What was found
FUSELAGE NOSE SECTION SKIN CRACKED 1.125, STA 12.000 L-27R AT STRUCTURAL MODIFICATION. PERFORMED MAJOR REPAIR IAW EODHL-030549, ED3384. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP HOLE ON CRACK END USING A 0.250 DIA DRILL IAW EODHL-030549, ED-3384. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED A REPAIR DOUBLER (2024-T3 AL0.071) IAW EODHL-030549, ED-3384. CLEANED, TREATED AND PRIMED DOUBLER IAW SRM 51-1-8B. APPLIED PRC SEALANT ON FAYING SURFACES IAW SRM 51-1-11 PG 9. INSTALLED DOUBLER ON FUSELAGE NOSE SECTION SKIN, STA 12.00 L-27R USING NEW FASTENERS IAW EODHL-030549, ED-3384, SRM 51-1-21 PG 1.