# SDR AWXA200300762

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 16, 2003
- Submitted: July 1, 2003
- Operation: Air carrier
- Aircraft: N620AW
- Make and model: Airbus A320-231
- Registry model: [Airbus A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (OpenAirDocs)
- Aircraft serial: 052
- Aircraft time: 44,107 hours, 20,093 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Stiffener
- Part number: D53370039201
- Condition: Cracked
- Location: Floor Support
- Stage of operation: IN
- How discovered: V
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/AWXA200300762

## Discrepancy

DURING C-04 CHECK A .5 INCH CRACK WAS FOUND ON LT OUTBOARD FLOOR SUPPORT SIDE RAIL STIFFENER (PROFILE) FR 37, Y-1732.  MAINTENANCE REMOVED DAMAGED PROFILE FR 37, Y-1732; FABRICATED A NEW REPLACEMENT PROFILE PER DWG D53370039; INSTALLED REPAIR PART IAW A320 SRM 51-42-11 PG 26-30 & 35 FIG 10-12.

---
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.
