What was found
DURING D-CHECK, THE SHEAR TIE CLIP AT THE RADIUS, UPPER END OF FORWARD SPAR WEB VERTICAL STIFFENER AT LBL 25 WAS FOUND CRACKED. REPLACED TIE CLIP PER BOEING SRM 51-10-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, THE SHEAR TIE CLIP AT THE RADIUS, UPPER END OF FORWARD SPAR WEB VERTICAL STIFFENER AT LBL 25 WAS FOUND CRACKED. REPLACED TIE CLIP PER BOEING SRM 51-10-1.