What was found
VERTICAL STABILIZER FUSELAGE STA. 1018, 8" ABOVE FUSELAGE SKIN, LBL AND RBL 10", LATERAL SUPPORT RIB STIFFENER AT STRAIN RELIEF RADIUS, CRACKED ON BOTH ENDS. / R&R STIFFENER IAW SRM AND DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STABILIZER FUSELAGE STA. 1018, 8" ABOVE FUSELAGE SKIN, LBL AND RBL 10", LATERAL SUPPORT RIB STIFFENER AT STRAIN RELIEF RADIUS, CRACKED ON BOTH ENDS. / R&R STIFFENER IAW SRM AND DWG.