As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FRONT SPAR SUPPORT ANGLE LOCATED AT BS 1016 BETWEEN STR 2R AND 2L EXTERNAL FUSELAGE AT VERTICAL STABILIZER. REPLACED FRONT SPAR SUPPORT ANGLE PN 176A3101U26 LOC AT BS 1016 BTW STR 2R AND STR 2L EXTERNAL FUSELAGE AT VERTICAL STABILIZER IAW B737700 SRM 514002 AND DWG 176A3101 REV