What was found
DURING ROUTINE C-CHECK INSPECTION, LT WING INBOARD FLAP L/E LWR FWD PART DENTED, XW 40.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED FASTENERS IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER (AL 2024 T3 0.050) IAW DC-8 SRM 57-2-5 FIG 2 (SHEET 2, 4) DC-8 SRM 57-7-1 FIG 1 PAGE 2 ITEM -B- AND -N-. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) DC8 SRM 51-1-9A, DC8 SRM 51-1-21.