# SDR YENA2026070900534

- 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 100
- 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/YENA2026070900534

## Discrepancy

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 CWB VERTICAL STRINGER 5, OPEN FASTENER HOLEON ZONE 2, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.105 INCH, IN FWD CARGO COMPARTMENT (1EA)(-Y765). (RESOLVED ON W/O: 1457737 TASKCARD: NR-00031 )   REF AEROMAN WO 2026 196/1 NR 299009 ACCOMPLISHED PERMANENT REPAIR OF CRACK DAMAGES ON THE CENTER WING BOX FRONT SPAR HORIZONTAL BEAMS AT   LEVEL FR36, Y-765 (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, EC NO. A26-513-01. MEASURES OF DEPTH CRACK IS: 0.105 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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