# SDR YENA2026072200611

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 8, 2026
- Submitted: July 23, 2026
- Operation: Air carrier
- Aircraft: [N519JB](https://openairdocs.org/aircraft/N519JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 01398
- Aircraft time: 91,449 hours, 33,975 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/YENA2026072200611

## Discrepancy

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED ON FR35 AT S30L, LOWER FUSELAGE. CRACK DEPTH = 0.100 INCHES APPROX, CRACK POSITION: 5 AND 11 OCLOCK, LOOKING FROM OUTSIDE.  REF AEROMAN WO 2026 244/1 NR 2026-301086.  PERFORMED REPAIR ON HOLE (H2) LOCATED ON FR35 AT LEVEL OF STR30 LH SIDE ON LOWER FUSELAGE IAW EA 53-0047-26, EC  AND RDAF 81807254/007/2026 ISSUE B. AIRBUS APPROVED THE REPAIR AS INTERIM  WITHOUT CATEGORY.

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