As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK AT FRONT SPAR CONNECTING SECTION AT RIB 1,2.5 INCH LONG. REMOVED TRANSVERSE FITTING AT VERTICAL STAB FWD SPAR RIB 1 AND REMOVED CONNECTION SECTION AT RIB 1 IAW SRM 51-72-10 PG 1-3. CLEANED AREA IAW AMM 12-21-11. REPROTECTED AREA IAW SRM 51-75-10 PG 3-8. INSTALLED NEW CONNECTING SECTION AND TRANSVERSE FITTING IAW SRM 51-72-10 PG 1-3. REPROTECTED AREA PER A310 SRM 51-75-10 PG 3-8.