# SDR DALA1134813218

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 16, 2011
- Submitted: May 17, 2011
- Operation: Air carrier
- Aircraft: [N318US](https://openairdocs.org/aircraft/N318US), registered now
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Aircraft serial: 206
- Aircraft time: 61,667 hours, 27,104 cycles
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Skin
- Condition: Corroded
- Location: Aft 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/DALA1134813218

## Discrepancy

AFT FUSELAGE SKIN AROUND VACUUM VENT HAS CORROSION.  REMOVED CORROSION IAW SRM 51-74-00.  REMAINING MATERIAL OUT OF LIMITS PER SRM 53-41-11.  REMOVED EXISTING FASTENERS PER SRM 51-42-11.  CUT OUT DAMAGED SKIN AREA IAW SRM 53-41-11.  FABRICATED DOUBLER AND FILLERS PER SRM 53-41-11.  LOCATED AND DRILLED PER SRM 53-41-11 FIG 205.  INSTALLED DOUBLER AND FILLERS IAW SRM  53-41-11 FIG 205.

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