What was found
FUSELAGE SKIN CRACKED UNDER COPILOTS SLIDER WINDOW, IN 2 PLACES OUT OF RIVET HEAD. FABBED AND INSTALLED DOUBLER PATCH USING .032 7075-T6 PER DC-6 O/H MANUAL FIGURES 11-7, 11-37, 11-52, AND 12-22.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FUSELAGE SKIN CRACKED UNDER COPILOTS SLIDER WINDOW, IN 2 PLACES OUT OF RIVET HEAD. FABBED AND INSTALLED DOUBLER PATCH USING .032 7075-T6 PER DC-6 O/H MANUAL FIGURES 11-7, 11-37, 11-52, AND 12-22.