# SDR CALA2018112502421

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: November 24, 2018
- Submitted: November 25, 2018
- Operation: Air carrier
- Aircraft: N424UA
- Make and model: Airbus A320-232
- Registry model: [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232) (OpenAirDocs)
- Aircraft serial: 506
- Aircraft time: 78,500 hours, 30,211 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Cleat
- Part number: D53230385200
- Condition: Corroded
- 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/CALA2018112502421

## Discrepancy

FWD CARGO COMPARTMENT FR30 STRINGER 41L-42L CLEAT HAS CORROSION REF 9296474 SUPPORT TASK FCD 5300-01440. R&R CLEAT LOCATED AT FR30 BETWEEN STRINGERS 41L-4 2L IAW SRM 51-42-11. FOUND CLEAT TO BE OUT OF LIMITS IAW GENERAL LIMITS ABD0001 PG 7 ISSUE G, NSA2110 PG 5 TABLE 2 & DWG C2D53230385. REMOVED .008 FROM THE ORIG MAT THICKNESS OF .055 REMAINING MAT IS .047 MAX ALLOWED MAT REMOVAL IS .004.

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