What was found
DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, LBL 33, WL 208. REMOVED AND REPLACED CHORD PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 22Y CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 188, LBL 33, WL 208. REMOVED AND REPLACED CHORD PER SRM.