# SDR IPXA2026073003261

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: May 28, 2026
- Submitted: August 6, 2026
- Operation: Air carrier
- Aircraft: [N572UP](https://openairdocs.org/aircraft/N572UP), registered now
- Make and model: Boeing 747-44AF
- Registry model: [Boeing 747-44AF](https://openairdocs.org/model/boeing-747-44af) (OpenAirDocs)
- Aircraft serial: 35669
- Aircraft time: 65,192 hours, 10,331 cycles
- System (JASC): [5320 · Fuselage Miscellaneous Structure](https://openairdocs.org/jasc/5320)
- Part: Stiffener
- Part number: 65B172777
- Condition: Worn
- 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/IPXA2026073003261

## Discrepancy

MAJOR REPAIR,  SUPPORT ROD INSIDE FUELING PANEL STATION AFT ATTACH BOLT HOLE IS ELONGATED AND ATTACH ANGLE IS WORN.   ACCOMPLISH THE REPAIR IAW EO-97627-REQ2 REV1 AND EGAT EI F2026A57M-1357, REVISION 1.  REFER TO DAMAGE REPORT FOR THE ORIGINAL MATERIAL & THICKNESS, REPAIR MATERIAL & THICKNESS, AND THE REPAIR DIMENSION & LOCATION.  DETERMINE THE FLIGHT CONTROL CUMULATIVE WEIGHT CHANGE NEEDS TO BE UPDATED: NO.  INITIATE DEFERRALS AS OUTLINED IN THE APPLICABLE TECHNICAL MANUAL, OR AS SPECIFIED IN THE ENGINEERING ORDER: NONE.

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