# Service difficulty reports that cite it: Airbus SB A300-57-6049

A list on [Airbus SB A300-57-6049](https://openairdocs.org/service-documents/airbus/a300-57-6049.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 FDEA202203020387](https://openairdocs.org/sdr/FDEA202203020387.md): None · Airbus A300* · Mar 2, 2022 · N730FD · No revision named
  > 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 F
- [SDR FDEA202009202270](https://openairdocs.org/sdr/FDEA202009202270.md): Web · Airbus A300F4605R · Sep 20, 2020 · N668FE · No revision named
  > DURING 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 APPROXIM
- [SDR FDEA201501140164](https://openairdocs.org/sdr/FDEA201501140164.md): Fitting · Airbus A300F4605R · Jan 14, 2015 · N672FE · Revision R06
  > RIGHT 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 R06
- [SDR FDEA201501140165](https://openairdocs.org/sdr/FDEA201501140165.md): Fitting · Airbus A300F4605R · Jan 14, 2015 · N672FE · Revision R06
  > RIGHT 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 R06
- [SDR 08FDEA03975](https://openairdocs.org/sdr/08FDEA03975.md): Fitting · Airbus A300B4622R · Sep 22, 2008 · N744FD · No revision named
  > FOUND 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
- [SDR 08FDEA03976](https://openairdocs.org/sdr/08FDEA03976.md): Fitting · Airbus A300B4622R · Sep 22, 2008 · N744FD · No revision named
  > FOUND 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 D
- [SDR 07FDEA03005](https://openairdocs.org/sdr/07FDEA03005.md): Fitting · Airbus A300B4622R · Aug 21, 2007 · N726FD · No revision named
  > FINDING 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

## 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 = 'airbus/a300-57-6049' 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/airbus/a300-57-6049/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.