# SDR CALA2020032000616

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: March 9, 2020
- Submitted: March 20, 2020
- Operation: Air carrier
- Aircraft: [N447UA](https://openairdocs.org/aircraft/N447UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 836
- Aircraft time: 70,409 hours, 28,961 cycles
- System (JASC): [5310 · Fuselage Main, Structure](https://openairdocs.org/jasc/5310)
- Part: Pressure Panel
- Part number: D2827004600
- 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/CALA2020032000616

## Discrepancy

WHILE PERFORMING EA 5330-05216 REV A FOUND SEVERAL HOLES CRACKED AT FR 36 RHS ON THE PRESSURE PANEL. HOLES THAT WERE CRACKED #6,7,9,12,39&57 SEE ECRA 5331-02636 FOR HOLE NUMBERING ACCOMPLISHED PART 1 OF ECRA 5331-02636 INTERIM REPAIR PLACED ON DIP PER PART 1C OF ECRA 5331-02636 TO ACCOMPLISH A PERMANENT REPAIR AT RHS FR 35-36 PRESSURE PANEL HOLES PER PART 3 OF EC/RA# 5331-02636 ON OR BEFORE 07-SEP-2020. PLANNING TO CONTACT ENGINEERING AFTER 07-AUG-2020, BUT BEFORE 01-SEP-2020 FOR PERMANENT REPAIR. ACCOMPLISH A PERMANENT REPAIR AT RHS FR 35-36 PRESSURE PANEL HOLES PER PART 3 OF EC/RA#: 5331-02636 ON OR BEFORE 07-SEPT-2020. PLANNING TO CONTACT ENGINEERING AFTER 07-AUG-2020, BUT BEFORE 01-SEPT-2020 FOR PERMANE

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.