What was found
CRACK IND IN EXTERNAL FUSE SKIN AFT I/B CORNER. REMOVED AND REPLACED SKIN PER DWG SR 27-53-024 & EA.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK IND IN EXTERNAL FUSE SKIN AFT I/B CORNER. REMOVED AND REPLACED SKIN PER DWG SR 27-53-024 & EA.