# SDR VQI2011F00031

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 17, 2011
- Submitted: December 27, 2011
- Operation: Air carrier
- Aircraft: [N622VA](https://openairdocs.org/aircraft/N622VA), registered now
- Make and model: Airbus A320-214
- Registry model: [Airbus A320-214](https://openairdocs.org/model/airbus-a320-214) (OpenAirDocs)
- Aircraft serial: 2674
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Floor Support
- Part number: D5347219720200
- 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/VQI2011F00031

## Discrepancy

REMOVED CORROSION AT CABIN FLOOR PANEL SUPPORT UPPER SURFACE BETWEEN FRAMES 68-70, RBL 6" IAW SRM 51-74-00.  PERFORMED UT THICKNESS INSP OF REWORKED AREA, FOUND TO BE AT UPPER SURFACE 0.150 MAX, 0.90 MIN USED DAKOTA MX-3 SN 3B264 IAW A320 NDTM 51-10-04.  R & R FLOOR SUPPORT BEAM IAW SRM 51-42-00-00.

---
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.