What was found
CORROSION ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; RBL 12; AND LBL 12.<[01] VERIFIED STEPS 1; 2; 5.;[02] REMOVED DAMAGE ON FUSELAGE CROWN SKIN FROM STA 1016+2 TO STA 1016+15; COMMON TO FASTENER HOLES AT BL 0; 10'X2.0' AREA; RBL 12;1.4'X0.800' AREA AND LBL 12; 12.3'X2.3' ALL I.A.W SRM 53-00-01-1A-1 ALLOWABLE DAMAGE 1 PAR 4.C(2)(A) DETAILS C.D AND MAINTENANCE WAS ACCOMPLISHED ON STEPS 1-6 AND WIP1 AND 2;[03] VERIFIED RII ITEMS COMPLETE.