As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FWD CARGO COMPARTMENT, BS 500G FRAME HAS CRACK INDICATION BETWEEN STRINGERS 20R AND 21R AT 1.04 IN POWER FEEDER WIRE PENETRATION HOLE. CUT OUT CRACK AT WIRE PENETRATION HOLE .250 IAW SRM 53-00-07, FIG 202. FABRICATED REPAIR ANGLES FROM .050 7075-O PO 9001187 DIM 3" X 11", AND .063 7075-O PO 90011223 DIM 3" X 10". HEAT TREATED MATERIAL TO 7075T6 IAW FAS REPORT 2-37153-801 REV A. INSTALLED REPAIR ANGLES IAW SRM 53-00-07 REPAIR 13.