# SDR AWXA200600933

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 18, 2006
- Submitted: June 12, 2006
- Operation: Air carrier
- Aircraft: [N625AW](https://openairdocs.org/aircraft/N625AW), registered now
- Make and model: Airbus A320-231
- Registry model: [Airbus A320-231](https://openairdocs.org/model/airbus-industrie-a320-231) (OpenAirDocs)
- Aircraft serial: 064
- Aircraft time: 52,979 hours, 23,723 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Part number: D53480022200
- Condition: Corroded
- Location: Fuselage
- 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/AWXA200600933

## Discrepancy

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION LOCATED ON FUSELAGE SKIN UNDER SCUFF PLATE AREA AT THE L2 DOOR, STR 23L, Y1340 AND FR 65+5 INCHES TO FR 65+5.5 INCHES.  NO ALLOWABLE LIMITS IN THE SRM.  MAINTENANCE REWORKED AREA ON FUSELAGE SKIN UNDER THE SCUFF PLATE AT THE L2 DOOR FROM FR 65+5 INCHES TO FR 65+5.5 INCHES AT STR 23L AND Y1340 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR 26-5341-06151-SS1.

---
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.