# SDR CALA2019071801216

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 17, 2019
- Submitted: July 19, 2019
- Operation: Air carrier
- Aircraft: [N428UA](https://openairdocs.org/aircraft/N428UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 523
- Aircraft time: 78,952 hours, 30,607 cycles
- System (JASC): [5312 · Fuselage Main, Bulkhead](https://openairdocs.org/jasc/5312)
- Part: Pressure Panel
- Part number: D5337090121000
- Condition: Cracked
- Location: Fuselage
- Stage of operation: IN
- How discovered: O
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CALA2019071801216

## Discrepancy

DURING INSPECTION AND MODIFICATION PER EA 5330-05216 OP2 AT LT PRESSURE PANEL AT FR35-36 HOLES SHOWN FIGURE 1 WERE FOUND WITH CRACK INDICATIONS DAMAGE IS BEYOND EA LIMITS PER NON ROUTINE 9293540 ACCOMPLISHED INTERIM REPAIR AT LH PRESSURE PANEL FR 35-36 HOLES IAW ECRA 5311-02199 PART 1 STEP 1. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5311-02199 ON OR BEFORE 05JAN2020. PLANNING TO CONTACT ENGINEERING AFTER 15DEC2019 BUT BEFORE 25DEC2019 FOR PERMANENT REPAIR. ALL WORK ACCOMPLISHED ON NR 9293540. APPROVED TO CARRY REF ECRA 5311-02199 PERMANENT REPAIR TO BE ACCOMPLISHED ON OR BEFORE 05JAN20, PLANNING TO CONTACT ENGINEERING AFTER 15DEC19 BUT BEFORE 25DEC19. TOMC-APPROVAL FROM SC1ELBYC COMMENT QC REVIEW QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT.

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