What was found
DURING SCHEDULED C-5 INSPECTION DISCOVERED LEFT FUSELAGE SKIN CRACK BETWEEN FS 378.25 TO 393.25. REMOVED SKIN CRACK AND INSTALLED FILLER AND DOUBLER REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING SCHEDULED C-5 INSPECTION DISCOVERED LEFT FUSELAGE SKIN CRACK BETWEEN FS 378.25 TO 393.25. REMOVED SKIN CRACK AND INSTALLED FILLER AND DOUBLER REPAIR.