What was found
CABIN RT STA 1189 XCW=-100 - XCW=-117 CTR WING UPPER PANEL FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01 VOL II, REV 96. ORIGINAL THICKNESS = 0.139", REMAINING THICKNESS = 0.107", MATERIAL REMOVED = 0.032" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A VOLUME I REVISION 96. REPAIR CARRIED OUT IAW EA.NR 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR GMM 6-2-100 REV 110.