# SDR AWXA200501122

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 5, 2005
- Submitted: September 28, 2005
- Operation: Air carrier
- Aircraft: N634AW
- Make and model: Airbus A320-231
- Registry model: [Airbus A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (OpenAirDocs)
- Aircraft serial: 091
- Aircraft time: 50,658 hours, 22,530 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Sill
- Part number: D53475765200
- Condition: Corroded
- Location: Bs 60-62
- 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/AWXA200501122

## Discrepancy

SAL - MAJOR REPAIR - DURING C4 CHECK DISCOVERED GALVANIC CORROSION AROUND NUT PLATE LOCATED ON BULK CARGO DOOR SEAL FROM FS 60 TO FS 62 AT STRINGER 38R.  RE-WORK OF DAMAGED AREA WAS FOUND TO BE OUT OF LIMITS IAW AIRBUS 320 SRM 53-41-49 PG 103, FIG 101.  MAINTENANCE CUT OUT DAMAGED AREA FROM FS 60 TO FS 62 AT STRINGER 38R IAW AIRBUS 320 SRM 51-41-49 PAGE 203.  FABRICATED DOUBLER AND FILLER IAW AIRBUS 320 SRM 53-41-49.  INSTALLED FABRICATED REPAIR PARTS FROM FS 60 TO FS 62 AT STRINGER 38R IAW AIRBUS 320 SRM 51-42-11 AND 53-41-49 FIG 203.

---
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.
