As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED CLIPS AT S-9L, BS 360 AND AT S-10L, BS 360. THE INTERIM REPAIR IS APPROVED BY AD 2005-20-03 BY FAA FORM 8100-9. THE REPAIR STRUCTURE WILL BE RE-INSPECTED PER SB 737-53A1204 STARTING AT 38,165 PTC AND REPEATED EVERY 6,000 FLIGHT CYCLES THEREAFTER. REPAIRED REF SRM 51-40-02 AND EVA 71519 ON NR K4083G AND K4082G.