What was found
FUSELAGE EXTERNAL SKIN AFT OF HOLD OPEN HOOK PIN CRACKED 0.375 STA 1610.000 L-14L TO L-15L (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 07-11-05, DWG Z20-R04 REV IR DATED 06-24-05. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1, SRM 51-1-20D PG. 21. CUT OUT DAMAGED SECTION IAW DWG Z20-R04. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED TRIPLER DOUBLER AND FILLER AND FINGER DOUBLER IAW DWG Z20-R04. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11 PG. 9. INSTALLED REPAIR PARTS IAW DWG Z20-R04, SRM 51-3-0 PG.1, SRM 51-1-21 PG 1, SRM 51-1-20D PG. 9, SRM 51-3-1 PG. 2A (TORQUED)