# SDR YENA2026070900552

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 5, 2026
- Submitted: July 10, 2026
- Operation: Air carrier
- Aircraft: [N568JB](https://openairdocs.org/aircraft/N568JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02063
- Aircraft time: 84,031 hours, 30,499 cycles
- System (JASC): [5315 · Fuselage Main, Floor Beam](https://openairdocs.org/jasc/5315)
- Part: Floorbeam
- Condition: Cracked
- Location: Zone 200
- 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/YENA2026070900552

## Discrepancy

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 HORIZONTAL FLOORBEAM VERTICAL RADIUS OF THE BACK SIDE OF THE SPAR VERTICAL STRINGER 3 ZONE 1 CRACK LENGTH IS 0 .850 INCH APPROX, IN FWD CARGO COMPARTMENT.  ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER BOX FRONT SPAR HORIZONTAL BEAMS AT  LEVEL FR36, Y254 (VERTICAL RADIUS, ZONE 1) IAW AEROMAN EA 57-0036-26, REV 0 (COVER PLUS PARTS 1 AND  2), AIRBUS RDAF 81801723/003/2026, ISSUE A, EC A26-513-01. MEASURE DEPTH OF CRACK IS: 0.850  INCH. PERFORMED HFEC AND ROTOTEST ON AFFECTS AREAS IAW NTM 51-10-08 AND NTM 51-10-01 NO CRACK  INDICATION FOUND.

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