As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE FIN TO BODY INTERFACE; SKATE ANGLE; IS CHAFED AT B.S. 1007-1016; L.B.L. 14. W.L. 307. / DAMAGE TO SKATE ANGLE AT BS 1007-1016; LBL 14; WL 307 FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE GIVEN IN B737-700 SRM. REPAIR BY REPLACEMENT IAW SRM 51-10-02; PARA 9. REMOVED DAMAGED ANGLE IAW SRM 51-40-02. INSTALLED A NEW ANGLE IAW SRM 51-40-02 AND DWG 147A0030; SH1; REV B