# SDR FDEA202501240125

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 24, 2025
- Submitted: January 24, 2025
- Operation: Air carrier
- Aircraft: [N650FE](https://openairdocs.org/aircraft/N650FE), 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: 726
- Aircraft time: 39,919 hours, 22,165 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Web
- Part number: A5383210320600
- Condition: Cracked
- Location: Zone 200
- Stage of operation: IN
- How discovered: E
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/FDEA202501240125

## Discrepancy

MDCC UNDER FLOOR PANEL - FR47, Y953-Y1456 FOUND 1EA WEB CRACKED. REPAIRED THE CRACKED WEB AT MDCC UNDER FLOOR PANEL FR47, Y953-Y1456 PER A300-600F   SRM53-15-15-201 FIG201. THIS IS CAT B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS   PER SRI53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT: 24000FC.   SUBSEQUENT INSPECTION AT INTERVAL: 3000FC, INSPECTION METHOD: DVI. MAJOR REPAIR IAW   FEDEX GMM6-2-100.

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