# SDR DALA2019052703183

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 26, 2019
- Submitted: May 27, 2019
- Operation: Air carrier
- Aircraft: N320US
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Aircraft serial: 213
- Aircraft time: 83,450 hours, 37,775 cycles
- System (JASC): [5312 · Fuselage Main, Bulkhead](https://openairdocs.org/jasc/5312)
- Part: Pressure Panel
- Condition: Cracked
- Location: Fuselage
- 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/DALA2019052703183

## Discrepancy

FR35R-36R PRESSURE PANEL AND LONGITUDINAL BEAM; TITANIUM ANGLE CRACKED AT HOLES A AND B, ABOVE PRESSURE PANEL REPAIR CUTOUT SHAPE -M-, LONGITUDINAL BEAM SECOND TO AFT VERTICAL HOLE CRACKED THROUGH HOLE AFT HOLE IS OVAL AS WELL SHAPE -M- AND LONGITUDINAL BEAM AFT VERTICAL HOLE IS OVAL IN SHAPE -M-, REPAIR PER PRI 577930-14AD REV 0,1,2,3,4,5,6,7 AND COMPLY WITH ER/A 577930-14AD REV ORIGINAL.

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