# SDR YENA2026092300893

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 21, 2026
- Submitted: September 24, 2026
- Operation: Air carrier
- Aircraft: [N588JB](https://openairdocs.org/aircraft/N588JB), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 02201
- Aircraft time: 82,570 hours, 29,949 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Condition: Cracked
- 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/YENA2026092300893

## Discrepancy

DURING HEAVY MAINTENANCE, A CRACK INDICATION WAS FOUND IN HOLE B IN  DOUBLE JOGGLE AREA, FR 16.  CRACK DIRECTION IS 3 OCLOCK VIEWED FROM OUTSIDE. CONFIRMED CRACK INDICATION USING BOROSCOPE IAW NTM 51-90-00.   PERFORMED A PERMANENT REPAIR OF FRAME 16 IAW SRM 53-11-12-300-012. FINAL DIAMETER OF HOLE BEFORE INSTALL BUSH IS 0.5250 IN (13.335 MM). REAMED TO 2ND OVER SIZED LEADER HOLE B. (0.281 IN) AND ASSOCIATED HOLE A (0.216 IN). THIS REPAIR IS CLASSIFIED CATEGORY B.

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