# Service difficulty reports: N241SY A list on [N241SY](https://openairdocs.org/aircraft/N241SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2026072276667](https://openairdocs.org/sdr/SWIA2026072276667.md): Tire · out of round · Jul 22, 2026 · N241SY · Emb ERJ170200LR · Tire > AFTER A STRONG NOSE WHEEL SHIMMY ON ROTATION, THE LANDING GEAR WOULD NOT COME UP. RAN THE QRH AND RETURNED TO THE AIRPORT. (FLIGHT 4038) SEE EAML 1946484 FOR NOSE SHIMMY INSPECTION & EAML 1946487. FOUND NOSE TIRES OUT OF ROUND. REMOVED AND REPLACED #1 AND - [SDR SWIA2025090200830](https://openairdocs.org/sdr/SWIA2025090200830.md): Cabin Pressure · faulted · Aug 30, 2025 · N241SY · Emb ERJ170200LR · Cabin Pressure Control System > DECLARED AN EMERGENCY AT FLT LEVEL 340 FEELINGS OF HYPOXIA. FIRST OFFICER REPORTED FEELING LIGHTHEADED/DISORIENTED WHILE TALKING TOFWD FLT ATTENDANT WHO ORIGINALLY CALLED THE FLT DECK WITH COMPLAINTS THAT THE AFT FLIGHT ATTENDANT LIGHTHEADED. STARTED AN EMERG - [SDR SWIA2024121601127](https://openairdocs.org/sdr/SWIA2024121601127.md): Shear Tie · corroded · Nov 27, 2024 · N241SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > SHEAR CLIP AT FR.87 BETWEEN STGR 27R AND STGR 28R IS CORRODED (C-CHECK RO 12/13/2024) INSTALLED NEW FR 87 STGR 27R-28R SHEAR CLIP REF. ERJ175 SRM 51-40-08. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED. PART REPLACED WITH OEM NO CHANGE TO WEIGHT AND - [SDR SWIA2024121601126](https://openairdocs.org/sdr/SWIA2024121601126.md): Seat Track · gouged · Nov 26, 2024 · N241SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN RH LATERAL SEAT TRACK SEGMENT FR 43-59 HAS GOUGE DAMAGE NEAR FR 43, 46, 47, 48, 54, 55, 57 AND 59. (C-CHECK RO 12/13/2024) REMOVED AND REPLACED THE DAMAGED R/H LATERAL SEAT TRACK SEGMENT BETWEEN FRAMES 43 AND 59 REF ERJ175 SRM 51-40-08. SEAT - [SDR SWIA2024121601367](https://openairdocs.org/sdr/SWIA2024121601367.md): Seat Track · gouged · Nov 25, 2024 · N241SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN RH LATERAL SEAT TRACK SEGMENT FR23-34 HAS GOUGE DAMAGE AT FR 23, 24, 25, 28, 29, 31, 32 AND 33. (C-CHECK RO 12/13/2024) REMOVED AND REPLACED RH LATERAL SEAT TRACK BETWEEN FR 23-34 REF EMB SRM 51-40-08. SEAT TRACK REPLACED WIRTH OEM PART NO C - [SDR SWIA2024121601366](https://openairdocs.org/sdr/SWIA2024121601366.md): Skin · corroded · Nov 25, 2024 · N241SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > DURING REMOVAL OF WASTE ACCESS DOOR FOUND CORROSION PRESENT ON THE WASTE BOX DOUBLER AREA COVERED BY THE WASTE ACCESS DOOR HINGE. (C-CHECK RO 12/13/2024) REMOVED AND REPLACED WASTE BOX DOUBLER WITH NEW REF. ERJ175 SRM 51-40-08. DOUBLER REPLACED WITH OEM - [SDR SWIA2024121601365](https://openairdocs.org/sdr/SWIA2024121601365.md): Seat Track · gouged · Nov 25, 2024 · N241SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN RH LATERAL SEAT TRACK SEGMENT FR 21-23 HAS GOUGE DAMAGE AT FR 21 AND 22. (C-CHECK RO 12/13/2024) REMOVED AND REPLACED MAIN CABIN RH LATERAL SEAT TRACK SEGMENT FR 20-23 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. - [SDR SWIA202412161125](https://openairdocs.org/sdr/SWIA202412161125.md): Seat Track · gouged · Nov 25, 2024 · N241SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > MAIN CABIN RH FLOOR INBOARD SEAT TRACK FR23-34 HAS GOUGE DAMAGE AT FR 23, 24, 25, 27, 28, 29, 30, 32-33, AND 34. (C-CHECK RO 12/13/2024) REMOVED AND REPLACED RH FLOOR INBOARD SEAT TRACK FR23-34 REF EMB SRM 51-40-08. SEAT TRACK REPLACED WITH OEM PART NO - [SDR SWIA202412161124](https://openairdocs.org/sdr/SWIA202412161124.md): Shear Tie · corroded · Nov 24, 2024 · N241SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > AFT CARGO HAS CORRODED SHEAR CLIP AT FR 84 STGR 27R-28R. (C-CHECK RO 12/13/2024) INSTALLED NEW FR 84 STGR 27R-28R SHEAR CLIP REF. ERJ175 SRM 51-40-08. SEE CONTINUATION CARD FOR FURTHER WORK PERFORMED. PART REPLACED WITH OEM NO CHANGE TO WEIGHT AND BALAN - [SDR SWIA202264573](https://openairdocs.org/sdr/SWIA202264573.md): None · cracked · Feb 4, 2022 · N241SY · Emb ERJ170200LR · Fuselage Structure (General) > FR 52 EXTERNALSUPPORT ANGLE IS CRACKED THROUGH THE O/B FASTENER FWD OF THE LH MLG WHEEL WELL AREA AS MARKED. (C CHECK RO 02/21/2022) REMOVED AND REPLACED FR 52 EXTERNAL SUPPORT ANGLE FWD OF THE LH MLG WHEEL WELL REF SRM 51-40-08. SE CONTINUATION CARD FOR WO - [SDR SWIA202264577](https://openairdocs.org/sdr/SWIA202264577.md): None · corroded · Feb 3, 2022 · N241SY · Emb EMB110* · Fuselage Main, Longeron/Stringer > AFT WET AREA FR87-88 R/H SHEAR PANEL HAS CORROSION 2 EA AREAS AS MARKED (C CHECK RO 02/21/2022) REMOVED AND REPLACED AFT WET AREA FR87-88 R/H SHEAR PANEL REF SRM 51-40-08 - [SDR SWIA202264576](https://openairdocs.org/sdr/SWIA202264576.md): None · corroded · Feb 3, 2022 · N241SY · Emb EMB110* · Fuselage Internal Stairs > AFT WET AREA FR89 R/H PANEL SUPPORT CORRODED THRU AT GALLEY MOUNT BOLT AREA (C CHECK RO 02/21/2022) REMOVED AND REPLACED RH PANEL SUPPORT FR89 REF SRM 51-40-08 - [SDR SWIA202264575](https://openairdocs.org/sdr/SWIA202264575.md): None · corroded · Feb 3, 2022 · N241SY · Emb EMB110* · Fuselage Internal Stairs > AFT WET AREA FR90 R/H SIDE GUSSET PLATE (TEXAS) CORRODED AT GALLEY MOUNT BOLT HOLE (C CHECK RO 02/21/2022) REMOVED AND REPLACED CORRODED AFT GUSSET PLATE FR90 R/H WITH NEW GUSSET PLAT AS REQUIRED REF SRM 51-40-08 - [SDR SWIA202264574](https://openairdocs.org/sdr/SWIA202264574.md): None · corroded · Feb 3, 2022 · N241SY · Emb EMB110* · Fuselage Internal Mounting Structure > FWD WET AREA FR12 TO FR14 R/H SIDE 3 HOLE SILL IS CORRODED AS MARKED (C CHECK RO 02/21/2022) REMOVED AND REPLACED FWD WET AREA FR12 TO FR14 R/H SIDE 3 HOLE SILL REF EMB SRM 51-40-08. - [SDR SWIA202264571](https://openairdocs.org/sdr/SWIA202264571.md): None · broken · Feb 3, 2022 · N241SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > FR86 RH SIDE FLOOR BOARD SUPPORT BROKEN OFF AS MARKED (C CHECK RO 02/21/2022) REMOVED AND INSTALLED NEW FRAME 86 RH SIDE FLOOR BOARD SUPPORT REF SRM 51-40-08. APPLIED SURFACE PROTECTION REF SRM 51-23-06 ANS CIC REF CPM 51-25-00. - [SDR SWIA202264570](https://openairdocs.org/sdr/SWIA202264570.md): None · broken · Feb 3, 2022 · N241SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > FR85 LH SIDE FLOORBOARD SUPPORT IS BROKEN AS MARKED (C CHECK RO 02/21/2022) REMOVED AND INSTALLED NEW FRAME 85 LH SIDE FLOOR BOARD SUPPORT REF SRM 51-40-08. APPLIED SURFACE PROTECTION REF SRM 51-23-06 AND APPLIED CIC REF CPM 51-25-00 - [SDR SWIA202264572](https://openairdocs.org/sdr/SWIA202264572.md): None · seized · Feb 1, 2022 · N241SY · Emb ERJ170200LR · Horizontal Stabilizer, Attach Fittings > LH ELEVATOR HINGE #1 AND 3 BOLTS THAT ATTACH THE HINGE TO THE ELEVATORS SURFACE WERE FOUND SEIZED DURING REMOVAL. (C CHECK RO 02/21/2022) / LH ELEVATOR HINGE #1 AND #3 BOLTS REPLACED ON RACK REF AMM 27-31-05 ## 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 = 'N241SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N241SY/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.