# SDR UALA2010110304075

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 1, 2010
- Submitted: November 5, 2010
- Operation: Air carrier
- Aircraft: [N824UA](https://openairdocs.org/aircraft/N824UA), registered now
- Make and model: Airbus A319-131
- Registry model: [Airbus A319-131](https://openairdocs.org/model/airbus-industrie-a319-131) (OpenAirDocs)
- Aircraft serial: 965
- Aircraft time: 41,162 hours, 16,154 cycles
- Engine: Iae V2522A5
- System (JASC): [5730 · Wing, Plate/Skin](https://openairdocs.org/jasc/5730)
- Part: Skin
- Condition: Corroded
- Location: Lt Wing
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/UALA2010110304075

## Discrepancy

CORROSION WAS FOUND ON THE LT WING TOP NR 2 PANEL BETWEEN RIB 19 AND RIB 20, AT MANUAL REFUELING PORT CUTOUT.  BLEND REPAIR WAS ACP IAW UA EVA 80263 AND EA 319-5721-13-A2032, ON N-R C6017Q.  REPAIR MUST BE INSPECTED AT THRESHOLD OF 200,300 FLIGHT HOURS, OR 124,500 FLIGHT CYCLES, WHICHEVER OCCURS FIRST.  INSP INTERVALS AND METHOD OF INSP HAVE NOT BEEN DETERMINED.  MFG WILL ISSUE A NEW RAS WITH THE INSP INTERVALS AND METHOD BEFORE AC ACCUMULATES ABOVE FH AND FC.

---
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.