What was found
INSPECTION FOUND FASTENERS LOOSE AND PULLING THROUGH EXTERNAL FUSELAGE SKIN AT STA 1342 TO 1348, LT SIDE. A REPAIR CHANNEL AND SKIN WERE INSTALLED IAW SRM 54-30-3, FIGURE 7.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FASTENERS LOOSE AND PULLING THROUGH EXTERNAL FUSELAGE SKIN AT STA 1342 TO 1348, LT SIDE. A REPAIR CHANNEL AND SKIN WERE INSTALLED IAW SRM 54-30-3, FIGURE 7.