What was found
.75 INCH CRACK EXTENDING FROM RIVET HOLE AT LT VERTICAL STABILIZER SKIN 6 INCHES FORWARD OF FRONT SPAR BASE. REPAIRED PER M/M 54-30-0, PG 801.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
.75 INCH CRACK EXTENDING FROM RIVET HOLE AT LT VERTICAL STABILIZER SKIN 6 INCHES FORWARD OF FRONT SPAR BASE. REPAIRED PER M/M 54-30-0, PG 801.