What was found
INSPECTION FOUND FUSELAGE SKIN CORRODED AT RT AFT OVERWING EXIT CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 16. THE EXIT HATCH WAS TESTED IAW MM 52-21-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND FUSELAGE SKIN CORRODED AT RT AFT OVERWING EXIT CUTOUT. THE SKIN WAS REPAIRED IAW SRM 53-30-3, FIGURE 16. THE EXIT HATCH WAS TESTED IAW MM 52-21-0.