# SDR FDEA202412181813

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 18, 2024
- Submitted: December 18, 2024
- Operation: Air carrier
- Aircraft: [N724FD](https://openairdocs.org/aircraft/N724FD), registered now
- Make and model: Airbus A300 B4-622R
- Registry model: [Airbus A300 B4-622R](https://openairdocs.org/model/airbus-a300-b4-622r) (OpenAirDocs)
- Aircraft serial: 530
- Aircraft time: 43,504 hours, 23,194 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame Splice
- Part number: A53812635202
- Condition: Cracked
- Location: Zone 100
- 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/FDEA202412181813

## Discrepancy

FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24LH & STGR26LH FASTENER HOLE H   FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5310-T0313717 B P3. TITLE: FUSELAGE - MAINFRAME - FASTENER HOLES   CRACKED C/T FRAME 47 SPLICE FITTING BETWEEN STR 24 & 26 (EO 6-5310-7-5017 PT5/PT6).   REPAIRED THE FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24LH & STGR26LH CRACKED   FASTENER HOLE H. THIS IS CATEGORY B REPAIR. FOLLOW-UP INSPECTION PER EA: 6-5310-  T0313717 B. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 53101603 FOR WORK DETAILS.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.