As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SUPPORT ANGLES 2 EA. UNDER PIE PANEL 8405 HAVE CORROSION ON UPPER SURFACES, ANGLES SUPPORT 2 EA PLUMBING LINES. REMOVED CORROSION PAIR THICKNESS .140 MATERIAL LOSS .050 FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02; INSTALLED FABED SUPPORT ANGLES UNDER PIE PANEL 8405; INSTALLED LINES IAW B737 MM 20-15-00 AND B737 MM 20-10-51; PERFORMED LEAK CHECK OF LINES IAW B737 MM 29-15-00 - NO LEAKS FOUND