As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXTERNAL FUSELAGE; STA 1016+3; LBL 11; 7' ABOVE FUSELAGE SKIN; LATTERAL ANGLE IS CRACKED IN RADIUS (COMMON TO FWD VERTICAL STAB A-FRAME FITTING) / REPMOVED AND REPLACED LATTERAL ANGLE P/N L776A3101-26 A TAG A84524 IAW BOEING DWG 3 176A3001 REV A.