What was found
DURING D-CHECK, FOUND VERTICAL STAB LEADING EDGE STA ZV147 UPPER RIB CRACKED AT AFT END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 55-01 FIG 2, SHEET 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING D-CHECK, FOUND VERTICAL STAB LEADING EDGE STA ZV147 UPPER RIB CRACKED AT AFT END. FABRICATED AND INSTALLED ANGLE REPAIR IAW SRM 55-01 FIG 2, SHEET 3.