# SDR FDEA202604110583

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 11, 2026
- Submitted: May 12, 2026
- Operation: Air carrier
- Aircraft: [N669FE](https://openairdocs.org/aircraft/N669FE), 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: 774
- Aircraft time: 38,233 hours, 21,763 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame Splice
- Part number: A57110530211
- 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/FDEA202604110583

## Discrepancy

MAIN FRAME, INSPECTION,  HOLES IN FUSELAGE FRAME 47 SPLICE FITTING   BETWEEN STR 24 & 26, LH /RH, AIRBUS SB A300-53-6123 COMPLIED WITH EO 6-5310-7-5017 P P6. TITLE: FUSELAGE - MAINFRAME - INSPECTION - HOLES IN   FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26, LT & RT, AIRBUS SB A300-53-6123.   REPAIRED THE CRACKED RT HOLE N IN UPPER FUSELAGE FR47 BTW S25 AND S26. THIS IS A CATEGORY B REPAIR. FOLLOW-UP INSPECTION PER EA 6-5310-T0387082.   MAJOR REPAIR IAW FEDEX GMM6-2-100.

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