What was found
VERTICLE STAB LT SIDE L/E ATTACH FLANGE HAS DRILL/ SCREW DAMAGE, 2ND LT FASTENER HOLE UP FROM FUSELAGE SKIN. ENLARGED THE FASTENER HOLE, REMOVE THE HIGH METAL AND FILL IN VOID WITH SEALANT IAW SRM PART II 51-40-02 AND 51-10-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICLE STAB LT SIDE L/E ATTACH FLANGE HAS DRILL/ SCREW DAMAGE, 2ND LT FASTENER HOLE UP FROM FUSELAGE SKIN. ENLARGED THE FASTENER HOLE, REMOVE THE HIGH METAL AND FILL IN VOID WITH SEALANT IAW SRM PART II 51-40-02 AND 51-10-03.