As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-7 CHECK, INSPECTION NOTED A CRACK IN THE FUSELAGE SKIN AT STA 727E STR 21 R. MAINTENANCE REMOVED THE DAMAGE. A DOUBLER WAS FABRICATED AND INSTALLED IN ACCORDANCE WITH THE REQUIREMENTS OF SRM 53-00-01 FIGURE 201 AND SRM 53-60-01.