Boeing SB 727-53-0183

Service difficulty reports that cite it · 6

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 = 'boeing/sb-727-53-0183' 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 DHL2002721505Skin · Boeing 727228DURING C-CHECK DISCREPANCY AS FOLLOWS, FUSELAGE SKIN CRACKED SECTION 41 LEFT SIDE BS 243 WL 215. CUTOUT CRACKED SECTION OF FUSELAGE SKIN IAW B-727 SRM 53-30-3. FABRICATED REPAIR DOUBLER IAW B-727 SRM Aug 6, 2002 · N721DH · No revision namedSDR C7WA200200024Skin · Boeing 727232DURING C-CHECK INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACK AT BS 203.8 BETWEEN RIGHT WL 219 AND WL 220. REPAIRED FUSELAGE SKIN FROM BS 191.0 TO BS 209.0 BETWEEN WL 214 AND 224.5 RBL 38.0 IAW S/B 72Jul 13, 2002 · N511PE · No revision namedSDR C7WA200200025Skin · Boeing 727232DURING C-CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN CRACK AT BS 196.5 WL 217. REPAIRED FUSELAGE SKIN FROM BS 191.5 TO BS 203.0 BETWEEN WL 212.5 AND WL 222.5 LBL 38.0 IAW S/B 727-53-0183 SECTION IIJul 13, 2002 · N511PE · No revision namedSDR DHL9770114CSkin · Boeing 72730CDURING C-CHECK, THE RIGHT SIDE OF FUSELAGE SKIN WAS FOUND CRACKED AT FASTENERS AT W/L 218, BS 251.6 AND 227.8. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA AT W/L 218 STA 227.8 DIMENSIONS 2 BY 1 AND Apr 25, 1997 · N701DH · No revision namedSDR B4MR96001Skin · Boeing 727191DURING C1 CHECK, INSPECTION FOUND AD94-07-08 AGING AIRCRAFT REFERENCE SB 727-53-0183: HFEC INSPECTION REVEALED FIVE CRACK INDICATIONS AT FASTENERS MARKED ON RIGHT HAND SECTION 41 FUSELAGE SKIN BS 219.Aug 12, 1996 · N503MG · No revision namedSDR 95ZZZX4362Skin · Boeing 727225VISUAL INSPECTION OF RT SECTION 41 EXTERNAL SKIN PER AD 94-07-08 AND SB 727-53-0183 REVEALED 14 EACH CRACKED FASTENER HOLES (9 EACH AT BS 235, 5 EACH AT BS 243), 18 INCHES TO 28 INCHES BELOW RT AFT SIAug 2, 1995 · N352PA · No revision named
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