR 2 EACH ESCAPE SLIDE MOUNT BRACKET BOLTS REF EMB175 AMM 20-10-01 ASSETT #456 DUE CAL 5-3-22 - [SDR SWIA202264086](https://openairdocs.org/sdr/SWIA202264086.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Fuselage Structure (General) > CORROSION ON LH FLOOR DOUBLER AROUND LH FORWARD WINDSCREEN FLOOR MOUNT FITTING AND ALONG THE FORWARD EDGE BETWEEN FRAMES 19 AND 20. (C CHECK RO 01/28/2022) / REMOVED AND REPLACED LH FLOOR DOUBLER AROUND LH FORWARD WINDSCREEN FLOOR MOUNT FITTING AND ALO - [SDR SWIA202264085](https://openairdocs.org/sdr/SWIA202264085.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Fuselage Structure (General) > CORROSION ON CENTER SHEAR PANEL AT FR 87-88 (C CHECK RO 01/28/2022) REMOVED AND REPLACED CENTER SHEAR PANEL AT FR 87-88 REF EMB SRM 51-40-08 - [SDR SWIA202264084](https://openairdocs.org/sdr/SWIA202264084.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > R/H SHEAR PANEL FR 87-88 HAS AREAS OF CORROSION. (C CHECK RO 01/28/2022) REMOVED AND REPLACED R/H SHEAR PANEL FR 87-88 REF EMB SRM 51-40-08 - [SDR SWIA202264083](https://openairdocs.org/sdr/SWIA202264083.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Life Jacket > FORWARD SERVICE DOOR 2 EACH ESCAPE SLIDE MOUNT BRACKET BOLTS CORRODED (C CHECK RO 01/28/2022) REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE MOUNT BRACKET BOLTS. REF. EMB 175 AMM 20-10-01. TW; TC1-456 CAL DUE; 5-3-22. - [SDR SWIA202264082](https://openairdocs.org/sdr/SWIA202264082.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION ON RH GUSSET SPLICE AT FR 90. (C CHECK RO 01/28/2022) REMOVED AND REPLACED RH GUSSET SPLICE AT FR 90 REF EMB SRM 51-40-08 - [SDR SWIA202264081](https://openairdocs.org/sdr/SWIA202264081.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > R/H FLOOR PANEL SUPPORT AT FR 87-90 IS CORRODED IN MULTIPLE AREAS. (C CHECK RO 01/28/2022) REMOVED AND REPLACED R/H FLOOR PANEL SUPPORT AT FR 87-90 REF EMB SRM 51-40-08 - [SDR SWIA202264080](https://openairdocs.org/sdr/SWIA202264080.md): None · corroded · Jan 10, 2022 · N105SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings > LH FLOOR BEAM SEAT TRACK CORRODED AS MARKED FR 82-85. (C CHECK RO 01/28/2022) / REPAIRED LH FLOOR BEAM SEAT TRACK FR 82-85 BY SPLICING SEAT TRACK REF EMB ETD2022-170-001077. - [SDR SWIA202264089](https://openairdocs.org/sdr/SWIA202264089.md): None · damaged · Jan 8, 2022 · N105SY · Emb ERJ170200LR · Doors > L2 FUSELAGE STOPS 4EA HAVE DAMAGED FACES. (C CHECK RO 01/28/2022) REMOVED AND REPLACED 1EA DAMAGED L2 FUSELAGE STOP. UPON FURTHER INSPECTION, FOUND ONLY 1EA FUSELAGE STOP TO BE DAMAGED. REF. E175 AMM 52-12-23 - [SDR SWIA202264078](https://openairdocs.org/sdr/SWIA202264078.md): None · dented · Jan 8, 2022 · N105SY · Emb ERJ170200LR · Fuselage Structure (General) > DENT OIL CANNING ON RH FUSELAGE, FWD. OF FRAME 94 AND ABOVE STRINGER 23R, AT REAR FUSELAGE ACCESS DOOR. (C CHECK RO 01/28/2022) REPAIRED DENT ON RH FUSELAGE, FWD. OF FRAME 94 AND ABOVE STRINGER 23R, AT REAR FUSELAGE ACCESS DOOR. REF SRM 53-30-01/REPAIR12P. - [SDR SWIA202264077](https://openairdocs.org/sdr/SWIA202264077.md): None · cracked · Jan 6, 2022 · N105SY · Emb ERJ170200LR · Fuselage Structure (General) > CRACKED RIVET AND EVIDENCE OF CRACKED AERODYNAMIC FLANGE AT FRAME 54, ABOVE OVER-WING PNL. (MARKED) (C CHECK RO 01/28/2022) REMOVED AND REPLACED AERODYNAMIC FLANGE AT FRAME 54 REF EMB SRM 51-40-08 - [SDR SWIA202264076](https://openairdocs.org/sdr/SWIA202264076.md): None · cracked · Jan 5, 2022 · N105SY · Emb ERJ170200LR · Aileron Tabs > R/H WING LOWER SURFACE HAS CRACK AT FORWARD EDGE OF MLG CUTOUT I/B OF GEAR. (C CHECK RO 01/28/2022) REPAIRED R/H LOWER SURFACE WING CRACK AT FWD EDGE OF MLG CUTOUT I/B OOF GEAR PER ETD2022-170-000846 REV.: A - [SDR SWIA202164079](https://openairdocs.org/sdr/SWIA202164079.md): None · corroded · Dec 17, 2021 · N105SY · Emb ERJ170200LR · Fuselage, Powerplant Attach Fittings > COMPLY WITH SCHEDULED MAINTENANCE CODE: 96/88 MO INSP E175 - COMPLY WITH ERJ175 96/88 MO INSPECIOTN, PART NUMBER: -, SERIAL NUMBER: 17000395, POSITION: (C CHECK RO 01/28/2022) COMPLIED WITH SCHEDULED MAINTENANCE CODE: 96/88 MO INSP E175 - COMPLIED WIT - [SDR SWIA202158151](https://openairdocs.org/sdr/SWIA202158151.md): Warning Message · false activation · May 17, 2021 · N105SY · Emb ERJ170200LR · Landing Gear Brake System > BRAKE LH FAULT MSG AFTER GEAR EXTENSION ON APPROACH. COMPLIED WITH QRH. MSG REMAINED UNTIL GEAR CYCLED. (FLIGHT 4735 - FILED CLOSED) TROUBLESHOT LH BRAKE FAULT MSG PER ERJ 175 FIM 32-41-00-810-823-A. PER SUBTASK 810-095-A IN THE CMC PREFORMED BCM1 PR - [SDR SWIA201744092](https://openairdocs.org/sdr/SWIA201744092.md): Fault Message · false activation · Dec 26, 2017 · N105SY · Emb ERJ170200LR · Landing Gear Brake System > RIGHT AND LEFT BRAKE FAULTS. PERFORMED A RESET IAW FIM, MESSAGES CLEARED. - [SDR SWIA201439203](https://openairdocs.org/sdr/SWIA201439203.md): Skin · dented · Aug 24, 2014 · N105SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > SMALL DENT AFT OF MAIN CABIN DOOR. PERFORMED A DETAILED INSPECTION OF THE DAMAGE AREA IAW SRM AND FOUND TWO DENTS THAT OUR OUT OF LIMITS IAW THE SRM. REPAIRED IAW ETD. - [SDR SWIA201438816](https://openairdocs.org/sdr/SWIA201438816.md): Light · failed · Jul 17, 2014 · N105SY · Emb ERJ170200LR · Emergency Lighting > EMERGENCY LIGHT OVER MAIN CABIN DOOR IS ONLY HALF LIGHTED WHEN SELECTED ON. R & R FORWARD EMERGENCY LIGHT ASSY IAW AMM. OPS CHECKED OK. ## 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 = 'N105SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N105SY/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.