As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION AFT PIT MAIN FRAME FWD ATTACH ANGLE BS 1680 BETWEEN S-28 - S-29R. REPAIRED CORROSION ON FRAME ATTACH ANGLE BY FABRICATING AND INSTALLING NEW FRAME ATTACH ANGLE FROM 7075-T6 .071" CLAD IAW B757 SRM 51-40-02, 51-70-11 AND 51-20-01.