As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON FSD STUB FRAME ON BS 291.5+9; .2' ABOVE SEAL DEPRESSOR; .3' LENGTH. REMOVED DAMAGE FSD STUB FRAME; LOCATED; DRILLED AND INSTALLED NEW FSD STUB FRAME SECTION LOCATED AT BS 291.5+9;2' ABOVE SEAL DEPRESSOR IAW SRM 51-40-02-0G-0 AND BOEING DWG 141A8370 REV: D.