What was found
VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BETWEEN DORSAL T/E STAB FORWARD ATTACH LUG. ACFT GROUNDED. REMOVED DAMAGED SKATE ANGLE, FABBED NEW ANGLE AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STAB TO FUSELAGE SKATE ANGLE CHAFED BETWEEN DORSAL T/E STAB FORWARD ATTACH LUG. ACFT GROUNDED. REMOVED DAMAGED SKATE ANGLE, FABBED NEW ANGLE AND INSTALLED IAW SRM 51-40-02-0G-0 AND 51-40-05-0G-0.