# SDR CALA2019051700772

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 13, 2019
- Submitted: May 17, 2019
- Operation: Air carrier
- Aircraft: [N464UA](https://openairdocs.org/aircraft/N464UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1290
- Aircraft time: 63,049 hours, 25,290 cycles
- System (JASC): [5312 · Fuselage Main, Bulkhead](https://openairdocs.org/jasc/5312)
- Part: Bulkhead
- Part number: D533370666200
- Condition: Damaged
- 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/CALA2019051700772

## Discrepancy

CENTER WING TANK FWD SPAR LT LOWER FWD FLANGE OF THE PRESSURE PANEL FASTENER HOLES 23 AND 24 PRODUCED REJECTABLE OUT OF ROUND INDICATIONS DURING ABHEC INSPECTION AD 2018-06-04 PER NR 9298909 ACCOMPLISHED INTERIM REPAIR OF LT FR 35-36 PRESSURE PANEL HOLES PER PART 1 OF ECRA 5331-02385. ACCOMPLISH THE PERMANENT REPAIR AT FUSELAGE FR 35-36 LT PRESSURE PANEL HOLES PER PART 3 OF ECRA 5331-02385 ON OR BEFORE 06NOV2019. PLANNING TO CONTACT ENGINEERING AFTER 06SEP2019 BUT BEFORE 06OCT2019 FOR PERMANENT REPAIR. INTERIM REPAIR PERFORMED PER ECRA 5331-02385 PART 1. NO PART 2 RECHECK REQUIRED AT THIS TIME. PART 3 TBD BY ENGINEERING. ACCOMPLISH THE PERMANENT REPAIR AT FUSELAGE FR35-36 LT/RT PRESSURE PANEL HOLES PER PART 3 OF ECRA 5331-02385 ON OR BEFORE 06NOV2019.

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