What was found
VERTICAL STABILIZER INTERNAL SIDE LATERAL EXPANSION JOINT ANGLE CRACKED IN RADIUS AT BS. 1016, STR. 2L 3" O/B OF STR. 2L, 8" ABOVE FUSELAGE SKIN / REPAIRED ANGLE IAW SRM & DWG.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL STABILIZER INTERNAL SIDE LATERAL EXPANSION JOINT ANGLE CRACKED IN RADIUS AT BS. 1016, STR. 2L 3" O/B OF STR. 2L, 8" ABOVE FUSELAGE SKIN / REPAIRED ANGLE IAW SRM & DWG.