What was found
INSPECTION TYPE-C, CRACK BS 211.8 RT SIDE AT WL 219.5 ON FUSELAGE SKIN. CRACK REMOVED PER SRM 53-30-3 FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION TYPE-C, CRACK BS 211.8 RT SIDE AT WL 219.5 ON FUSELAGE SKIN. CRACK REMOVED PER SRM 53-30-3 FIG 3.