What was found
VERTICAL STABILIZER TO FUSELAGE ATTACHMENT STRUCTURE BETWEEN STAB REAR SPAR AND T/E IS CRACKED ON FWD RT FLANGE ACCESS THROUGH PANEL 324CLX FS 1746. R & R ATTACHED STRUCTURE ANGLE IAW SRM-300 51-40-02. ACFT WAS GROUNDED.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STABILIZER TO FUSELAGE ATTACHMENT STRUCTURE BETWEEN STAB REAR SPAR AND T/E IS CRACKED ON FWD RT FLANGE ACCESS THROUGH PANEL 324CLX FS 1746. R & R ATTACHED STRUCTURE ANGLE IAW SRM-300 51-40-02. ACFT WAS GROUNDED.