What was found
INNER FUSELAGE SKIN IS CORRODED BETWEEN STRINGERS 21L AND 21R AT FRAME 67. REPAIRED FUSELAGE SKIN IAW EO EM-53MR-2189.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INNER FUSELAGE SKIN IS CORRODED BETWEEN STRINGERS 21L AND 21R AT FRAME 67. REPAIRED FUSELAGE SKIN IAW EO EM-53MR-2189.