What was found
STA 966 INBOARD VERTICAL FLANGE OF SUPPORT, THERE IS A CRACK 2.5 INCHES LONG, FORWARD OF AFT BOLT. ACCOMPLISHMENT OF PERMANENT REPAIR REQUIRED BY 30 APR 04. STA. 966 XW3 THE INBOARD VERTICAL FLANGE OF THE SUPPORT, THERE IS A CRACK 2.5 INCH LONG, FORWARD OF AFT BOLT. INSTALLED *TEMPORARY REPAIR PER FAA FORM 8110-3 DATED 23 APR 04, BOEING MSG 1-DFUSS. TEMPORARY REPAIR GOOD FOR 7 REVENUE FLIGHT DAYS. REMOVED AND REPLACED LT STA NR 3 WING/FUSELAGE FITTING IAW DOUG DRAWING 589477 AND DC8 SRM 51-1-20.