As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STOP DRILLED CRACK AND BEGAN FABRICATING REPAIR PER M/M 55-30-0 FIG 803. CHEM TREATED PER PS 900-2-4-1 NR 2. TREATED AND PAINTED PER PS 900-2 NR 5. OK TO INSTALL. INSTALLED REPAIR ANGLE PER M/M 55-30-0 PG 803. STRINGER WAS FOUND CRACKED ON VERTICAL STAB.