# SDR FDEA201005271689

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 27, 2010
- Submitted: May 28, 2010
- Operation: Air carrier
- Aircraft: N403FE
- Make and model: Airbus A310-203
- Registry model: [Airbus A310-203](https://openairdocs.org/model/airbus-industrie-a310-203) (OpenAirDocs)
- Aircraft serial: 230
- Aircraft time: 35,997 hours, 30,322 cycles
- Engine: Ge CF680
- System (JASC): [5315 · Fuselage Main, Floor Beam](https://openairdocs.org/jasc/5315)
- Part: Stiffener
- Part number: A53774722200
- Condition: Cracked
- Location: Fuselage
- 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/FDEA201005271689

## Discrepancy

LWR FWD CARGO CEILING FRAME 25 FLOORBEAM FWD SIDE 27" RT OF CTRLINE THE VERTICAL STIFFENER IS CRACKED AT THE TOP (APPROX. LENGTH IS 1/4IN) BLENDED CRACK AT FRME 25 IAW SRM 51-73-10.  NDT VERIFIED REMOVAL OF CRACK.  FABRICATED REPAIR ANGLE AND REPAIRED CROSSBEAM AT FR 25 AND 27" RT OF   CTRLINE IAW SRM 53-10-15 FIG 203, SHEET 1.

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