# SDR DALA2026053103292

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 27, 2026
- Submitted: May 31, 2026
- Operation: Air carrier
- Aircraft: [N341NW](https://openairdocs.org/aircraft/N341NW), registered now
- Make and model: Airbus A320-212
- Registry model: [Airbus A320-212](https://openairdocs.org/model/airbus-industrie-a320-212) (OpenAirDocs)
- Aircraft serial: 380
- Aircraft time: 96,420 hours, 43,802 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Fitting
- 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/DALA2026053103292

## Discrepancy

DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALE D THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA.  PER SECTION II OF 633308-14AD, ACCOMPLISH SECTION II INITIAL INSPECTION WITHIN 29,500 FC FROM SECTION I (21MAY26). REPEAT SECTION II INSPECTION WITHIN EVERY 8,700 FC AFTER INITIAL INSPECTION. ASSOCIATED ER/A 32-633308 ADDED FOR AC 3241. (LP: 1616599, AIRCRAFT WAS GROUNDED)

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