# SDR 08FDEA00826

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 10, 2008
- Submitted: March 10, 2008
- Operation: Air carrier
- Aircraft: N425FE
- Make and model: Airbus A310-203
- Registry model: [Airbus A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (OpenAirDocs)
- Aircraft serial: 264
- Aircraft time: 36,499 hours, 24,558 cycles
- System (JASC): [5340 · Fuselage Main, Attach Fittings](https://openairdocs.org/jasc/5340)
- Part: Attach Angle
- Part number: A5341076720000
- 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/08FDEA00826

## Discrepancy

AFT CARGO PIT; FWD BULKHEAD AT FRAME 54;  THE CEILING ATTACH ANGLE IS CORRODED FROM 131 TO 139 CM (51.5" TO 54.5 ").  REMOVED CORROSION IAW SRM 51-74-10. ORIGINAL MATERIAL THICKNESS .098. REMAINING LATERIAL .050. MATERIAL REMOVED .048.   OUT OF LIMITS IAW SRM 53-10-00.  REMOVED ANGLE IAW SRM 51-40-21.   FABBED NEW ANGLE IAW DWG A53410767. ALODINED IAW SRM 51-21-10. PRIMED AND PAINTED IAW SRM 51-23-10. PART MARKED IAW GMM 7-0-1001. INSTALLED ANGLE IAW SRM 51-40-21. MINOR REPAIR.

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