As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE-C/CK, 1 INCH CRACK IN FUSELAGE SKIN STA 1700 LONGERON 17 RIGHT ALONG SHEAR CLIP FASTENERS. REMOVED CRACKED SKIN IAW DC8 SRM 53-2-1 FIG 7. FABBED DOUBLER AND FILLER AND FINGER DOUBLER IAW DC8 SRM 53-2-1 FIG 7. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21A AND 51-1-20D AND 51-1-21.