What was found
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED INNER FRAME CHORD PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE FRAME INNER CHORD CRACKED AT BS 348.2, STR 15L. REMOVED AND REPLACED INNER FRAME CHORD PER SRM.