What was found
INSIDE VERTICAL STABILIZER LATERAL SUPPORT ANGLE CRACKED IN RADIUS AT BS. 1016, LBL 12, 8" ABOVE FUSELAGE SKIN / R&R ANGLE IAW DWG AND SRM.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSIDE VERTICAL STABILIZER LATERAL SUPPORT ANGLE CRACKED IN RADIUS AT BS. 1016, LBL 12, 8" ABOVE FUSELAGE SKIN / R&R ANGLE IAW DWG AND SRM.