What was found
DURING ROUTINE C-CHECK INSPECTION, FUSELAGE L-35L CORRODED, STA 690.000 STA 781.000. REMOVED LEVEL I CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18. PERFORMED BLEND OUT 0.003”. MATERIAL THICKNESS 0.160”, REMAINING MATERIAL 0.157 FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-0 FIG 11 SHEET 3 PAGE 2P. CLEANED, TREATED AND PRIMED IAW DC-8 SRM 51-1-8B.