# SDR FDEA202601120048

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: January 12, 2026
- Submitted: January 16, 2026
- Operation: Air carrier
- Aircraft: [N658FE](https://openairdocs.org/aircraft/N658FE), 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: 752
- Aircraft time: 39,616 hours, 22,274 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- 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/FDEA202601120048

## Discrepancy

NDT INSP - RT CENTER BOX REAR SPAR FR47 FWD FITTING RIB1 HOLE "C" FOUND CRACK SIGNAL.  COMPLIED WITH EA 6-5710-T0386164 REPAIRED THE CRACKED CENTER WING BOX REAR SPAR   RHS FR47 FWD FITTING RIB1 HOLE "C". TITLE: WINGS - BASIC WING STRUCTURE - FR47 RH REAR   SPAR HOLE C CRACK REPAIR - SB A300-57-6113 AND R57110371 EMBODIMENT.  THIS IS A CAT "B"   REPAIR AND THE POST REPAIR INSPECTION REQUIREMENTS WILL BE PROVIDED PRIOR TO THE   EXPIRATION OF INTERIM RDAF. THE FOLLOW UP INSPECTION IS TRACKED BY EA 6-5710-T0386164.   MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 57107844 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.