# SDR DALA2024041904582

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 17, 2024
- Submitted: April 19, 2024
- Operation: Air carrier
- Aircraft: [N353NW](https://openairdocs.org/aircraft/N353NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 786
- Aircraft time: 75,888 hours, 35,719 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Part number: UNKNOWN
- Condition: Cracked
- Location: Frm 68
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/DALA2024041904582

## Discrepancy

SHIP 3253 DISC: CRACK INDICATION FOUND ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R, CRACK LENGHT= 1.0 INCH APPROX. C/A: ACCOMPLISHED ER/A 616797-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616797-14AD REV 0 THRU REV. 5. IT HAS BEEN VALIDATED,PERFORMED REPAIR INSTRUCTIONS ON FRAME WEB HORIZONTAL FLANGE LOCATED ON FR68 AT LEVEL OF STRINGER 22R AS PER ER/A 616797-14ADREV.0 THRU REV. 5. HAS BEEN COMPLIED WITH APPROVED DATE: 16-APR-24. SEE LOG PAGE # 0297395 FOR TIME CONTROLLED ITEMS SECTION DTEFOR FRAME WEB HORIZONTAL FLANGE, REPAIR APPROVAL IS LIMITED TO 6 MONTHS AFTER SECTION I (APR/2024). ADDITIONAL ENGINEERINGAUTHORIZATION (ER/A) REVISION IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT

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