What was found
FOUND ONE INCH LONG CRACK AT ATTACH POINT FOR RIGHT ENGINE PYLON PANEL 8105, AFT OUTBOARD NUTPLATE AREA. INSTALLED CRACK REPAIR PER STRUCTURAL REPAIR MANUAL 54-01, FIGURE 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND ONE INCH LONG CRACK AT ATTACH POINT FOR RIGHT ENGINE PYLON PANEL 8105, AFT OUTBOARD NUTPLATE AREA. INSTALLED CRACK REPAIR PER STRUCTURAL REPAIR MANUAL 54-01, FIGURE 2.