As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL FIN L/H SUPPORT ANGLE ON FUSELAGE FOR PANELS 323AL 323BL 323CL HAS CORROSION. REF AAR N/R 9940933. CLEANED CLOSURE ANGLE ON UPPER FUSELAGE BELOW VERT. STAB FROM REF B737 SRM 53-80-71-2R-6. INSTALLED REPAIR ANGLE AND STRAP AS STA 1016 TO 1132, L/H SIDE AS PER REF B737 SOPM 20-30-03 NO PER REF 53-80-71-2R-6. CORROSION FOUND ONLY CRACK FROM STA 1016 TO 1027, CUT OUT DAMAGE SECTION ON CLOSURE ANGLE FROM STA 1016 TO 5.300 AS PER