What was found
NR 1 PYLON STRUT I/B SIDE STRUT ACCESS HOLE FOR PANEL 416BR AFT UPPER CORNER SKIN IS CRACKED. STOP DRILLED CRACK. FABRICATED & INSTALLED 2EA DOUBLERS. HFEC INSP, NO CRACK PAST STOP DRILL.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
NR 1 PYLON STRUT I/B SIDE STRUT ACCESS HOLE FOR PANEL 416BR AFT UPPER CORNER SKIN IS CRACKED. STOP DRILLED CRACK. FABRICATED & INSTALLED 2EA DOUBLERS. HFEC INSP, NO CRACK PAST STOP DRILL.