What was found
SKIN LAP JOINT, AT STRINGER BS 259-360, HAS 9 SINK HOLES HAVE CRACK INDICATIONS. REMOVED DAMAGE PER SRM 53-30-3 FIG 5. COMPLETED REPAIR PER SB 53-0072 REV 5 AND SRM 53-30-3. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
SKIN LAP JOINT, AT STRINGER BS 259-360, HAS 9 SINK HOLES HAVE CRACK INDICATIONS. REMOVED DAMAGE PER SRM 53-30-3 FIG 5. COMPLETED REPAIR PER SB 53-0072 REV 5 AND SRM 53-30-3. (M)