# SDR 08FDEA02828

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 11, 2008
- Submitted: July 15, 2008
- Operation: Air carrier
- Aircraft: [N675FE](https://openairdocs.org/aircraft/N675FE), 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: 789
- Aircraft time: 15,830 hours, 8,473 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Web
- Part number: A5378198422200
- 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/08FDEA02828

## Discrepancy

MAIN CABIN METAL PANEL UNDER FLOOR PANEL 231 WG FROM FRAME 26 TO FRAME 28 IS CORRODED.  REMOVED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6.  FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-70-10.  RECEIVED 2 NEW THRUST BRACKETS P/N A5378198422200, PO 624015.1 AND A5378198423400, PO 623903.1.   PART MARKED THRUST BRACKETS IAW FEDEX GMM 7-0-1001.  LOCATED AND DRILLED HOLES IAW A300-600 SRM 51-40-  44.  ALODINED; PRIMED AND PAINTED THE THRUST BRACKETS IAW A300-600 AMM 51-23-10-0.  INSTALLED THRUST BRACKETS IAW A300-600 SRM 51-40-21; PARA 6.  APPLIED CIC TO THRUST BRACKETS IAW A300-600 AMM 51-22-00-0.

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