What was found
DURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP LWR FWD SKIN NON STANDRAD REPAIR, XF 16.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER + FILLER (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 L. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS 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.