# SDR FDEA202504160598

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 16, 2025
- Submitted: April 16, 2025
- Operation: Air carrier
- Aircraft: [N676FE](https://openairdocs.org/aircraft/N676FE), 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: 790
- Aircraft time: 34,994 hours, 19,996 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Part number: A57110530211
- 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/FDEA202504160598

## Discrepancy

CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH   FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL   COMPLIED WITH EO 6-5710-E0342809 D P2. TITLE: WINGS - CENTER WING BOX - INSPECTION OF   REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE. SBÏ¿½S A300-57-6049 R08, A300-57-  6086 R07, A300-57-6121 IR & 300-57-6050 R03. REPAIRED THE CENTER WING BOX REAR SPAR AND   BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE CRACKED FASTENER "I" HOLE. THIS   IS CATEGORY A REPAIR. MINOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57103894 FOR WORK   DETAILS.

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