What was found
INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 2112-2116 BETWEEN S25L AND S26L. THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 7, FIGURE 202. A DIP WAS ISSUED TO REINSPECT THE AREA WITHIN 16,000 FLIGHT CYCLES AND TO PERFORM A PERMANENT REPAIR WITHIN 30,000 FLIGHT CYCLES IAW SRM 53-00-01, REPAIR 7, TABLE 204.