# SDR FDEA202603150375

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 15, 2026
- Submitted: March 27, 2026
- Operation: Air carrier
- Aircraft: [N688FE](https://openairdocs.org/aircraft/N688FE), 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: 874
- Aircraft time: 23,240 hours, 13,555 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Web
- Part number: A53832100208
- Condition: Cracked
- Location: Zone 200
- 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/FDEA202603150375

## Discrepancy

MDCC UNDER FLOOR WEB AT FR47, BETWEEN Y0 AND Y450 CRACKED.  REPAIRED THE MDCC UNDER FLOOR CRACKED WEB AT FR47, BETWEEN Y0 AND Y450 PER A300-  600F SRM53-15-15-201-C2. THIS REPAIR IS CATEGORY B PER A300-600F SRM53-15-15-201-C2, IT   MUST BE INSPECTED AT DEFINED INTERVALS,THE INSPECTION INSTRUCTION REFERENCE IS   A300-600F SRI53-15-15-2-002-00. INSPECTION THRESHOLD FROM REPAIR EMBODIMENT:24000FC.   SUBSEQUENT INSPECTION AT INTERVAL OF 3000FC UNTIL 37500FC. INSPECTION METHOD:   DETAILED VISUAL. MAJOR REPAIR IAW FEDEX GMM6-2-100.

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