# SDR YENA2026091800850

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 18, 2026
- Submitted: September 19, 2026
- Operation: Air carrier
- Aircraft: [N523JB](https://openairdocs.org/aircraft/N523JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 01506
- Aircraft time: 87,883 hours, 32,500 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/YENA2026091800850

## Discrepancy

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 BULK HEAD LH SIDE AT LEVEL OF STGR 30 AT OPEN FASTENER HOLE LOWER OUTBOARD COMMON TO MILLED COUPLING, CRACK DIRECTION ARE 4 AND 9OCLOCK, CRACKDEPTH IS 0.120 INCHAPOROX., IN FWD CARGO COMPARTMENT (2EA); (RESOLVED ON W/O: 1435456 TASKCARD: NR-00047 ) REF AEROMANW/O 2026 279/1 NR 348543 ACCOMPLISHED MAJOR REPAIR OF THE REPORTED CRACK AT THE FR35 LHS AT HOLE #2 ON FWD AND AFT SKIN LAYERS AND AT HOLE #W1 ON THE FR35 WEB LAYER I.A.W.AEROMAN EA 53-0055-26 REV.0 (COVER PARTS 1-6) SOLUTION LIFE OR LIMITATION: 6 MONTHS IAW AIRBUS RDAF 81825284/003/2026#A AND EC NO.A26-710-01.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
