What was found
STABILATOR RUBS AGAINST FUSELAGE SCREW. .5 INCH GAP ON LT SIDE, .2500 INCH GAP ON RT SIDE. (GL13200405339)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STABILATOR RUBS AGAINST FUSELAGE SCREW. .5 INCH GAP ON LT SIDE, .2500 INCH GAP ON RT SIDE. (GL13200405339)