What was found
VERTICAL STAB RT ATTACH ANGLE CRACKED AT AFT T/E AREA. REMOVED RT SIDE VERTICAL STAB AFT ATTACH ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. INSTALLED ANGLE IAW AMM 51-42-13-001-001-A01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB RT ATTACH ANGLE CRACKED AT AFT T/E AREA. REMOVED RT SIDE VERTICAL STAB AFT ATTACH ANGLE IAW SRM 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. INSTALLED ANGLE IAW AMM 51-42-13-001-001-A01.