# SDR FDEA201509272969

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 27, 2015
- Submitted: September 28, 2015
- 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: 249 hours, 13,694 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Crossbeam
- Part number: A53275341202
- Condition: Cracked
- Location: Frame 58
- 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/FDEA201509272969

## Discrepancy

MDCC CROSSBEAM CRACKED AT FRAME 58, Y1700.   IAW SRM 53-10-15 FIGURE 211 REWORK THE STIFFENER & CUT OUT THE CRACK.  PERFORM HFEC INSPECTION TO THE CUT OUT & REWORKED AREA IAW NTM 51-10-08 & NO CRACK FOUND.  MANUFACTURED THE REPAIR ANGLE & DRILL THE FASTENER HOLES IAW SRM 53-10-15 FIGURE 211.  INSTALL THE REPAIR ANGLE IAW SRM 53-10-15   FIGURE 211.  THIS REPAIR CATEGORY IS A, MAJOR REPAIR IAW GMM 6-2-100.

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