What was found
CRACK FOUND ON RT FUSELAGE SKIN AROUND RIVET HOLE AT FRAME 75, FIRST RIVET BELOW STR 2R. DOUBLER REPAIR IAW SRM 53-31-01 PARA 11. REF FCBS 53-30-07-001 FIG 1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK FOUND ON RT FUSELAGE SKIN AROUND RIVET HOLE AT FRAME 75, FIRST RIVET BELOW STR 2R. DOUBLER REPAIR IAW SRM 53-31-01 PARA 11. REF FCBS 53-30-07-001 FIG 1.