# SDR FDEA202406300890

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 30, 2024
- Submitted: July 3, 2024
- Operation: Air carrier
- Aircraft: [N745FD](https://openairdocs.org/aircraft/N745FD), 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: 668
- Aircraft time: 71,981 hours, 26,630 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Fitting
- Part number: A57111092203
- 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/FDEA202406300890

## Discrepancy

CENTER WING BOX - REAR SPAR LOWER FLANGE FR47 RHS HOLE "P" INNER SURFACE FOUND   SCRATCH COMPLIED WITH EA: 6-5710-150047 E P7 REPAIRED THE CENTER WING BOX REAR SPAR LOWER   FLANGE FR47 RHS SCRATCHED AND CRACKED HOLE "P". TITLE: WINGS - CENTER WING BOX -   REAR SPAR LOWER FLANGE AT FRAME 47. THIS IS CAT B REPAIR AND THE RDAF REPRESENTS A   STAGE 1 APPROVAL FOR STATIC STRENGTH ANALYSIS AND AWAITING FURTHER DT APPROVAL.   THIS REQUIREMENT WILL BE TRACKED BY ENMDS TO OBTAIN STAGE 2 AND/OR STAGE 3   APPROVAL WITHIN 6 MONTHS. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57106846 FOR   WORK DETAIL.

---
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.
