What was found
RIGHT VERTICAL STAB TO FUSELAGE PANEL SKATE ANGLE CHAFING IN SEVERAL AREAS. REPLACED SKATE ANGLE PER AARD 51-10-05-1.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT VERTICAL STAB TO FUSELAGE PANEL SKATE ANGLE CHAFING IN SEVERAL AREAS. REPLACED SKATE ANGLE PER AARD 51-10-05-1.