# SDR DALA13006333214

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 5, 2013
- Submitted: February 6, 2013
- Operation: Air carrier
- Aircraft: N314US
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Aircraft serial: 160
- Aircraft time: 67,439 hours, 30,165 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/DALA13006333214

## Discrepancy

DURING INSPECTION, FOUND RT AFT FUSELAGE LAV VENT HAS CORROSION ON SKIN SURFACE. PERFORMED REPAIR IAW SRM 53-41-11 FIG 205.  BLENDED AREA IAW SRM 51-74-00.  CHECKED LIMITS DEPTH: 0.011" MAX ALLOW 0.06" FOUND TO BE OUT OF LIMITS IAW SRM 53-41-11, DIAGRAM 102 SHEET 1, CUT OUT DAMAGE SKIN IAW SRM 53-41-11, STEP 2E; FABRICATED REPAIR PARTS 1EA DOUBLER MAT 2024-T3. .071C BATCH 000213529 AND 2 EA FILLER MAT 2024-T3 .063C BATCH 0002339436 IAW SRM 53-41-11; INSTALLED REPAIR PARTS IAW SRM 51-42-11 & SRM 53-41-11 DIMENSION OF CUT OUT L; 2" W; 1".

---
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.