N171SY

Service difficulty reports · 31

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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 = 'N171SY' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR SWIA2026021775292Bleed Air Sys · warning messageON CLIMBOUT. BLEED 1 OVERPRESSURE MESSAGE ON CLIMBOUT. RAN QRH. MESSAGE DID NOT EXTINGUISH AFTER FIRST STEP. AFTER 2ND STEPS OF PROCEDURE MESSAGE EXTINGUISHED. (FLIGHT 3439). MX ACTION CW IAW AMM 36-11-03-040-801-A. INTERROGATED CMC, FOUND FAULT 36111210AMFeb 17, 2026 · N171SY · Emb ERJ170200LR · Pneumatic Distribution SystemSDR SWIA2025100600929Skin · dentedDUE TO BIRD STRIKE, FOUND DENT ON FWD FUSELAGE LOWER LH SIDE SKIN. THE DENT IS LOCATED BETWEEN FR01 AND FR02, AND BETWEEN STGR 25L AND STGR 26L. IT MEASURES 3.3 INCHES LONG, 2.75 INCHES WIDE, AND 0.077 INCHES DEEP. THERE IS A CREASE AND OIL CANNING PRESENT. (Sep 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA202509300029Skin · dentedDUE TO BIRD STRIKE, FOUND DENT ON FWD FUSELAGE LOWER LH SIDE SKIN. THE DENT IS LOCATED BETWEEN FR01 AND FR02, AND BETWEEN STGR 25L AND STGR 26L. IT MEASURES 3.3 INCHES LONG, 2.75 INCHES WIDE, AND 0.077 INCHES DEEP. THERE IS A CREASE AND OIL CANNING PRESENT. (Sep 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2025070100629Skin · damagedFUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY MAJOR REPAIR, COMPLIED WITH PERMANENT REPAIR OF RT AFT SIDE OF FUSELAGE SKIN, BETWEEN HYDRAULIC SYSTEMJun 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2025063000029Skin · ground damageFUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSJun 29, 2025 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWI2025F00632Seat Track · gougedR/H PASSENGER CABIN FLOOR O/B LATERAL SEAT TRACK AT FR20 TO FR21 HAS GOUGE (C-CHECK RO 05/11/2025)REMOVED AND REPLACED R/H PASSENGER CABIN FLOOR O/B LATERAL SEAT TRACK BETWEEN FR16 TO FR20. REF: SRM 51-40-08. SEAT TRACK REPLACE WITH OEM PART NO CHANGE TO WEIGApr 21, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWI2025F00631Seat Track · corrodedR/H PASSENGER CABIN FLOOR AT FR17 R/H SEAT TRACK HAS SURFACE CORROSION (C-CHECK RO 05/11/2025)REPAIRED R/H PASSENGER CABIN FLOOR AT FR17 R/H SEAT TRACK IN ACCORDANCE WITH REF EMB SRM 53-10-10/REPAIR 01.Apr 21, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202505120421Seat Track · corrodedL/H PASSENGER CABIN FLOOR AT FR17 L/H SEAT TRACK HAS SURFACE CORROSION (C-CHECK RO 05/11/2025)REMOVED AND REPLACED L/H PASSENGER CABIN FLOOR BTW FR12-FR20 L/H SEAT TRACK. REF: EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.Apr 21, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA20250512419Seat Track · corrodedCORROSION ON RH FLOOR SEAT TRACK AT FR 76 AND 80. (C-CHECK RO 05/11/2025)REMOVED AND REPLACED RH FLOOR SEAT TRACK AT FR 76-80 IN ACCODANCE WITH ETD2022-170-022163-C. REPLACED WITH NEW OEM PART. NO CHANGE TO WEIGHT AND BALANCE REQUIRED.Apr 19, 2025 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWI2025F00630Rib · crackedCRACK RH HORIZONTAL RIB 12 LOWER FWD FLANGE AT AFT RIVET. (C-CHECK RO 05/11/2025)REMOVED AND REPLACED RH HORIZONATL RIB 12 REF. EMB SRM 51-40-08, AND ETD2025-170-906827.Apr 18, 2025 · N171SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR SWIA20250512418Rib · crackedSUSPECTED CRACK LH HORIZONTAL RIB 12 LOWER FWD FLANGE AT AFT RIVET. (C-CHECK RO 05/11/2025)REMOVED AND REPLACED HORIZONTAL RIB 12 REF. EMB SRM 51-40-08, AND ETD2025-170-906827.Apr 18, 2025 · N171SY · Emb ERJ170200LR · Horizontal Stabilizer, Spar/RibSDR SWIA202266588None · corrodedAFT WET AREA R/H LONGITUDINAL BEAM HAS CORROSION ON THE TOP SURFACE AT FR. 88. (C-CHECK RO 10/4/2022) / REMOVED AND REPLACED AFT WET AREA R/H LONGITUDINAL BEAM AT FR 88 REF SRM 51-40-08. APPLIED SURFACE PROTECTION REF SRM 51-23-06. NO CHANGE TO WEIGHT Sep 23, 2022 · N171SY · Emb EMB110* · Fuselage Main, FrameSDR SWIA202266587None · gougedCF I L/H INBOARD SEAT TRACK HAS MULTIPLE AREAS OF GOUGES FROM FR 22 TO FR 29 AS MARKED (C-CHECK RO 10/4/2022) CORRECT LOCATION OF SEAT TRACK REPAIR IS FR 23- 27. SPLICED IN SEAT TRACK FILLER PN PE11056-F3A INTO CFI L/H INBOARD SEAT TRACK FROM FR23 TO FRSep 15, 2022 · N171SY · Emb EMB110* · Fuselage, Powerplant Attach FittingsSDR SWIA202266586None · gougedCF I R/H INBOARD SEAT TRACK HAS MULTIPLE GOUGES FROM FWD OF FR23 TO FR34 AS MARKED (C-CHECK RO 10/4/2022) REMOVED AND REPLACED CFI R/H INBOARD SEAT TRACK FR23 TO FR34 REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE CHANGE REQUIRED.Sep 15, 2022 · N171SY · Emb EMB110* · Fuselage, Powerplant Attach FittingsSDR SWIA2020022748854Doubler · corrodedCORROSION IN L/H O/B DOUBLER BETWEEN FR.87-88. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED CORRODED LH O/B DOUBLER BETWEEN FR87-88 REF SRM. SEE CONTINUATION CARD FOR DETAILS.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2020022748853Floor Support · corrodedCORROSION IN R/H FLOOR SUPPORT BETWEEN FR.90-90A. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H FLOOR SUPPORT BETWEEN FR.90-90A PER REF: SRM APPLIED SURFACE PROTECTION PER REF: SRM, APPLIED CIC PER REF: CPM SEE CONTINUATION CARD FOR WORK PREFORMEDFeb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748852Seat Track · corrodedCORROSION IN L/H SEAT TRACK FR.84. (C-CHECK) RO 2/22/2020 REMOVED CORROSION ON AFT END OF OTBD CROWN CORNER ON L/H SEAT TRACK AT FR.84. DAMAGE AREA: L = 0.296" X W = 0.093" X D = 0.100". CROWN NOMINAL: 0.354". REMAINING MATERIAL: 0.344". REF EMB SRM. CALIFeb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020022748851Floor Support · corrodedCORROSION IN R/H O/B SILL FROM FR.88-90. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H O/B SILL FROM FR.88-90. PER REF: SRM SEE CONTINUATION CARD FOR WORK PREFORMEDFeb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748850Structure · corrodedCORROSION IN R/H O/B SILL FR.84. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H O/B SILL FR.84. PER REF: SRM SEE CONTUINUATION CARD FOR WORK PREFORMEDFeb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748849Floor Support · corrodedCORROSION IN L/H FLOOR SUPPORT FR.87. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED L/H FLOOR SUPPORT FR.87. PER REF: SRM SEE CONTINUATION CARD FOR WORK PREFORMEDFeb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748848Structure · corrodedCORROSION IN R/H O/B SILL FR.17. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED ON R/H O/B SILL FR 17-21 , REF. SRM AND RESTORED SURFACE PROTECTION RIVETS HEAD , REF. SRM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748847Structure · corrodedCORROSION IN R/H O/B SILL FR.14. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H O/B SILL FR.14. REF SRM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748846Floor Support · crackedCRACK IN R/H FLOOR SUPPORT FR.86. (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H FLOOR SUPPORT FR.86 PER REF SRM. APPLIED SURFACE PROTECTION PER REF SRM APPLIED CIC PER CPM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748845Angle · crackedCRACK IN ANGLE FR.12 LBL 38". (C-CHECK) RO 2/22/2020 REMOVED , LOCATED, DRILLED AND INSTALLED FR 12 ANGLE AT LBL 38 PER SRM AND SRM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748844Angle · crackedCRACK IN ANGLE FR.12 AT BL 0". (C-CHECK) RO 2/22/2020 REMOVED , LOCATED, DRILLED AND INSTALLED FR 12 ANGLE AT BL0 PER SRM AND SRM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA2020022748842Skin · corrodedCORROSION IN FR.84 RBL 27". (C-CHECK) RO 2/22/2020 REMOVED CORROSION AT FR 84 RBL 27" . INSTALLED DOUBLER AND FILLER REF ETD.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Plate/SkinSDR SWIA2020022748841Frame · corrodedCORROSION IN FR.84 LBL 32". (C-CHECK) RO 2/22/2020 COMPLIED WITH INSTALL OF OUTER DOUBLER AND REINFORECEMNT L ANGLE ON FR 84 LBL 32" PER ETD- SEE CONTINUATION CARD FOR WORK ACCOMPLISHED. THIS REPAIR DOES NOT ADVERSELY AFFECT A FATIGUE CRITICAL STRFeb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, FrameSDR SWIA2020022748840Seat Track · corrodedCORROSION IN R/H SEAT TRACK FR.84. (C-CHECK) RO 2/22/2020 SPLICE IN NEW R/H SEAT TRACK FR.84 REF ETD.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020022748839Seat Track · corrodedCORROSION IN L/H BEAM FR.18-20 LBL 10". (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED LH SEAT TRACK BEAM FR 12-FR20 REF EMB SRM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020022748838Seat Track · corrodedCORROSION IN R/H BEAM FR.16-20 RBL 10". (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED R/H BEAM FR.16-20 RBL 10". REF EMB SRM.Feb 7, 2020 · N171SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2020022748843Attach Angle · crackedLH ATTACH ANGLE AT FRAME 52 CRACKED (C-CHECK) RO 2/22/2020 REMOVED AND REPLACED LH ATTACH ANGLE AT FRAME 52 REF EMB SRMFeb 6, 2020 · N171SY · Emb ERJ170200LR · Fuselage Main, Attach Fittings
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