# Service difficulty reports that cite it: Boeing SB 727-53-0183

A list on [Boeing SB 727-53-0183](https://openairdocs.org/service-documents/boeing/sb-727-53-0183.md).

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.

- [SDR DHL2002721505](https://openairdocs.org/sdr/DHL2002721505.md): Skin · Boeing 727228 · Aug 6, 2002 · N721DH · No revision named
  > DURING 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
- [SDR C7WA200200024](https://openairdocs.org/sdr/C7WA200200024.md): Skin · Boeing 727232 · Jul 13, 2002 · N511PE · No revision named
  > DURING 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 72
- [SDR C7WA200200025](https://openairdocs.org/sdr/C7WA200200025.md): Skin · Boeing 727232 · Jul 13, 2002 · N511PE · No revision named
  > DURING 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 II
- [SDR DHL9770114C](https://openairdocs.org/sdr/DHL9770114C.md): Skin · Boeing 72730C · Apr 25, 1997 · N701DH · No revision named
  > DURING 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
- [SDR B4MR96001](https://openairdocs.org/sdr/B4MR96001.md): Skin · Boeing 727191 · Aug 12, 1996 · N503MG · No revision named
  > DURING 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.
- [SDR 95ZZZX4362](https://openairdocs.org/sdr/95ZZZX4362.md): Skin · Boeing 727225 · Aug 2, 1995 · N352PA · No revision named
  > VISUAL 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 SI

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/service-documents/boeing/sb-727-53-0183/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain, except the copies of manufacturers’ service documents, which belong to their rights holders.