What was found
CORROSION WAS DISCOVERED ON THE RT WING UPPER SKIN PANEL AT WS285.65. DAMAGE IS LOCATED NEAR THE AFT EDGE OF THE SKIN PANEL BETWEEN THE REAR SPAR AND STRINGER S-1. REMOVED CORROSION IAW SRM 57-20-01. PERFORMED HFEC INSPECTION OF BLENDED AREA IAW NDT MANUAL 51-00-19. NO DEFECTS NOTED. FABRICATED AND INSTALLED DOUBLER IAW DOCUMENT 470505REA06 AND FLIGHT VEHICLES CONSULTING DWG 57-13152-1, REV 1. FUEL LEAK CHECK GOOD IAW AMM 28-11-00.