As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING DVI & HFEC, FOUND CRACK ON CTR WING BOX REAR SPAR VERTICAL PRESS WEB ALONG THE VERTICAL PRESS DECK AT RBL 42.000 & WL 204.000 DOT 012. INSTALLED CTR WING BOX REAR SPAR VERTICAL PRESS WEB REPAIR IAW SRM 57-10-10 FG 204. SEE STEPS BELOW THIS REPAIR IS A CATEGORY B & INSPECTION THRESHOLD IS 56.000 FLIGHT CYCLES AFTER REPAIR INSTALLATION INSPECTION METHOD HIGH FREQUENCY EDDY CONNECT.