# Service difficulty reports: N160SY A list on [N160SY](https://openairdocs.org/aircraft/N160SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA2026030475414](https://openairdocs.org/sdr/SWIA2026030475414.md): Spring · broken · Mar 4, 2026 · N160SY · Emb ERJ170200LR · Landing Gear Selector > ON APPROACH, RECEIVED MLG LEVER DISAGREE MESSAGE, & RT MAIN WAS NOT INDICATING DOWN. RAN QRH & MESSAGE CLEARED & GEAR OPS NORMAL ON SECOND APPROACH. (FLIGHT 5574) INTERROGATED CMC, FOUND FAULT CODES 32612208PSS & 32611213PSS. RT MLG R2 DOWNLOCK SPRING BROKE - [SDR SWIA202405150001](https://openairdocs.org/sdr/SWIA202405150001.md): Skin · chafed · May 1, 2024 · N160SY · Emb ERJ170200LR · Fuselage Main, Plate/Skin > RH SLAT PANEL #3 NOSE SKIN HAS CHAFES IN TWO SPOTS AS MARKED. (C-CHECK RO 5/14/2024) BLENDED OUT THE CHAFES ON RH WING #3 SLAT LEADING EDGE NOSE SKIN. BLEND DIMENSIONS AS FOLLOWS; D=.010", L= 1.747", W= 1.498", NOMINAL THICKNESS=.087", MAXIMUM ALLOWABLE - [SDR SWIA2024051500430](https://openairdocs.org/sdr/SWIA2024051500430.md): Rib · damaged · Apr 30, 2024 · N160SY · Emb ERJ170200LR · Wing, Rib/Bulkhead > DURING COMPLETION OF SB170-57-0073 REV. 1 FOUND ELONGATED MOUNT HOLE FOR UPPER IB RIB 42 CONNECTION IN R/H WING OB SPAR 1 P/N 170-31107-052 (C-CHECK RO 5/14/2024) REPAIRED ELONGATED HOLE ON UPPER IB RIB 42 CONNECTION ON RH WING OB SPAR 1 PN: 170-31107-052 - [SDR SWIA2024051500426](https://openairdocs.org/sdr/SWIA2024051500426.md): Skin · scratched · Apr 26, 2024 · N160SY · Emb ERJ170200LR · Leading Edge Devices > RH WING #3 SLAT INBOARD END UPPER SKIN HAS TWO SCRATCHES. (C-CHECK RO 5/14/2024) DAMAGE ACCEPTED AS PERMANENTLY ALLOOWABLE WITH NO ADDITIONAL REPAIR REQUIRED PER ETD2024-170-012219 THE REWORKED AREAS MUST BE DETAILED VISUAL INSPECTED EVERY 24 MONTHS FOR C - [SDR SWIA2024051500425](https://openairdocs.org/sdr/SWIA2024051500425.md): Seat Track · gouged · Apr 25, 2024 · N160SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > GOUGES ON L/H SIDEWALL SEAT TRACK BETWEEN FR 21-23 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 5/14/2024) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK BETWEEN FR 21-23 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 (310857) AND APPLIED CIC PROTECT - [SDR SWI202405150409](https://openairdocs.org/sdr/SWI202405150409.md): Seat Track · corroded · Apr 25, 2024 · N160SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > RH INBD SEAT TRACK FR 43-59 GOUGED AND CORRODED AS MARKED: FR 43, 43-45, 46, 47, 48, 49, 50, 56, 57 AND 58 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED RH INBD SEAT TRACK FR 43-59 REF SRM 51-40-08 REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT - [SDR SWI2024F00407](https://openairdocs.org/sdr/SWI2024F00407.md): Seat Track · corroded · Apr 24, 2024 · N160SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > LH IB SEAT TRACK HAS MULTIPLE LOCATIONS WHERE CORROSION IS PRESENT AS MARKED FR 74- FR 84 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED LH IB SEAT TRACK FR 74- FR 84. REF EMB SRM 51-40-08. THIS REPAIR DOES NOT CHANGE WEIGHT AND BALANCE. SEE CONTINUATION CARD - [SDR SWI20240515000406](https://openairdocs.org/sdr/SWI20240515000406.md): Seat Track · corroded · Apr 24, 2024 · N160SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > LH OB SEAT TRACK HAS MULTIPLE LOCATIONS WHERE CORROSION IS PRESENT AS MARKED FR 74- FR 84 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED LH OB SEAT TRACK FR 74- FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED. - [SDR SWIA2024051500424](https://openairdocs.org/sdr/SWIA2024051500424.md): Seat Track · corroded · Apr 24, 2024 · N160SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > RH IB SEAT TRACK HAS MULTIPLE LOCATIONS WHERE CORROSION IS PRESENT AS MARKED FR 74- FR 84 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED RH IB SEAT TRACK FR 74-84 REF SRM 51-40-08. RESTORED SURFACE PROTOCTION REF SRM 51-23-06 PO 313198 AND CPM 51-25-00 PO 314 - [SDR SWIA2024051500421](https://openairdocs.org/sdr/SWIA2024051500421.md): Floorbeam · corroded · Apr 21, 2024 · N160SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > CORROSION, AFT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LH AND CENTER SHEAR PANELS. (C-CHECK RO 5/14/2024) REMOVED AND REPLACED A FT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87, REF SRM 51-40-08. RESTORE - [SDR SWI2023F00476](https://openairdocs.org/sdr/SWI2023F00476.md): Unknown · warning message · Nov 19, 2023 · N160SY · Emb ERJ170200LR · Pneumatic Distribution System > SHORTLY AFTER TAKEOFF, WITH ECS OFF AND APU ON, BLEED 2 OVERPRESS CAUTION MESSAGE APPEARED. COMPLETED ASSOCIATED QRH AND THE MESSAGE EXTINGUISHED. THE MESSAGE DID NOT RETURN, NORMAL OPERATION THEREAFTER. (FLIGHT 4746 FILED CLOSED)INTERROGATED CMC AND FOUND BLE - [SDR SWIA202158734](https://openairdocs.org/sdr/SWIA202158734.md): Floorbeam · corroded · May 29, 2021 · N160SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > AFT WET AREA-FLOOR CROSSBEAM FR 84 HAS CORROSION/ LIGHT SCORE MARK ON UPPER FLANGE 12" OTBD OF RH SEAT TRACK (C-CHECK RO 6/11/2021) INSTALLED NEW L ANGLE REPAIR AT FR84 REF ETD 2021-170-017514 SRM53-00-10 REPAIR 03. REFER TO ATTACHMENTS FOR WORK PERFO - [SDR SWIA202158733](https://openairdocs.org/sdr/SWIA202158733.md): Seat Track · corroded · May 28, 2021 · N160SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > FWD WET AREA- RH FLOOR SEAT TRACK (Y= 10.7") HAS CORROSION ON FLOOR FLANGE AT FR 17 (C-CHECK RO 6/11/2021) BLENDED OUT CORROSION REF SRM 51-10-03. LENGTH: 1.237" / WIDTH:.494" / DEPTH:.024" / ORIGINAL THICKNESS:.080' / REMAINING MATERIAL:.056" / ASS - [SDR SWIA202158732](https://openairdocs.org/sdr/SWIA202158732.md): Floorbeam · damaged · May 28, 2021 · N160SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > FWD WET AREA- FRAME 17 FLOOR CROSS BEAM UPPER FLANGE HAS SCORE MARK EXTENDING BETWEEN LH FLOOR SEAT TRACK (Y= -10.7") AND RH FLOOR SEAT TRACK (Y= 10.7") (C-CHECK RO 6/11/2021) BLENDED OUT DAMAGE REF SRM 51-10-03. LENGTH: 21.500" / WIDTH:.900" / DEPTH: - [SDR SWIA202158735](https://openairdocs.org/sdr/SWIA202158735.md): Door Frame · corroded · May 27, 2021 · N160SY · Emb ERJ170200LR · Fuselage Main, Structure > FWD CARGO DOOR FRAME, CORROSION AROUND NUT PLATES IN SEAL REST SURFACE, AS MARKED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED FWD CARGO DOOR FRAME NUTPLATES AS MARKED. REF. SRM 51-75-16. - [SDR SWIA201845097](https://openairdocs.org/sdr/SWIA201845097.md): Sensor · dirty · Sep 26, 2018 · N160SY · Emb ERJ170200LR · Landing Gear Position and Warning > RETURN TO FIELD. LANDING GEAR WOULD NOT RETRACT. LG WOW SYS FAIL CAUTION MSG. (FLT#5261) FO: 09/27/2018 CLOSED CLEANED BOTH WOW SENSORS IAW AMM. PERFORMED MULTIPLE GEAR SWINGS IAW AMM. OPS CHECK GOOD. ## 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 = 'N160SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N160SY/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.