# SDR DALA13006693214

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 10, 2013
- Submitted: February 11, 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): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Floor Support
- Condition: Corroded
- Stage of operation: IN
- How discovered: O
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DALA13006693214

## Discrepancy

DURING INSPECTION, FOUND AFT FUSELAGE UNDERFLOOR BET FR66 AND FR67, STR 26R HAS CORROSION.  REPLACED STRINGER, PN D5348004720201, BATCH: 0002384124 IAW SRM 51-42-11 AND DWG D53480024.  FABRICATED NEW CLEAT CLIP ON STAM TRAVELER T13/979626, MAT 2024-0 .071C BATCH 0001942001, FABRICATED NEW CONNECTING SECTION ON STAM TRAVELER T13/979625, MAT 2024--T351/3X3.  BATCH 0002185878. STRINGER DAMAGE DIMENSION L=18" W=1.0" D=0.040" NO ALLOWABLE DAMAGE LIMITS ESTABLISHED.

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