# SDR IPXA2026052841073

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 12, 2026
- Submitted: May 28, 2026
- Operation: Air carrier
- Aircraft: [N341UP](https://openairdocs.org/aircraft/N341UP), registered now
- Make and model: Boeing 767-34AF
- Registry model: [Boeing 767-34AF](https://openairdocs.org/model/boeing-767-34af) (OpenAirDocs)
- Aircraft serial: 37861
- Aircraft time: 37,574 hours, 13,968 cycles
- System (JASC): [5321 · Fuselage Floor Panel](https://openairdocs.org/jasc/5321)
- Part: Floor Panel
- Part number: 453T1996113
- Condition: Damaged
- Location: Zone 100
- 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/IPXA2026052841073

## Discrepancy

LOADER REPORT LOWER AFT CARGO R/H SIDE NEAR DOORWAY FLOOR PANEL EDGE DAMAGE 1. I.A.W. 767-300F SRM 53-00-50-2R-0 REV. 95 PERFORM REPAIR AS BELOW STEP. :CUT OUT THE DAMAGE AND CLEAN.  MEASURE THE CUT OUT ( L : 3.7", W : 0.9", AT AFT EDGE, 3.5" FROM R/H EDGE ).   APPLY THE COMPOUND TO THE CUT OUT AREA CURED AT 125°F FOR 3 HOURS.  BOND THE REPAIR PLIES WITH RESIN CURED AT 170°F FOR 2 HOURS WITH A MINIMUM VACUUM OF 20 IN/HG. CONDITION CHECK IS SATISFACTORY.

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