What was found
DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN, .50 INCH AT STA 859 ABOVE LT PYLON. INSTALLED DOUBLER REPAIR IAW SRM 53-01, FIG. 2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND CRACK IN FUSELAGE SKIN, .50 INCH AT STA 859 ABOVE LT PYLON. INSTALLED DOUBLER REPAIR IAW SRM 53-01, FIG. 2.