What was found
FUSELAGE SKIN PANEL CORRODED BETWEEN BS 259 TO 360, BETWEEN STRINGERS 14 TO 24L. R & R THE SKIN PANEL IAW ER AND EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN PANEL CORRODED BETWEEN BS 259 TO 360, BETWEEN STRINGERS 14 TO 24L. R & R THE SKIN PANEL IAW ER AND EA.