What was found
INSPECTION FOUND EXTERNAL FUSELAGE SKIN UNDER FWD WING TO BODY FAIRING CORRODED AT STA 769 BETWEEN STRINGERS 28R AND 27R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 53 AND FILLET ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND EXTERNAL FUSELAGE SKIN UNDER FWD WING TO BODY FAIRING CORRODED AT STA 769 BETWEEN STRINGERS 28R AND 27R. A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 53 AND FILLET ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2.