What was found
FUSELAGE SKIN DAMAGE AT F/STA 736 TO 743 BETWEEN STRINGERS 24 AND 25. TO REPAIR FUSELAGE SKIN DAMAGE CAUSED BY A FORKLIFT. CUT OUT DAMAGE AND PERFORM REPAIR, PER DC-6 A&B SRM FIGURE 12-21 FUSELAGE PLATING REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN DAMAGE AT F/STA 736 TO 743 BETWEEN STRINGERS 24 AND 25. TO REPAIR FUSELAGE SKIN DAMAGE CAUSED BY A FORKLIFT. CUT OUT DAMAGE AND PERFORM REPAIR, PER DC-6 A&B SRM FIGURE 12-21 FUSELAGE PLATING REPAIR.