# SDR SWAA2024030848162

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 2, 2024
- Submitted: March 8, 2024
- Operation: Air carrier
- Aircraft: [N8565Z](https://openairdocs.org/aircraft/N8565Z), registered now
- Make and model: Boeing 737-8H4
- Registry model: [Boeing 737-8H4](https://openairdocs.org/model/boeing-737-8h4) (OpenAirDocs)
- Aircraft serial: 42533
- Aircraft time: 19,940 hours, 10,049 cycles
- System (JASC): [5345 · Fuselage, Equipment Attach Fittings](https://openairdocs.org/jasc/5345)
- Part: Mount
- Part number: UNKNOWN
- Condition: Corroded
- Location: Lavatory
- Stage of operation: IN
- How discovered: 9
- Nature of condition: O
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/SWAA2024030848162

## Discrepancy

AFT GALLEY LAV MOUNT HAS CORROSION AROUND BASE AT STA 947 LBL 24.<[01] CLEANED CORROSION PER SRM 51-10-02. REWORKED AREA MEASURED OUT OF LIMITS IAW SRM 53-70-51-1A-1 FIG. 104; DETAIL E.;[07] CUT AND REMOVED ENTIRE UPPER SECTION OF STA 947 CHORD I.A.W SRM 53-70-51-2R-5.;[08] VERIFIED CUT AND REMOVED ENTIRE UPPER SECTION OF STA 947 CHORD I.A.W SRM 53-70-51-2R-5.;[09] ACCOMPLISHED HFEC SURFACE AND HOLE PROBE OF REPAIR AREA PER NDT PART 6 51-00-00 PROC. 23 AND 51-00-00 PROC 16 NO DEFECTS NOTED;[10] FLAP PEENED UPPER CHORD CUT EDGE IAW SRM 53-70-51-2R-5 AND RESTORED FINISH PER SRM 51-21-73;[11] VERIFIED FLAP PEENED UPPER CHORD CUT EDGE IAW SRM 53-70-51-2R-5 AND RESTORED FINISH PER SRM 51-21-73.;[12] FABRICATED; LOCATED; AND DRILLED T-CHORD IAW SRM 53-70-51-2R-5;[13] VERIFIED FABRICATED; LOCATED; AND DRILLED T-CHORD IAW SRM 53-70-51-2R-5.;[14] OK TO INSTALL T-CHORD.;[15] INSTALLED T-CHORD AND SPLICE PER SRM 53-70-51-2R-5. OK TO INSTALL REMOVED ATTACHING STRUCTURE.;[16] INSTALLED T-CHORD AND SPLICE PER SRM 53-70-51-2R-5. (RII)<BR> OK TO INSTALL REMOVED ATTACHING STRUCTURE.

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