# Service difficulty reports that cite it: Boeing SB 737-53-1182

A list on [Boeing SB 737-53-1182](https://openairdocs.org/service-documents/boeing/sb-737-53-1182.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 SROM200700006](https://openairdocs.org/sdr/SROM200700006.md): Frame · Boeing 737205 · Aug 1, 2007 · N736BP · Revision R1
  > NR63-CRACK ON BODY FRAME INNER CHORD BS616 RT SIDE AT STUB BEAM LOWER CHORD ATTACH (ABOVE WING BOX BL64R). DAMAGE OF BODY FRAME INNER CHORD STA 616 RT SIDE AT STUB BEAM LOWER CHORD ATTACH REMOVED IAW
- [SDR PIDR2006033](https://openairdocs.org/sdr/PIDR2006033.md): Frame · Boeing 737301 · Oct 16, 2006 · N573US · No revision named
  > CRACK IN BS 616 FRAME RT SIDE BELOW FLOOR. REPAIRED DAMAGED AREA IAW SB 737-53-1182.
- [SDR PIDA06114](https://openairdocs.org/sdr/PIDA06114.md): Frame · Boeing 7374B7 · Sep 12, 2006 · N447US · No revision named
  > CRACK AT FRAME STA 616 RBL 64 JUST BELOW FLOOR LEVEL. REPAIRED IAW SB 737-53-1182 FIG 9.
- [SDR PIDA06087](https://openairdocs.org/sdr/PIDA06087.md): Attach Angle · Boeing 7374B7 · Aug 9, 2006 · N448US · No revision named
  > STA 601 BEAM AFT SIDE OF FWD OVERWING EXIT HAS A CRACKED ATTACH ANGLE. REPAIRED PER EA 53-219 AND SB 737-53-1182.
- [SDR PIDA06088](https://openairdocs.org/sdr/PIDA06088.md): Frame · Boeing 7374B7 · Aug 9, 2006 · N448US · No revision named
  > INBOARD CHORD OF STA 601R FRAME IS CRACKED AT BOTTOM FASTENER. REPAIRED PER SB 737-53-1182 AND EA 53-217.
- [SDR PIDA20050150](https://openairdocs.org/sdr/PIDA20050150.md): Frame · Boeing 737228 · Sep 28, 2005 · N251TR · No revision named
  > CRACK AT I/B CHORD LOWER FASTENER HOLE IN BS 616 FRAME LEFT. REPAIRED FRAME PER SB 737-53-1182.
- [SDR DL73K011088](https://openairdocs.org/sdr/DL73K011088.md): Frame · Boeing 737232 · Jun 29, 2001 · N317DL · No revision named
  > CRACKS WERE FOUND AT THE BOTTOM TWO FASTENERS ON THE INNER CCHORD OF THE LEFT FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM JOINT. THE CRACKS ARE TYPICAL OF THAT SHOWN IN S/B 737-53-1182. THE CRACKS
- [SDR AWXA0001830](https://openairdocs.org/sdr/AWXA0001830.md): Frame · Boeing 73733A · Jun 5, 2001 · N168AW · No revision named
  > fuselage frame inner chord cracked at FLOORBEAM attach point left side BS 616. cut out damaged area; FABBED repair angle and filler; drilled, treated, primed and installed repair IAW BOEING S/B 737-53
- [SDR AWXA0001806](https://openairdocs.org/sdr/AWXA0001806.md): Frame · Boeing 7373G7 · Jun 4, 2001 · N156AW · No revision named
  > FWD SIDE OF FUSELAGE FRAME CRACKED ABOVE CENTER WING BS 616 LBL 65. TRIMMED OUT DAMAGE; INSTALLED REPAIR ANGLE AND FILLER IAW AWA ER 03-5311-01130-DL2 AND SB 737-53-1182.
- [SDR DL73K010869](https://openairdocs.org/sdr/DL73K010869.md): Frame · Boeing 737232 · May 30, 2001 · N320DL · No revision named
  > A CRACK WAS FOUND IN THE LOWER FASTENER HOLE OF BOTH THE LT AND RT FS 616 FRAME TO STUB BEAM. THE CRACK WAS REMOVED AND REPAIRED PER S/B 737-53-1182 AT HMV.
- [SDR DL73K010230](https://openairdocs.org/sdr/DL73K010230.md): Frame · Boeing 737232 · Feb 9, 2001 · N315DL · No revision named
  > A CRACK WAS FOUND AT THE LOWER FASTENER ON THE LEFT SIDE OF THE FS 616 FRAME AT THE OVERWING FRAME TO STUB BEAM. THE CRACK IS TYPICAL TO THAT SHOWN ON S/B 737-53-1182. THE DAMAGE WAS REPAIRED PER S/B
- [SDR AWXA0001266](https://openairdocs.org/sdr/AWXA0001266.md): Frame · Boeing 7373G7 · Feb 7, 2001 · N157AW · No revision named
  > FUSELAGE FRAME INNER CHORD CRACKED STA 616 LBL 65. REPAIRED IAW SERVICE BULLETIN 737-53-1182.
- [SDR AWXA0001267](https://openairdocs.org/sdr/AWXA0001267.md): Frame · Boeing 7373G7 · Feb 7, 2001 · N157AW · No revision named
  > FUSELAGE FRAME INNER CHORD CRACKED STA 616 RBL 65. REPAIRED IAW SERVICE BULLETIN 737-53-1182.
- [SDR DL73K010018](https://openairdocs.org/sdr/DL73K010018.md): Frame · Boeing 737232 · Jan 5, 2001 · N313DL · No revision named
  > A CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT SIDE FS 616 FRAMES AT THE OVERWING FRAME TO STUB JOINT. THIS IS THE TYPICAL CRACK OF S/B 737-53-1182. THE CRACK WAS CUT
- [SDR DL73K002106](https://openairdocs.org/sdr/DL73K002106.md): Frame · Boeing 737232 · Oct 25, 2000 · N310DA · No revision named
  > A CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT FS 616 FRAMES AT THE OVERWING FRAME TO BEAM JOINT STUB. ERA 396361-14 AUTHORIZES A REPAIR SIMILIAR TO THAT OF SB 737-53
- [SDR DL73K001336](https://openairdocs.org/sdr/DL73K001336.md): Frame · Boeing 737232 · Jul 17, 2000 · N308DL · No revision named
  > ONE CRACK WAS FOUND IN EACH OF THE LEFT AND RIGHT FS 616 IN THE LOWER FASTENER OF THE INNER CHORD AT FRAME TO STUB BEAM JOINT. THE CRACKS WERE 1.25 INCH IN LENGTH AND WERE TYPICAL TO THOSE SHOWN IN S/
- [SDR DL73K001276](https://openairdocs.org/sdr/DL73K001276.md): Frame · Boeing 737232 · Jul 7, 2000 · N305DL · No revision named
  > A CRACK WAS FOUND IN THE LOWER FASTENER OF THE INBOARD CHORD OF THE FS 616 JUST BELOW THE CABIN FLOOR. THE CRACK IS SIMILIAR TO THAT OF S/B 737-53-1182. ADDITIONALLY, A PILOT HOLE FROM THE FACTORY WAS
- [SDR USAA990810](https://openairdocs.org/sdr/USAA990810.md): Frame · Boeing 737301 · Aug 3, 1999 · N341US · No revision named
  > CLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A.50 INCH CRACK BOTTOM END OF FRAME STA 616 INBOARD CHORD ANGLE RT SIDE FRAME. INSTALLED FILLER AND DOUBLER PER SB 737-53-1182 AND EA 64972. (X)
- [SDR 98ZZZM499](https://openairdocs.org/sdr/98ZZZM499.md): Frame · Boeing 73733A · Jun 7, 1998 · N172AW · No revision named
  > DURING 'C' CHECK INSPECTION DISCOVERED CRACKING CONDITIONS ON THE BOTTOM OF THE INNER FRAME CHORD ON BOTH LEFT (LBL 70.53) AND RIGHT (RB 70.53) SIDES OF THE AIRCRAFT AT BS 616. REPAIRED BY INSPECTING
- [SDR W8PA970613](https://openairdocs.org/sdr/W8PA970613.md): Frame · Boeing 7373B7 · May 22, 1997 · N951WP · No revision named
  > CRACK IN FRAME INNER CHORD BS 616, RBL 665, WL 201. CRACK WAS REPAIRED PER SB 737-53-1182. (X)
- [SDR W8PA970744](https://openairdocs.org/sdr/W8PA970744.md): Frame · Boeing 7373L9 · May 22, 1997 · N960WP · No revision named
  > FOUND BS 616 RBL 65, WL 201 CRACK ON FRAME INNER CHORD BY LOWER FASTENER. CUT OUT DAMAGE AREA OF FRAME INNER CHORD. FABRICATED REPAIR ANGLES AND FILLER AND INSTALLED. ALL WORK DONE IAW SB 737-53-1182

## 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-737-53-1182' 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-737-53-1182/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.
