# SDR WRNA200600019

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 18, 2006
- Submitted: June 21, 2006
- Operation: Air carrier
- Aircraft: [N821SC](https://openairdocs.org/aircraft/N821SC), registered now
- Make and model: Airbus A300 B4-203
- Registry model: [Airbus A300 B4-203](https://openairdocs.org/model/airbus-industrie-a300-b4-203) (OpenAirDocs)
- Aircraft serial: 211
- Aircraft time: 50,653 hours, 20,839 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- 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/WRNA200600019

## Discrepancy

DURING INSPECTION, CORROSION WAS FOUND ON FUSELAGE SKIN ABOVE THE RT FORWARD PASSENGER DOOR, TWO AREAS, AT S9L BETWEEN FR 14C AND FR 14B AND 1 AREA AT S11L BETWEEN FR13 AND FR13A.  ACCOMPLISHED REPAIR PER AVBORNE REPAIR REFERENCE 25599-7-02-02-2006, (AIRBUS REPAIR DESIGN APPROVAL SHEET RAS/AS/028/2006) PERFORMED SMOOTH REWORK OF CORRODED AREAS, PERFORMED INSPECTIONS, ROTOTEST AND DVI OF HOLES IN CORRODED AREAS, HFEC AND DVI OF CORRODED AREAS, INSTALLED OVERSIZE FASTENERS IN CORRODED AREAS AND RE-PROTECT PER SRM.

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