# SDR YENA2026091000775

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 5, 2026
- Submitted: September 11, 2026
- Operation: Air carrier
- Aircraft: [N521JB](https://openairdocs.org/aircraft/N521JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 01452
- Aircraft time: 89,342 hours, 33,063 cycles
- System (JASC): [5313 · Fuselage Main, Longeron/Stringer](https://openairdocs.org/jasc/5313)
- Part: Stringer
- 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/YENA2026091000775

## Discrepancy

DURING HEAVY MAINTEANCE, CRACK INDICATION FOUND ON STR 5 LH FR 74 PLUS 1 INCH .CRACK DIRECTION PARALEL TO RADIUS OF STRINGER.CRACK LENGTH 0.250INCH; (RESOLVED ON W/O: 1458309 TASKCARD: NR-00069 )  REF AEROMAN W/O 2026 280/1 NR 346167. ACCOMPLISHED THE REPAIR OF CRACK DAMAGE ON THE REAR FUSELAGE TAILCONE ON STRINGER 5LH AT LEVEL OF    
  FR74 IN ACCORDANCE WITH AEROMAN EA 53-0083-26 REV. 0 ( COVER AND PART 1 ) AND AIRBUS RDAF         
  81841016/003/2026 ISSUE B IAW EC NO. A26-695-01

---
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.
