# Service difficulty reports: N165SY A list on [N165SY](https://openairdocs.org/aircraft/N165SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2026030675433](https://openairdocs.org/sdr/SWIA2026030675433.md): Actuator · tripped · Mar 6, 2026 · N165SY · Emb ERJ170200LR · Trailing Edge Flap Actuator > DUE TO FLAP FAIL DIVERT ODI, PERFORM FURTHER IN-DEPTH TROUBLESHOOTING OF FLAPS SYSTEM. (FLIGHT 4703) CONFIRMED WITH PIC THAT FLAPS UP LANDING DID NOT CAUSE A HIGH ENERGY STOP EVENT. NO HIGH ENGERGY STOP INSPECTION REQUIRED. CMC FLAGGED FAULT CODE 27512009A - [SDR SWIA202506250004](https://openairdocs.org/sdr/SWIA202506250004.md): Unknown · odor · Jun 24, 2025 · N165SY · Emb ERJ170200LR · Air Distribution System > PLANE HAS STRANGE ODOR. ON DEPARTURE FAS CALLED TO REPORT ODOR WAS INTENSIFYING AND A BROWNISH GRAY HAZE WAS IN THE CABIN. LEVELED OFF AT 5000 CALLED BACK THEY SAID IT WAS STARTING TO GO AWAY. AS WE CLIMBED IT BEGAN TO CLEAR. THE ODOR WAS ALWAYS PRESENT DURING - [SDR SWI2024F01158](https://openairdocs.org/sdr/SWI2024F01158.md): Seat Track · chafed · Oct 19, 2024 · N165SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > RH IB SEAT TRACK CF III HAS CHAFING AND CORROSION AT MULTIPLE LOCATIONS BETWEEN FR 83/84, 82/83, 81/82, 80/81, 79/80, 78/79, 74/75 (C-CHECK RO 11/6/2024) REMOVED AND REPLACED RH IB SEAT TRACK CF III FR74-FR84 IAW REF EMB SRM 51-40-08. NEW PART INSTALLE - [SDR SWIA20241019](https://openairdocs.org/sdr/SWIA20241019.md): Seat Track · corroded · Oct 19, 2024 · N165SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > LH IB SEAT TRACK CF III HAS CHAFING AND CORROSION AT MULTIPLE LOCATIONS BETWEEN FR 83/84, 82/83, 81/82, 80/81, 79/80, 78/79, 76/77, 74/75. (C-CHECK RO 11/6/2024) REMOVED AND REPLACED LH INBD SEAT TRACK FRAMES 74-84 REF ETD 2022-170-022163 REV.B. SEE CON - [SDR SWIA202265300](https://openairdocs.org/sdr/SWIA202265300.md): None · broken · Apr 2, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > LH AND RH PANEL SUPPORT BRACKETS ON FRAME 86 ARE BROKEN. (C CHECK RO 04/08/22) REMOVED AND REPLACED LH AND RH PANEL SUPPORT BRACKETS ON FRAME 86 REF SRM 51-40-08. APPLIED TOPCOAT TO FASTENERS REF SRM 51-23-06 - [SDR SWIA202265284](https://openairdocs.org/sdr/SWIA202265284.md): None · corroded · Mar 29, 2022 · N165SY · Emb ERJ170200LR · Fuselage Main, Frame > CORROSION - FRAME 14 O/B OF R/H SEAT TRACK. (C CHECK RO 04/08/22) REPAIRED FR14 AS REQUIRED REF SRM 53-00-10/REPAIR03 AND ITEMS 1-12 ON CONTINUATION CARD FOR WORK ACCOMPLISHED - [SDR SWIA202265286](https://openairdocs.org/sdr/SWIA202265286.md): None · chafed · Mar 28, 2022 · N165SY · Emb ERJ170200LR · Nacelle/Pylon Structure > R/H PYLON ACCESS PANEL 429ML HAVE CHAFED LOCK PAD AND CHAFE ON INTERNAL SIDE OF AFT DOOR AS MARKED. (C CHECK RO 04/08/22) / REMOVED AND REPLACED INNER DOUBLER AND LOCK PAD REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. - [SDR SWIA202265299](https://openairdocs.org/sdr/SWIA202265299.md): None · corroded · Mar 27, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION ON FWD WET AREA R/H AFT SILL AT FR17 AS MARKED. (C CHECK RO 04/08/22) / REMOVED AND REPLACED R/H AFT SILL AT FR17 REF EMB SRM 51-40-08 - [SDR SWIA202265298](https://openairdocs.org/sdr/SWIA202265298.md): None · corroded · Mar 27, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION ON FWD WET AREA R/H FWD SILL BETWEEN FR13-14 IN 2 LOCATIONS AS MARKED. (C CHECK RO 04/08/22) / REMOVED AND REPLACED FWD WET AREA R/H FWD SILL BETWEEN FR 13-14 IN 2 LOCATION REF: SRM 51-40-08 - [SDR SWIA202265297](https://openairdocs.org/sdr/SWIA202265297.md): None · corroded · Mar 27, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION ON FWD WET AREA L/H FLOOR DOUBLER BETWEEN FR19-20 AS MARKED. (C CHECK RO 04/08/22) / REMOVED AND REPLACED OUT OF LIMITS DOUBLER WITH NEW L/H DOUBLER FR19-20 IN WET AREA AS REQUIRED REF SRM 51-40-08 - [SDR SWIA202265295](https://openairdocs.org/sdr/SWIA202265295.md): None · corroded · Mar 27, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > R/H SPLICE AT FR 89 HAS CORROSION. (C CHECK RO 04/08/22) REMOVED AND REPLACED WITH NEW R/H SPLICE AT FR 89, REF SRM 51-40-08 - [SDR SWIA202265282](https://openairdocs.org/sdr/SWIA202265282.md): None · corroded · Mar 27, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION ON FWD WET AREA R/H FLOOR BEAM BETWEEN FR13-18 IN 6 LOCATIONS AS MARKED. (C CHECK RO 04/08/22) / REMOVED AND REPLACED R/H FLOOR BEAM BETWEEN FR12-21 REF EMB SRM 51-40-08. BEAM WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED. SE - [SDR SWIA202265294](https://openairdocs.org/sdr/SWIA202265294.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION FOUND LH OUTBD TOP OF FR 84 AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED OUT OF LIMITS PANEL SUPPORT WITH NEW PANEL SUPPORT AT LH FR84 REF SRM 51-40-08 - [SDR SWIA202265293](https://openairdocs.org/sdr/SWIA202265293.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Mounting Structure > CORROSION FOUND RH OUTBD TOP OF FR 84 AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED RH OTBD AT FR 84 REF EMB SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF EMB SRM 51-23-06 - [SDR SWIA202265292](https://openairdocs.org/sdr/SWIA202265292.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION FOUND IN AFT WET AREA LOCATED ON FR 87 AT LBL 4.375" AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED WITH NEW MIDDLE SHEAR PLATE AT AFT WET AREA LOCATED ON FR 87 AT LBL 4.375", REF SRM 51-40-08 - [SDR SWIA202265291](https://openairdocs.org/sdr/SWIA202265291.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION FOUND IN AFT WET AREA LOCATED ON GUSSET PLATE FR 87 AT RBL 40" AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED LOCATED ON GUSSET PLATE FR 87 AT RBL 40", REF SRM 51-40-08. - [SDR SWIA202265290](https://openairdocs.org/sdr/SWIA202265290.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION FOUND IN AFT WET AREA LOCATED ON FR 90 AT RBL 23" AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED WITH NEW GUSSET AT AFT WET AREA LOCATED ON FR 90 AT RBL 23", REF SRM 51-40-08. - [SDR SWIA202265289](https://openairdocs.org/sdr/SWIA202265289.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION FOUND IN AFT WET AREA LOCATED ON FR 90 AT RBL 11" AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED WITH NEW GUSSET AT AFT WET AREA LOCATED ON FR 90 AT RBL 11", REF SRM 51-40-08. - [SDR SWIA202265288](https://openairdocs.org/sdr/SWIA202265288.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION FOUND IN AFT WET AREA LOCATED ON FR 90 AT LBL 4.375" AS MARKED. (C CHECK RO 04/08/22) REMOVED AND REPLACED GUSSET AT FR 90 AT LBL 4.375" REF EMB SRM 51-40-08 - [SDR SWIA202265287](https://openairdocs.org/sdr/SWIA202265287.md): None · corroded · Mar 26, 2022 · N165SY · Emb ERJ170200LR · Fuselage Internal Stairs > CORROSION FOUND IN AFT WET AREA ALONG RH SHEAR PANEL ON FR 87. (C CHECK RO 04/08/22) REMOVED AND REPLACED RH SHEAR PANEL ON FR 87, REF SRM 51-40-08. - [SDR SWIA202265285](https://openairdocs.org/sdr/SWIA202265285.md): None · cracked · Mar 24, 2022 · N165SY · Emb ERJ170200LR · Fuselage Structure (General) > ANGLE CRACKED FR.52 L/H AT WHEEL WELL BULKHEAD. (C CHECK RO 04/08/22) REMOVED AND REPLACED CRACKED ANGLE AT FR.52 L/H AT WHEEL WELL BULKHEAD REF SRM 51-40-08, 51-23-06, CPM 51-25-00-910-001-A SEE CONTINUE CARD FOR WORK ACCOMPLISHED. - [SDR SWIA202265281](https://openairdocs.org/sdr/SWIA202265281.md): None · damaged · Mar 24, 2022 · N165SY · Emb ERJ170200LR · Fuselage Structure (General) > LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN BETWEEN FR32-33 AND STGR 11R-12R AS MARKED. (C CHECK RO 04/08/22) REPAIRED LIGHTNING STRIKE BY PERFORMING CUTTING OUT DAMAGE AND INSTALLING FILLER AND DOUBLER REF ETD2022-170-011754-B (1).PDF - [SDR SWIA202265280](https://openairdocs.org/sdr/SWIA202265280.md): None · cracked · Mar 23, 2022 · N165SY · Emb ERJ170200LR · Wing Structure > RH WING SPAR 1 OUTBOARD EXTENSION IS CRACKED AT THE WINGTIP TO WING SPAR ATTACHMENT. (C CHECK RO 04/08/22) REMOVED AND REPLACED CRACKED R/H WING SPAR 1 WITH NEW SPAR 1 AS REQUIRED.REF SRM 51-40-08 ## 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 = 'N165SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N165SY/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.