What was found
STRUCTURE INSIDE OF VERTICAL STAB PANEL 324CLX, ON TOP OF FUSELAGE HAS CRACKS IN FWD ANGLE. REMOVED WEB TO FORM IAW SRM 51-40-02, DRILLED AND INSTALLED NEW STIFFENER IAW SRM 51-40-05 AND 51-40-02,
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
STRUCTURE INSIDE OF VERTICAL STAB PANEL 324CLX, ON TOP OF FUSELAGE HAS CRACKS IN FWD ANGLE. REMOVED WEB TO FORM IAW SRM 51-40-02, DRILLED AND INSTALLED NEW STIFFENER IAW SRM 51-40-05 AND 51-40-02,