What was found
CABIN LT STA 1189 XCW=108 - XCW=111 CTR WING UPPER PANEL FOUND CORROSION. CORROSION REMOVED IAW SRM 51-21-01, VOL II, REV 96. ORIGINAL THICKNESS = 0.132", REMAINING THICKNESS = 0.105", MATERIAL REMOVED = 0.027" FOUND EXCEEDED LIMIT IAW SRM 57-20-00, FIG 8A, VOL I REV 96. REPAIR CARRIED OUT IAW EA 8-5710-132436, THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.