As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 8L CRACKED AT RIB NR 8 STRINGER 8L, FIN STA 157.200 CRACK TERMINATES IN FASTENER HOLE AND HFEC INSPECTED AREA AND VERIFIED IAW NDTM 51.00.00 PART 6. FABRICATED REPAIR ANGLE IAW SRM 55.30.5 FIGURE 1. TREATED AND PRIMED PARTS IAW SRM 51.10.2. INSTALLED REPAIR PARTS AT STRINGER 8LT RIB NR 8 FIN STA 157.2 IAW SRM 55.30.5 FIGURE 1 AND 51.30.2.