As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE SKIN IS CRACKED AT FRAME 77 STRINGERS 6R-7R. PERFORMED SKIN BUSHING (.4375" BUSHING) REPAIR AT RIVET LOCATION ON EXTERNAL FUSELAGE SKIN AT FRAME 77 BETWEEN STRINGERS 6R-7R IAW SRM 53-32-01RE ITEM 9 FIGURE 213 AND EO1-53-22-0266.