# Service difficulty reports: N156SY A list on [N156SY](https://openairdocs.org/aircraft/N156SY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWI2024F00113](https://openairdocs.org/sdr/SWI2024F00113.md): Seat Track · gouged · Jan 21, 2024 · N156SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > RH INBOARD SEAT TRACK SEGMENT FR74 - 84 CROWN TEETH HAVE MULTIPLE AREAS OF SURFACE PROTECTION DAMAGE AND 8 GOUGED AREAS (FR74, 74/75, 78/79, 80, 80/81, 81/82, 82/83, AND 83/84). (C-CHECK RO 2/9/2024) REMOVED AND REPLACED RH INBOARD SEAT TRACK SEGMENT FR74 - [SDR SWI2024F00112](https://openairdocs.org/sdr/SWI2024F00112.md): Floor Support · corroded · Jan 21, 2024 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > 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 2/9/2024) REMOVED AND REPLACED RH LONGITUDIUNAL BEAM AT FR 87. REF EMB SRM 51-40-08. SEE CONITUATION FOR ALL WORK P - [SDR SWIA20240209121](https://openairdocs.org/sdr/SWIA20240209121.md): Floor Support · corroded · Jan 21, 2024 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > 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 2/9/2024) REMOVED AND REPLACED L/H LONGITUDINAL FLOOR BEAM, FRAME 86-89, WHERE THE BEAM PASSES BETWEEN THE L/H AND - [SDR SWIA202266904](https://openairdocs.org/sdr/SWIA202266904.md): Rib · cracked · Nov 15, 2022 · N156SY · Emb ERJ170200LR · Fuselage Main, Structure > CRACK IN LEFT WHEEL WELL BETWEEN OPENINGS FOR FLIGHT CONTROL CABLES. (FLIGHT 4724) REMOVED AND REPLACED LEFT SIDE INBOARD RIB COMPLEMENT AT FRAME 52 IAW SRM 51-42-01. - [SDR SWIA202266728](https://openairdocs.org/sdr/SWIA202266728.md): None · smoke · Nov 5, 2022 · N156SY · Emb EMB110* · Fire Protection System > D: FLIGHT ATTENDANT REPORTS A SPARK AND WISP OF SMOKE BETWEEN FORWARD GALLEY COFFEE MAKERS. / C: NEF-GAL-2 / CAT C DUE 11/15/22 (FLIGHT 4789 - FILED CLOSED) NOV 05, 2022 STATION: CLT--INSPECTED FORWARD COFFEE MAKERS FOR EVIDENCE OF ANY ELECTRICAL OR SMOKE - [SDR SWIA202158146](https://openairdocs.org/sdr/SWIA202158146.md): Seal Rest · corroded · May 2, 2021 · N156SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION FORWARD CARGO DOOR CUTOUT, ON THE LOWER FORWARD SEAL REST IN 3 LOCATIONS (RIVET BUCKTAILS ON 2 NUTPLATES AND 1 SPOT ON EDGE UNDER LATCH FITTING), X= 305", Y= +17", Z=-63". (C-CHECK RO 5/8/2021) REMOVED AND REPLACED (2EA) NUTPLATES ON THE FORW - [SDR SWIA202158145](https://openairdocs.org/sdr/SWIA202158145.md): Seal Rest · corroded · May 2, 2021 · N156SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION FORWARD CARGO DOOR CUTOUT, ON THE LOWER AFT SEAL REST IN 2 LOCATIONS (RIVET BUCKTAILS ON 2 NUTPLATES), X= 345", Y= +17", Z=-63". (C-CHECK RO 5/8/2021) REMOVED AND REPLACED RIVETS ON THE 2 NUTPLATES FORWARD CARGO DOOR CUTOUT, ON THE LOWER AFT S - [SDR SWIA202158144](https://openairdocs.org/sdr/SWIA202158144.md): Seal Rest · corroded · May 2, 2021 · N156SY · Emb ERJ170200LR · Fuselage Main, Structure > CORROSION FORWARD CARGO DOOR CUTOUT, ON THE LOWER CENTER SEAL REST IN 4 LOCATIONS, X= 325", Y= +17", Z=-63". (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT, ON THE LOWER CENTER SEAL REST REF EMB SRM 51-40-08 - [SDR SWIA202158143](https://openairdocs.org/sdr/SWIA202158143.md): Support · corroded · Apr 25, 2021 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FWD FUSELAGE LH SILL OB AFT OF FR 19 HAS CORROSION AROUND FASTENER HOLE. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD FUSELAGE LH SILL OB AFT OF FR 19 REF EMB SRM 51-40-08 - [SDR SWIA202158142](https://openairdocs.org/sdr/SWIA202158142.md): Support · corroded · Apr 25, 2021 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FWD FUSELAGE LH SILL IB AFT OF FR 19 HAS CORROSION AROUND NUT HOLE. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD FUSELAGE LH SILL IB AFT OF FR 19 REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED - [SDR SWIA202158141](https://openairdocs.org/sdr/SWIA202158141.md): Support · corroded · Apr 25, 2021 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FWD WET AREA RH SILL HAS CORROSION AFT OF FR 13. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD WET AREA RH SILL AFT OF FRAME 13 AND APPLIED SURFACE PROTECTION PER SRM 51-23-06 SRM 51-40-08 - [SDR SWIA202158140](https://openairdocs.org/sdr/SWIA202158140.md): Floorbeam · corroded · Apr 24, 2021 · N156SY · Emb ERJ170200LR · Fuselage Main, Floor Beam > CORROSION- AFT WET AREA, RH OUTBD FLOOR SUPPORT PANEL HAS CORROSION AT FR 90 AS MARKED. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED AFT WET AREA, RH OUTBD FLOOR SUPPORT PANEL AT FR 90 REF EMB SRM 51-40-08 - [SDR SWIA202158137](https://openairdocs.org/sdr/SWIA202158137.md): Seat Track · corroded · Apr 24, 2021 · N156SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings > FWD WET AREA RH SEAT TRACK FWD OF FR 13 HAS CORROSION AROUND NUT HOLE. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED FWD WET AREA RH SEAT TRACK REF SRM 51-40-08. NO CHANGE IN WEIGHT AND BALANCE. - [SDR SWIA202158136](https://openairdocs.org/sdr/SWIA202158136.md): Shear Panel · corroded · Apr 24, 2021 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > CORROSION- AFT WET AREA, RH FLOOR BEAM BETWEEN CENTER AND RH SHEAR PANEL HAS CORROSION AS MARKED. ( FR87-88) (C-CHECK RO 5/8/2021) REMOVED AND REPLACED RH FLOOR BEAM BETWEEN CENTER AND RH SHEAR PANEL ( FR87-88) REF EMB SRM 51-40-08. NO CHANGE IN WEIGHT - [SDR SWIA202158139](https://openairdocs.org/sdr/SWIA202158139.md): Support Angle · cracked · Apr 21, 2021 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > FR 52 SUPPORT ANGLE IS CRACKED THROUGH THE O/B FASTENER FWD OF THE LH MLG WHEEL WELL AREA AS MARKED. (C-CHECK RO 5/8/2021) REMOVED AND REPLACED L/H FR 52 SUPPORT ANGLE FWD OF MLG WHEEL WELL REF SRM 51-40-08. DOME SEALED AND TOPCOATED FASTENERS REF SRM 5 - [SDR SWIA202158138](https://openairdocs.org/sdr/SWIA202158138.md): Bulkhead Web · cracked · Apr 21, 2021 · N156SY · Emb ERJ170200LR · Fuselage Main, Bulkhead > FR 52 LH WEB FWD OF THE LH MLG WHEEL WELL AREA HAS DAMAGE/ CRACKED IN 2 AREAS. (C-CHECK) REMOVED AND REPLACED L/H FR 52 WEB FWD OF MLG WHEEL WELL REF SRM 51-40-08. TOPCOATED FASTENERS REF SRM 51-23.-06. - [SDR SWIA2018103145198](https://openairdocs.org/sdr/SWIA2018103145198.md): Tip Cap · cracked · Oct 19, 2018 · N156SY · Emb ERJ170200LR · Wing, Plate/Skin > RT WING TIP SPAR 1 CRACKED AT WING TIP ATTACH POINT. (C-CHECK) RO: 10/25/2018. REMOVED AND REPLACED THE RT WING TIP REF AMM 57-30-00. - [SDR SWIA2018103145189](https://openairdocs.org/sdr/SWIA2018103145189.md): Tip Cap · cracked · Oct 19, 2018 · N156SY · Emb ERJ170200LR · Wing, Plate/Skin > LT WING TIP CRACKED AT WING TIP ATTACH POINT. (C-CHECK) RO: 10/24/2018. REMOVED AND REPLACED THE LT WING TIP REF AMM 57-30-00. - [SDR SWIA2018103145197](https://openairdocs.org/sdr/SWIA2018103145197.md): Retainer · bent · Oct 17, 2018 · N156SY · Emb ERJ170200LR · Cargo/Baggage Doors > FWD CARGO DOOR AFT LOWER CORNER SEAL RETAINER BENT. (C-CHECK) RO: 10/24/2018. RECONTOURED DENT ON THE FWD CARGO DOOR AFT LOWER SEAL RETAINER REF SRM 52-00-02. - [SDR SWIA2018103145194](https://openairdocs.org/sdr/SWIA2018103145194.md): Panel · cracked · Oct 17, 2018 · N156SY · Emb ERJ170200LR · Aircraft Structures > PANEL 822DRW HAS CRACK IN COMPOSITE. (C-CHECK) RO: 10/24/2018. REPAIRED AND TOUCHED UP PAINT ON PANEL 822DRW IN REFERENCE TO AMM 50-31-00. - [SDR SWIA2018410315193](https://openairdocs.org/sdr/SWIA2018410315193.md): Panel · cracked · Oct 17, 2018 · N156SY · Emb ERJ170200LR · Aircraft Structures > 822ARW PANEL HAS CRACK IN COMPOSITE.(C-CHECK) RO: 10/25/2018. REPAIRED AND TOUCHED UP PAINT ON PANEL 822ARW IN REFERENCE TO AMM 50-31-00. - [SDR SWIA2018103145192](https://openairdocs.org/sdr/SWIA2018103145192.md): Vane · cracked · Oct 17, 2018 · N156SY · Emb ERJ170200LR · Engine (Turbine/Turboprop) > PANEL 421DR VANE IS CRACKED AT THE WELD.(C-CHECK) RO: 10/24/2018. TIG WELDED CRACK REF MM. - [SDR SWIA2018103145191](https://openairdocs.org/sdr/SWIA2018103145191.md): Vane · cracked · Oct 17, 2018 · N156SY · Emb ERJ170200LR · Engine (Turbine/Turboprop) > PANEL 411DR VANE IS CRACKED AT THE WELD. (C-CHECK) RO: 10/24/2018. TIG WELDED CRACK REF MM. - [SDR SWIA2018103145195](https://openairdocs.org/sdr/SWIA2018103145195.md): Panel · cracked · Oct 16, 2018 · N156SY · Emb ERJ170200LR · Fuselage Miscellaneous Structure > TIRE BURST PANEL CRACKED IN LT MLG WHEEL WELL. (C-CHECK) RO: 10/24/2018. COMPLIED WITH REPAIR OF LT MLG WHEEL WELL FAIRING, REF SRM 53-22-04. ## 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 = 'N156SY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N156SY/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.