# SDR FDEA202001160141

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 16, 2020
- Submitted: February 4, 2020
- Operation: Air carrier
- Aircraft: [N686FE](https://openairdocs.org/aircraft/N686FE), 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: 804
- Aircraft time: 27,476 hours, 15,641 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Web
- Part number: A53832100208
- Condition: Cracked
- Location: Frame 47
- 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/FDEA202001160141

## Discrepancy

MAIN DECK FR47 UNDERFLOOR WEB BETWEEN Y0 AND Y450 CRACKED REPAIRED THE CRACKED WEB OF MAIN DECK FR47 UNDERFLOOR BETWEEN Y0 AND Y450   PER A300-600F SRM53-15-15-C2-201 PARA.5. THE REPAIR WAS CATEGORY B AND IT MUST BE   INSPECTED AT DEFINED INTERVALS PER A300-600F SRI 53-15-15-2-002-00. INSPECTION   THRESHOLD FROM REPAIR EMBODIMENT: 24000FC. SUBSEQUENT INSPECTION AT INTERVAL   OF 3000FC UNTIL 42500FC. INSPECTION METHOD: DETAILED VISUAL. MAJOR REPAIR IAW   FEDEX GMM6-2-100.

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