# SDR FDEA202608201196

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: August 20, 2026
- Submitted: August 21, 2026
- Operation: Air carrier
- Aircraft: [N125FE](https://openairdocs.org/aircraft/N125FE), registered now
- Make and model: Boeing 767-3S2F
- Registry model: [Boeing 767-3S2F](https://openairdocs.org/model/boeing-767-3s2f) (OpenAirDocs)
- Aircraft serial: 42717
- Aircraft time: 21,694 hours, 7,698 cycles
- System (JASC): [5730 · Wing, Plate/Skin](https://openairdocs.org/jasc/5730)
- Part: Panel
- Part number: 114T610162
- Condition: Delaminated
- Location: Zone 600
- 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/FDEA202608201196

## Discrepancy

RIGHT WING UPPER L/E PANEL ABOVE PYLON AT ISS 337.60 HAS EROSION ACROSS L/E, WITH NUMEROUS FASTENER HEADS PULLING THROUGH SKIN.   ALSO FOUND SEVERAL DOUBLE DRILLED HOLES ON THE RT WING LEADING EDGE RIBS AND CHORDS BETWEEN WS 337 & 356.   THERE ARE NO PUBLISHED REPAIRS FOR THIS TYPE OF DAMAGE  SEAL RIB INSTL WS 337,  SPLICE STRAP, UPPER SPLICE CHORD, SHEAR CHORD, SHEAR CHORD, SEAL RIB INSTL WS 356.   REMOVAL OF FASTENERS FROM THE NON-CONFORMING LOCATIONS REVEALED DRILL-THROUGH DAMAGE PENETRATING THE UNDERLYING INBD SLAT TRACK BETWEEN APPROX. WS 345.5 & 356.6 AS WELL AS THE ADJACENT STRUCTURAL CLIPS.  R & R PANEL -BONDED IAW DWG 114T6101, REV A, SHT 12 & 13.  COMPLIED WITH EA H-5710-T0388288M, PT 1.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
