What was found
A 0.5 INCH CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN ON THE LT SIDE, AT S-11. CRACK RUNS FROM A FASTENER HOLE AT S-11 AND EXTENDS FWD FOR APPROXIMATELY 0.5 INCH. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER INSTALLED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
A 0.5 INCH CRACK WAS FOUND IN THE VERTICAL STABILIZER SKIN ON THE LT SIDE, AT S-11. CRACK RUNS FROM A FASTENER HOLE AT S-11 AND EXTENDS FWD FOR APPROXIMATELY 0.5 INCH. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER INSTALLED.