Airbus SB A300-57-6049

Service difficulty reports that cite it · 7

Newest first, with the revision each cites, as OpenAirDocs read it from the records’ text. OpenAirDocs read these citations from the records’ text, so one can be misread: check it against the record. A newer revision may exist that no record cites.

Query with SQL
duckdb -csv -c "SELECT s.sdr_id, s.difficulty_date, s.aircraft_make, s.aircraft_model, s.part_name, string_agg(DISTINCT c.revision, ', ' ORDER BY c.revision) AS revisions,
    bool_or(c.incorporated_by_reference) AS incorporated_by_reference, bool_or(c.in_regulatory_text) AS in_regulatory_text
  FROM 'https://openairdocs.org/data/latest/service_document_citation.parquet' c JOIN 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' s ON s.sdr_id = c.record_id
  WHERE c.document_id = 'airbus/a300-57-6049' AND c.record_type = 'faa_service_difficulty_report'
  GROUP BY ALL
  ORDER BY max(c.record_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 FDEA202203020387None · Airbus A300*RH WING REAR SPAR HOLE 5 (E) BUSHING-REMOVE/NSTALL FOR ROTATING PROBE INSPECTION. I.A.W A300-600 SRM 51-72-20-201 REMOVE BUSHING ACCOMPLISHED. I.A.W EA NO.6-5710-161497 TITLE:WINGS-AD2005-23-08-MAIN FMar 2, 2022 · N730FD · No revision namedSDR FDEA202009202270Web · Airbus A300F4605RDURING THE ACCOMPLISHMENT OF STEP (9)(C) OF EO 6-5710-E0342809 P5 (LT WING), A CRACK NDICATION WAS NOTED APPROXIMATELY .500" FROM THE BOTTOM OF HOLE G AT THE 7 O'LOCK POSITION. CRACK MEASURES APPROXIMSep 20, 2020 · N668FE · No revision namedSDR FDEA201501140164Fitting · Airbus A300F4605RRIGHT FUSE CTR WING BOX OF REAR SPAR N HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0314943 P1 TITLE:WINGS-BASIC WING STRUCTURE -AD 2014- 20-18-FR47 RT FASTENER HOLES CRACKED (SB A300-57-6049 R06Jan 14, 2015 · N672FE · Revision R06SDR FDEA201501140165Fitting · Airbus A300F4605RRIGHT FUSE CTR WING BOX OF REAR SPAR I HOLE FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0314943 P1 TITLE:WINGS-BASIC WING STRUCTURE -AD 2014- 20-18-FR47 RT FASTENER HOLES CRACKED (SB A300-57-6049 R06Jan 14, 2015 · N672FE · Revision R06SDR 08FDEA03975Fitting · Airbus A300B4622RFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE N, Y, U) ON VERTICAL FLANGE, C 47, LHS. REPAIR PERFORMED BY OVERSIZING THE HOLES OF EXTERNAL FITTING AND INSTALL A CONICAL WASHER AT Sep 22, 2008 · N744FD · No revision namedSDR 08FDEA03976Fitting · Airbus A300B4622RFOUND DAMAGED HOLES DURING ACCOMPLISHMENT OF SB A300-57-6049 (HOLE I, L, N, U) ON VERTICAL FLANGE, C 47, RHS. REPAIR PERFORMED BY OVERSIZING THE HOLES, EXTERNAL FITTING CUT OUT AT HOLE I AND NDT FOR DSep 22, 2008 · N744FD · No revision namedSDR 07FDEA03005Fitting · Airbus A300B4622RFINDING CRACKS DURING ACCOMPLISHMENT OF SB A300-57-6049 AND A300-57-6086 IN CENTER WING BOX CORNER ANGLE FITTING (HOLE A (LT/RT), Q, G , I (LT). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA Aug 21, 2007 · N726FD · No revision named
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