As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H SIDE OF VERTICAL STABILIZER; SKIN PANEL FASTENERS (2) ARE PULLED/PULLING TRHOUGH PANEL. 1.) 8.5' AFT OF DORSIL FIN T/E AND 44' UP FROM FUSELAGE SKIN. 2.) 11' AFT OF DORSIL FIN T/E AND 42' UP FROM FUSELAGE SKIN. / REPLACED 2 EACH FASTENERS AT L/H SIDE OF VERTICAL STABILIZER; SKIN PANEL 1) 8.5' AFT OF DORSIL FIN T/E AND 44' UP FROM FUSELAGE 2) 11' AFT OF DORSIL FIN T/E AND 42' UP FROM FUELAGE IAW SRM 51-40-02