N176CA

Service difficulty reports · 109

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 = 'N176CA' 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 U2RA201211110002Web · crackedMAIN DECK BS 1660-1680, RBL 3 FLOOR WEB CRACKED ON FORWARD UPPER CORNER. CRACK LENGTH 1.2". REPLACED WEB, IAW DWG 146N5190.Nov 11, 2012 · N176CA · Boeing 75728A · Fuselage Miscellaneous StructureSDR U2RA201211110001Deck Plate · corrodedMAIN DECK BS 1680-1720 DECK PLATE HAS FIVE LOCATIONS OF HEAVY CORROSION, LENGTH = 50", WIDTH = 4", DEPTH= .035" ORIGINAL THICKNESS = .071". DECK PLATE, REPLACED FROM BS 1680-1720 LBL 58" - RBL 58".Nov 11, 2012 · N176CA · Boeing 75728A · Fuselage Floor PanelSDR U2RA201211090001Doubler · corrodedBS 1645, STRINGER 29L-29R SKIN DOUBLER HAS CORROSION. CORROSION AREA LENGTH .3", WIDTH .2", DEPTH .035", ORIGINAL THICKNESS .061". SKIN DOUBLER, REPLACED IAW DWG 146N3600.Nov 9, 2012 · N176CA · Boeing 75728A · Fuselage Main, Plate/SkinSDR U2RA201210110001Air Duct · crackedLOST PRESSURIZATION- REGAINED AT 10,000 FEET. FOUND AIR DUCT CRACKED.Oct 11, 2012 · N176CA · Boeing 757200 · Air Distribution SystemSDR U2RA201208200004Wedge · delaminatedNR 7 SLAT T/E WEDGE AFT EDGE DELAMINATION 33.75" FROM OTBD END AREA 2.1875" X 1.5". REF AD 91-22-51, SB 757-57-0066.Aug 16, 2012 · N176CA · Boeing 75728A · Leading Edge DevicesSDR U2RA201208200003Wedge · delaminatedNR 4 SLAT T/E WEDGE AFT EDGE DELAMINATED 30.5 FROM INBD END AREA .75 X 2.8750. REF AD 91-22-51, SB 757-57-0066.Aug 16, 2012 · N176CA · Boeing 75728A · Leading Edge DevicesSDR U2RA201208200002Wedge · delaminatedNR 3 SLAT T/E WEDGE DELAMINATED 30.5" FROM INBD END AT AFT EDGE AREA .8750" X 6". REF AD 91-22-51, SB 757-57-0066.Aug 16, 2012 · N176CA · Boeing 75728A · Leading Edge DevicesSDR U2RA201208200001Wedge · delaminatedNR 2 SLAT T/E WEDGE DELAMINATED ON AFT EDGE 28" FROM INBD EDGE AREA 1.1250" X 5.5". REF AD 91-22-51, SB 757-57-0066.Aug 16, 2012 · N176CA · Boeing 75728A · Leading Edge DevicesSDR U2RA2012072426801Compressor · stalledDURING CLIMB OUT AT 600 FT, NR 1 COMPRESSOR STALL.Jul 24, 2012 · N176CA · Boeing 75728A · Turbine Engine Compressor Section
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