# SDR AWXA200600938

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 17, 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 Panel
- Part number: D53231318200
- 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/AWXA200600938

## Discrepancy

SAL - MAJOR REPAIR - DURING C6 CHECK DISCOVERED CORROSION ON EXISTING REWORKED AREA AT FR 25 TO FR 26 AND STR 41R TO STR 42R.  CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS.  MAINTENANCE CUT OUT DAMAGED AREA IAW AIRBUS 320 SRM 53-00-11.  INSTALLED FABRICATED DOUBLER AND FILLER AT FR 25 TO FR 26 AND STR 41R TO STR 42R IAW AIRBUS 320 SRM 53-00-11 FIG 212.

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