What was found
DURING ROUTINE C-CHECK INSPECTION RT WING INBD L/E SLANT PANEL UPPER SKIN SURFACE CORRODED, STA XCW 69.000 AND XFS 207.000. REPAIR ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, FAX TIN-N 043, BOEING MESSAGE DATE 03/31/2004. REMOVED CORROSION IAW DC8 SRM 51-1-I PG 17-18, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED SLANT PANEL IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-3-0 PG 1. TRIMMED OUT HOLE LOCATIONS ON NEW SLANT PANEL, FABRICATED FILLER, DOUBLER IAW BOEING MESSAGE 03-31-04, CLEANED, TREATED AND PRIMED AREA, FILLER, DOUBLER IAW DC8 SRM 51-1-8B. INSTALLED FILLER, DOUBLER ON NEW SLANT PANEL IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1 20D PG 9, DC8 SRM 51-3-0 PG 1, DC8 SRM 51-1-21 PG 1.