What was found
CORROSION ON FUSELAGE SKIN AT RT WING L/E FILLET PANEL ON STA Y=803, LONG 29-28, RT ORIGINAL'S 0.157" AND REMAINING'S 0.088". ON STA Y=800, LONG 29-28, RT IS 0.150" AND REMAINING'S IS 0.087". ON STA Y=797, LONG 29-28, RT ORIGINAL'S 0.144" AND REMAINING'S 0.107". ON STA Y=793, LONG 29-28, RT IS 0.138" AND REMAINING'S 0.106". ON STA Y=790, LONG 29-28 RT IS 0.130" AND REMAINING'S 0.088", AND STA Y=786, LONG 29-28, RT IS 0.122" AND REMAINING'S 0.089". THEREFORE THESE ARE OUT OF LIMITS. REWORKED AREAS WIHIN LIMITS WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 26, 21 AND 14 AND 53-04, PAR 57. AREAS OUT OF LIMITS WILL BE ATTENDED WITH NRC 239.