What was found
FUSELAGE SKIN PANEL CORRODED BETWEEN BS. 360 TO BS 540, STRINGERS 24L - 27R. REPAIRED THE SKIN PANEL IAW SRM & EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN PANEL CORRODED BETWEEN BS. 360 TO BS 540, STRINGERS 24L - 27R. REPAIRED THE SKIN PANEL IAW SRM & EA.