What was found
INSPECTION FOUND L/H FUSELAGE SKIN DENTED AT BS 676 BETWEEN S27L AND S28L. REPAIRED IAW SRM 53-00-01, REPAIR 7, FIGURE 202. A DIP WAS INITIATED TO REINSPECT THE REPAIR AT 30,000 FLIGHT CYCLES WITH REPEAT INSPECTION AT 16,000 FLIGHT CYCLES PER SRM 53-00-01, REPAIR 7, TABLE 204.