What was found
INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1350 LONG 34R. CUT OUT CRACK, NDT VERIFIED NO CRACK AT CUT OUT AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-1 FIG 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA 1350 LONG 34R. CUT OUT CRACK, NDT VERIFIED NO CRACK AT CUT OUT AREA. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-1 FIG 7.