# Service difficulty reports that cite it: Boeing SB 737-53-1061

A list on [Boeing SB 737-53-1061](https://openairdocs.org/service-documents/boeing/sb-737-53-1061.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 AWXA200300608](https://openairdocs.org/sdr/AWXA200300608.md): Floorbeam · Boeing 737277 · May 14, 2003 · N178AW · Revision R4
  > DURING C-15 CHECK A 2 INCH CRACK WAS FOUND ON TRANSVERSE FLOORBEAM WEB OUTBOARD OF LBL 45.50, BS 639. MAINTENANCE REMOVED DAMAGED ON WEB AT LBL 45.50, BS 639; FABRICATED REPAIR DOUBLERS AND A STRAP PE
- [SDR AWXA200300638](https://openairdocs.org/sdr/AWXA200300638.md): Floorbeam · Boeing 737277 · May 14, 2003 · N178AW · No revision named
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A.25 INCH CRACK WAS ON FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50. MAINTENANCE REMOVED DAMAGED FLOORBEAM WEB ANGLE AT BS 639, LBL 45.50; FABRICATED A NEW REPLACEM
- [SDR AWXA200300609](https://openairdocs.org/sdr/AWXA200300609.md): Frame · Boeing 737277 · May 13, 2003 · N178AW · No revision named
  > YVR - MAJOR REPAIR - DURING C-15 CHECK A.25 INCH CRACK WAS FOUND ON LT FUSELAGE FRAME AT BS 639. MAINTENANCE REMOVED DAMAGED SECTION OF LT FUSELAGE FRAME AT BS 639; FABRICATED SPLICE REPAIR AND NEW S
- [SDR P2EA00145](https://openairdocs.org/sdr/P2EA00145.md): Beam · Boeing 737247 · Apr 28, 2000 · N912MP · No revision named
  > SJO - DURING C-CHECK, STUD BEAM WEB CRACKED AT BS 597, RBL 48 AND WL 204. REPAIRED STUD BEAM WEB AT BS 297 FROM RBL 45 TO RBL 56 AND BETWEEN WL 200 TO WL 208 IAW SB 737-53-1061 SECTION III PART III PA
- [SDR P2EA00154](https://openairdocs.org/sdr/P2EA00154.md): Beam · Boeing 737247 · Apr 28, 2000 · N912MP · Revision 4
  > SJO - DURING C-CHECK, FOUND CABIN STUB BEAM WEB AT BS 616 FROM RBL 45 TO RBL 56 BETWEEN WL 208 AND WL 200 HAS CRACK. L = 0.373 INCH. W = 0.0005 INCH. REPAIRED STUB BEAM AT BS 616 FROM RBL 45 TO RBL 56
- [SDR P2EA00155](https://openairdocs.org/sdr/P2EA00155.md): Beam · Boeing 737247 · Apr 28, 2000 · N912MP · Revision 4
  > SJO - DURING C CHECK, FOUND CABIN STUB BEAM WEB AT BS 639 FROM RBL 45 TO RBL 56 BETWEEN WL 208 AND WL 200 HAS CRACK. L = 0.373 INCH, W = O.0005 INCH. REPAIRED CABIN STUB BEAM WEB AT BS 639 FROM RBL 45
- [SDR P2EA00161](https://openairdocs.org/sdr/P2EA00161.md): Web · Boeing 737247 · Apr 28, 2000 · N912MP · Revision 4
  > SJO - DURING C-CHECK, FOUND STUB BEAM WEB BS 639 LBL 62 WL 204, WITH CRACK. L = 1.125 INCH. REPAIRED STUB BEAM WEB BS 639 LBL 62 WL 204, IAW BOEING SB 737-53-1061, REV 4 DATED 7-16-92 SECTION III, PAR
- [SDR P2EA00140](https://openairdocs.org/sdr/P2EA00140.md): Frame · Boeing 737247 · Apr 15, 2000 · N912MP · Revision 4
  > SJO - DURING C-CHECK, FRAME CRACKED AT BS 597, STR 17L. REPAIRED STR 17L AT BS 597 BETWEEN STR 15L AND WING CHORD IAW SB 737-53-1061 REV 4 SECTION III PART III. SEE COOPESA W/O N10316-2-199, VAM100 NR
- [SDR P2EA00141](https://openairdocs.org/sdr/P2EA00141.md): Frame · Boeing 737247 · Apr 15, 2000 · N912MP · Revision 4
  > SJO - DURING C-CHECK, FRAME CRACKED AT BS 597 STR 17R. REPAIRED FRAME FROM STR 15R TO WING CHORD IAW SB 737-53-1061 REV 4 SECTION III PARA II. SEE COOPESA W/O N10316-2-201, VAM100 NR 620, 912SDA125 AN
- [SDR P2EA00053](https://openairdocs.org/sdr/P2EA00053.md): Beam · Boeing 737222 · Feb 5, 2000 · N603DJ · Revision 4
  > SJO - DURING Q-CHECK, STUD BEAM WEB CRACKED AT BS 639. REPAIRED STUD BEAM WEB AT BS 639, BETWEEN LBL 46 AND LBL 56.5 AND FROM WL 200 TO WL 208 IAW SB 737-53-1061 REV 4 PART III FIG 2 DATED JULY 16, 19
- [SDR P2EA00052](https://openairdocs.org/sdr/P2EA00052.md): Frame · Boeing 737222 · Jan 27, 2000 · N603DJ · Revision 4
  > SJO - DURING Q-CHECK, FRAME WEB CRACKED AT BS 639, BETWEEN 16L AND 17L. REPAIRED FRAME WEB AT BS 639 IAW SB 737-53-1061, REV 4 DATED JULY 16, 1992. (M)
- [SDR AWXA9900294](https://openairdocs.org/sdr/AWXA9900294.md): Angle · Boeing 737277 · Aug 31, 1999 · N181AW · No revision named
  > C-CHECK, FLOORBEAM ATTACH ANGLE TO FUSELAGE AT STA 598 WL 208 LT CUSP LINE CRACK STR 17L. REMOVED, FABRICATED, AND INSTALLED REPAIR PARTS PER AWA ER 2-53-15-86 + SB 737-53-1061.
- [SDR P2EA99291](https://openairdocs.org/sdr/P2EA99291.md): Floorbeam · Boeing 737247 · Aug 23, 1999 · N204AU · Revision 4
  > SJO - FLOORBEAM WEB CRACKED AT BS 578 BETWEEN RBL 55 AND RBL 55 AT WL 206. REPAIRED IAW SERVICE BULLETIN 737-53-1061 REVISION 4. (M)
- [SDR ASAA9910177](https://openairdocs.org/sdr/ASAA9910177.md): Fitting · Boeing 737210C · Jun 25, 1999 · N743AS · No revision named
  > PHX - DURING SCHEDULED D-CHECK, THE OVERWING STUB FRAME ATTACH FITTING STATION 639 RBL 45.5 CRACKED WERE FRAME TIES INTO SEAT TRACK FRAME WEB. REPAIRED PER SB 737-53-1061. (M)
- [SDR P2EA98291](https://openairdocs.org/sdr/P2EA98291.md): Angle · Boeing 737281 · Nov 19, 1998 · N219US · Revision 4
  > SJO - ANGLE CRACKED AT BS 559, RBL 46, WL 205 DEFECT SIZE LENGTH.4375. REPLACED FUSELAGE LOWER CHORD AT BS 559, WL 204, BETWEEN RBL 46 INCHES AND RBL 70 INCHES PER BOEING SERVICE BULLETIN 737-53-1061

## 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-737-53-1061' 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-737-53-1061/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.