# SDR YENA2026070900542

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 4, 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): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- 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/YENA2026070900542

## Discrepancy

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 4, OPEN FASTENER HO LE ON ZONE 2, CRACK DIRECTION IS 11 OCLOCK, CRACK DEPTH IS 0.100 INCH, IN FWD CARGO COMPARTMENT (1 EA)(-Y254); (RESOLVED ON W/O: 1457737 TASKCARD: NR-00044 )  REF AEROMAN NR 2026 -299011 WO 2026 196/1 ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER WING BOX FRONT SPAR HORIZONTAL BEAMS AT  LEVEL FR36, (Y-254)(HOLE ON ZONE 2) IAW AEROMAN EA 57-0036-26, REV. 0 (COVER PLUS PARTS 1 AND 2); AIRBUS RDAF 81801723/003/2026, ISSUE A AND EC NO. A26-513-01. MESURES OF CRACK DEPTH IS 0.100 INCH. PERFORMED HFEC AND ROTOTEST ON AFFECTS AREAS AS PER NTM 51-10-08 AND NTM 51-10-01. NO CRACK  INDICATION FOUND.

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