What was found
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE ANGLE CRACKED, BS 360, LBL 68, WL 230. REMOVED AND REPLACED ANGLE PER SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE ANGLE CRACKED, BS 360, LBL 68, WL 230. REMOVED AND REPLACED ANGLE PER SRM.