N240SY

Service difficulty reports · 21

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 = 'N240SY' 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 SWIA2025031106Shutoff Valve · faultedGOT CABIN ALTITUDE HI WARNING MESSAGE WHEN DESCENDING THROUGH FL210 CABIN ALTITUDE INCREASED TO 12000. WENT THROUGH THE QRC AND QRH PERFORMED EMERGENCY DESCENT, MESSAGE EXTINGUISHED UPON REACHING 10,000. (FLIGHT 3863) REMOVED AND REPLACED LH NAPRSOV AND Mar 6, 2025 · N240SY · Emb ERJ170200LR · Cabin Pressure Control SystemSDR SWIA20250307006Warning Message · illuminatedGOT CABIN ALTITUDE HI WARNING MESSAGE WHEN DESCENDING THROUGH FL210 CABIN ALTITUDE INCREASED TO 12000. WENT THROUGH THE QRC AND QRH PERFORMED EMERGENCY DESCENT, MESSAGE EXTINGUISHED UPON REACHING 10,000. (FLIGHT 3863 - FILED OPEN) THIS IS CURRENTLY A WORMar 6, 2025 · N240SY · Emb ERJ170200LR · Cabin Pressure Control SystemSDR SWIA2024112210301Floor Support · gougedCENTER FUSELAGE III, RH FLOOR BEAM Y=+273MM FROM FR74 TO FR79 HAS GOUGES IN CENTER OF SEAT TRACK IN SEVERAL PLACES (C-CHECK RO 11/21/2024) REMOVED AND REPLACED CENTER FUSELAGE III, RH FLOOR BEAM Y=+273MM FROM FR74 TO FR79 REF EMB 175 SRM 51-40-08.Oct 30, 2024 · N240SY · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR SWIA202411221029Seat Track · gougedRH LATERAL SEAT TRACK HAS GOUGES IN SEVERAL AREAS FROM FR74 TO FR83 (C-CHECK RO 11/21/2024) REMOVED AND REPLACED RH LATERAL SEAT TRACK FROM FR74 TO FR83 REF EMB 175 SRM 51-40-08Oct 29, 2024 · N240SY · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202163811None · crackedFRAME CLIP CRACKED ON COCKPIT FLOOR AT FR12 AND LEFT BUTT LINE 36". (C CHECK RO 1/14/2022) REMOVED AND REPLACED FRAME CLIP AT FR 12 AND LEFT BUTT LIN 36". REF EMB SRM 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.Dec 28, 2021 · N240SY · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR SWIA202163810None · crackedFRAME CLIP CRACKED ON COCKPIT FLOOR AT FR12 AND CENTER BUTT LINE. (C CHECK RO 1/14/2022) REMOVED AND REPLACED FRAME CLIP AT FR 12 CENTER BUTT LINE. REF 51-40-08. SEE CONTINUATION FOR WORK PERFORMED.Dec 28, 2021 · N240SY · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR SWIA202163802None · damagedL/H WING FLAP TRACK 1A HAS DEPTH REDUCTION DAMAGE OF .039" WITH MAX ALLOWABLE DEPTH OF .068". DAMAGE IS IN ALLOWABLE LIMITS, BUT WILL REQUIRE AN INSPECTION INTERVAL EVERY 200FC PER SRM 57-52-03/AD01. ASSET# TC2-7153 CAL DUE 11-18-22. (C CHECK RO 1/14/2022) Dec 28, 2021 · N240SY · Emb ERJ170200LR · AileronsSDR SWIA202163809None · crackedL/H WHEEL WELL FR 52 ANGLE CRACKED. (C CHECK RO 1/14/2022) REMOVED AND REPLACED L/H WHEEL WELL FR 52 ANGLE REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR DETAILSDec 27, 2021 · N240SY · Emb ERJ170200LR · Fuselage Structure (General)SDR SWIA202163808None · corrodedCORROSION, AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRAME 86 BETWEEN STRINGERS 28R AND 27R. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FDec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Main, Longeron/StringerSDR SWIA202163807None · crackedAFT WET AREA, LH AND RH PANEL SUPPORTS ARE CRACKED/BROKEN OFF ON FRAME 86 FLOOR CROSS BEAM. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH AND RH FLOOR PANEL SUPPORTS ON AFT WET AREA, FRAME 86. / SEE CONTINUATION CARD FOR WORK PERFORMED. REF SRM 51-40-Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal StairsSDR SWIA202163806None · corrodedCORROSION - LH SILL AT FR19 (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH SILL AT FR19 REF EMB SRM 51-40-08Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163805None · noneCORROSION, AFT WET AREA, ON LH SPLICE PLATE AT FRAME 89. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH SPLICE PLATE AT FRAME 89 REF EMB SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF EMB SRM 51-23-06Dec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163804None · corrodedCORROSION, AFT WET AREA, ON RH SHEAR PANEL BETWEEN FRAMES 86 AND 87 AROUND GALLEY MOUNT POINTS AND ALONG FORWARD EDGE (C CHECK RO 1/14/2022) / REMOVED AND REPLACED RH SHEAR PANEL BETWEEN FRAMES 86 AND 87 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WORDec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163803None · corrodedCORROSION, AFT WET AREA, ON CENTER SHEAR PANEL BETWEEN FRAMES 86 AND 87 AROUND GALLEY MOUNT POINT AND FORWARD EDGE. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED CENTER SHEAR PANEL BETWEEN FRAMES 86 AND 87 REF EMB SRM 51-40-08 SEE CONTINUATION CARD FOR WODec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163800None · corrodedCORROSION, AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRAME 88 BETWEEN STRINGERS 28R AND 27R. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FDec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163799None · corrodedCORROSION, AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRAME 85 BETWEEN STRINGERS 28R AND 27R. (C CHECK RO 1/14/2022) / REMOVD AND REPLACED AFT WET AREA INTERNAL SIDE OF FUSELAGE BELOW FLOOR, ON SHEAR CLIP ATTACHED TO FRADec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163798None · corrodedCORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM FORWARD OF FRAME 87 IN AN ELONGATED SCREW HOLE. (C CHECK RO 1/14/2022) / REMOVED AND REPLACED RH LONGITUDINAL FLOOR BEAM FORWARD OF FRAME 87. BEAM WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BADec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163797None · corrodedCORROSION - LH I/B SEAT TRACK BETWEEN FR19/20 (C CHECK RO 1/14/2022) / REMOVED AND REPLACED LH I/B SEAT TRACK BETWEEN FR19/20 REF EMB SRM 51-40-08. PART WAS REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCEDec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage, Powerplant Attach FittingsSDR SWIA202163796None · corrodedCORROSION, 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 1/14/2022) / REMOVED AND REPLACED LH LONGITUDINAL FLOOR BEAM AT FRAME 87 REF EMB SRM 51-40-08 SEE CONTINUATION CARDec 26, 2021 · N240SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWIA202163801None · gougedPILOT SEAT, I/B SEAT TRACK HAS GOUGE ON THE FWD STOP/ RAMP AS MARKED (C CHECK RO 1/14/2022) REMOVED AND REPLACED PILOT SEAT IB SEAT TRACK. REF AMM 53-06-01Dec 23, 2021 · N240SY · Emb ERJ170200LR · Fuselage, Powerplant Attach FittingsSDR SWIA202158375A/C Pack · seizedFA HEARD A POP AND NOTICED HAZE IN THE CABIN APPROX 3 MINS AFTER TAKEOFF. OFF SMELL WAS NOTED, NOT SMOKE. SMELL AND HAZE DISSIPATED WITHIN A MINUTE. SMELL AND HAZE WAS NOTED AGAIN AFTER LANDING. (FLIGHT 3732 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERMay 23, 2021 · N240SY · Emb ERJ170200LR · Cabin Cooling System
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