# SDR DALA2024090808792

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 3, 2024
- Submitted: September 9, 2024
- Operation: Air carrier
- Aircraft: [N368NW](https://openairdocs.org/aircraft/N368NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 996
- Aircraft time: 72,934 hours, 34,188 cycles
- System (JASC): [5340 · Fuselage Main, Attach Fittings](https://openairdocs.org/jasc/5340)
- Part: Flange
- Condition: Cracked
- Location: Zone 100
- 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/DALA2024090808792

## Discrepancy

SHIP 3268 DISC: SB 53-1491 - S18 REAR FUSELAGE, FR68RH HORIZONTAL FLANGE FILLET RADIUS AT STR22RH - CRACK. ER/A 616556-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 616556-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 19,700 FC FROM SECTION I REPAIR EMBODIMENT . THEREAFTER, REPEAT SECTION II WITHIN EVERY 19,700 FLIGHT CYCLES. ASSOCIATED ER/A 00-616556 ADDED FOR AC 3268. (LP: 0537298)

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