What was found
DURING ROUTINE C CHECK INSPECTION, FOUND WING FUSELAGE PANEL NUMBER 716 FILLET PANEL RIGHT SIDE CRACKED AT STATION 690.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR REMOVED DAMAGED AREA. FABRICATED FILLER AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-8-1 PAGES 3-4, DC8 SRM 51-1-9 PAGE 1, DC8 SRM 53-2-4 PARAGRAPH 3, 51-1-9 PARAGRAPH 3AND 2.