What was found
DURING INITIAL INSPECTION FOR SB57-3815, A CRACK WAS FOUND IN THE LEFT WING REAR SPAR CAP AFT FLANGE AT THE SUSPECT RIVET HOLE AT WS 115. THE CRACK STOPPED AT THE RADIUS OF THE VERITCAL LEG OF THE AFT SPAR WEB.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INITIAL INSPECTION FOR SB57-3815, A CRACK WAS FOUND IN THE LEFT WING REAR SPAR CAP AFT FLANGE AT THE SUSPECT RIVET HOLE AT WS 115. THE CRACK STOPPED AT THE RADIUS OF THE VERITCAL LEG OF THE AFT SPAR WEB.