As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 FUSELAGE SKIN CRACKED AT VERT FIN AND CENTER SPAR CANT BULKHEAD AT TACH POINT FS 1770 LONG 8L. TRIMMED OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR DOULBER AND SKIN FILLER IAW DC8 SRM 53-2-1 FIG 7. PERFORMED HFEC IAW DC8 NDT SPM 06-10-01.001. NO CRACKS NOTED. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.