# SDR DALA1130373252

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 30, 2011
- Submitted: May 2, 2011
- Operation: Air carrier
- Aircraft: [N352NW](https://openairdocs.org/aircraft/N352NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 778
- Aircraft time: 40,495 hours, 18,096 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/DALA1130373252

## Discrepancy

FUSELAGE FROM FR 69 TO 70 AROUND VACUUM OUTLET HAS CORROSION.  BLENDED AREA IAW SRM 51-73-00. DIM; L=1.0" W=0.3" D=0.009" OUT OF LIMITS IAW SRM 53-41-11.  CUT OUT IAW SRM 53-41-11 FIG 205.  FABBED REPAIR PARTS IAW SRM 53-41-11.  PERFORMED HFEC IAW NTM 51-00-08, INSTALLED REPAIR PARTS IAW SRM 51-42-11 & SRM 53-41-11, REPAIRED IAW SRM 53-41-11.  FIRST INSP AFTER REPAIR REQ AT 53900 FC & SUB INSP AT INTERVALS OF 18000 FC.

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