# SDR CALA2022111603142

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 15, 2022
- Submitted: November 16, 2022
- Operation: Air carrier
- Aircraft: [N431UA](https://openairdocs.org/aircraft/N431UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 571
- Aircraft time: 78,372 hours, 30,345 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Fitting
- Part number: D5348006228600
- Condition: Damaged
- Location: Frm 66
- 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/CALA2022111603142

## Discrepancy

FOUND DISCREPANT HOLE SIZES CANNOT BE VERIFIED WITH A PREVIOUSLY APPROVED REPAIR ON LH FR 66 AFT DOOR STOP FITTING SEE AEROMAN NON ROUTINE 2022-360050 ATTACHMENT HOLES PER PART 2 OF LATEST REVISION OF ECRA 5341-01 CONTACT ENGINEERING AFTER 90,645 TOTAL FLIGHT AIRCRAFT CYCLES INDICATION FOUND.PERFORMED ROTOTEST INSPECTION ASPER NTM -333 ON OR BEFORE 92,645 TOTAL AIRCRAFT FLIGHT CYCLES.GENERATE A BUT BEFORE 91,645 TOTAL AIRCRAFT FLIGHT CYCLES FOR THE ECRA 51-10-01 IN ALL OPEN FASTENERS HOLES OF DOOR FITTING STOP AND 2ND DIP LOGPAGE REFERENCING THE ONE GENERATED FOR THE REPAIRED 5341-01333 INSPECTION REQUIREMENTS.  PERFORMED HFEC EDDY CORRENT NO CRACK INDICATION FOUND HOLES ON THE LH FR 66 DOOR STOP FITTING #1 THRU #7, PLANNING TO AS PER NTM 51-10-08 ON ALL SURROUNDING AREAS AND NOT CRACK PERFORMED INTERIM REPAIR LOC. LH FR 66 DORR STOP FITTINGS 1 THRU 7 HOLES, THIS REPAIR IS CATEGORY B IAW EC/RA  5341-01333 REV A AND EA 53-0361-22.  GENERATE DTA DIP LOG PAGE TO ACOMPLISH INITIAL INSPECTION AT THE LH FR 66 DOOR STEP FITTING 1 THRU 7.  ACCOMPLISH INITIAL INSPECTION AT THE LH FR66 DOOR STOP REVISION OF ECRA 5341-01333 ON OR BEFORE 92,645 TOTAL AIRCRAFT FITTINGS #1 THRU #7 ATTACHMENT HOLES PER PART 2 OF THE LATEST FLIGHT CYCLES." SEE LP 9787743 FOR 2ND DIP REQUIRED. PERFORMED PART 1 INTERIM REPAIR PER AEROMAN EA-53-0361-22 REV0 AS APPENDIX A IN ECRA 5341-01333. GENERATE DTA DIP TO READ AS OK TO CARRY INITIAL INSPECTION OF REPAIR AT LH FR66 DOOR STOP.

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