As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK FOUND ON DORSAL FIN FWD RIB FITTING. / [01] REMOVED DORSAL FIN FWD RIB AS PER REF B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW RIB AS PER REF B737-700 SRM 51-40-05-0G-0;[03] VERIFIED STEPS 1 AND 2. OK TO INSTALL NEW RIB.;[04] INSTALLED NEW RIB P/N 174A1108-2 AT DORSAL FIN FWD AS PER REF B737-700 SRM 51-40-02-0G-0 AND DWG # 174A1008;[05] VERIFIED STEP 4.