What was found
UPPER WING SKIN CRACKED AT W/STA 96R, STRINGER #3. TO REPAIR A SMALL CRACK AROUND A FUEL QUANTITY PROBE ACCESS HOLE AT W/STA 96R, STRINER 3. TRIM OUT CRACK AND REPAIR SKIN PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-30.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPPER WING SKIN CRACKED AT W/STA 96R, STRINGER #3. TO REPAIR A SMALL CRACK AROUND A FUEL QUANTITY PROBE ACCESS HOLE AT W/STA 96R, STRINER 3. TRIM OUT CRACK AND REPAIR SKIN PER DC-6 A&B OVERHAUL MANUAL FIGURE 13-30.