# SDR FDEA201001140137

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 14, 2010
- Submitted: January 14, 2010
- Operation: Air carrier
- Aircraft: [N681FE](https://openairdocs.org/aircraft/N681FE), registered now
- Make and model: Airbus A300 F4-605R
- Registry model: [Airbus A300 F4-605R](https://openairdocs.org/model/airbus-industrie-a300-f4-605r) (OpenAirDocs)
- Aircraft serial: 799
- Aircraft time: 15,457 hours, 8,384 cycles
- System (JASC): [5720 · Wing Miscellaneous Structure](https://openairdocs.org/jasc/5720)
- Part: Support
- Part number: A5724105920300
- Condition: Cracked
- Location: Rt Wing
- 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/FDEA201001140137

## Discrepancy

RT WING T/E UPPER PANEL SUPPORT IS CRACKED FROM RIB 6A TO RIB 7.  REMOVED CRACKED SUPPORT/STIFFENER IAW SRM 51-40-21, PARA 7.  MACHINED NEW STIFFENER IAW DWG A57241059.  ACCOMPLISHED FPI IAW DWG A57241059 IAW PROCESS 526.2501 AND ABP 6-5230.  NO CRACKS NOTED.  ALODINED IAW SRM 51-21-10.  PAINTED IAW SRM 51-40-44.  PART MARKED IAW GMM 7-0-1000 AND DWG A57241059.   INSTALLED STIFFENER IAW SRM 51-40-21, PARA 7 AND DWG A57246859.

---
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.
