# SDR CALA2024051301468

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 9, 2024
- Submitted: May 13, 2024
- Operation: Air carrier
- Aircraft: [N472UA](https://openairdocs.org/aircraft/N472UA), registered now
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 1435
- Aircraft time: 70,487 hours, 29,485 cycles
- System (JASC): [5311 · Fuselage Main, Frame](https://openairdocs.org/jasc/5311)
- Part: Frame
- Part number: SR531890A07901
- Condition: Corroded
- Location: Fr 68 S23r
- 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/CALA2024051301468

## Discrepancy

FR 68 AT STR23 RH, PREVIOUS CORROSION REPAIR WAS REEVALUATED AND SUBSEQUENTLY REPAIRED IAW ECRA5341-01452. WEB AT STR23RH WAS REPAIRED AT BFM. REPAIR IS EXPECTED TO BECOME PART 3 OF LATEST REV OF ECRA5341-01452 ON/BEFORE MAY 3, 2025. PERMANENT SOLUTION W/ INSP REQMTS. ACCOMP A PERMANENT REPAIR PER ACCOMPLISHED INTERIM REPAIR IAW ECRA5371-01452 AND VTMAE EA 320-5341-13-A3552. PART 1.  DIP REQ''D AS FOLLOWS: FUSELAGE FR68 OK TO CARRY PER ECRA 5341-01452,FUSELAGE FRAME  WEB 68 AT TOMC-APPROVAL FROM SC1ELBYC COMMENT STR23RH WAS REPAIRED AT BFM. REPAIR IS EXPECTED TO BECOME PERMANENT SOLUTION W/ INSP REQMTS. ACCOMP A PERMANENT REPAIR PER PART 3 OF THE LATEST REV OF ECRA 5341-01452 ON OR BEFORE MAY 03, 202.

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