As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACCESS PANEL 139CL FORWARD KEEL BEAM REQUIRE FURTHER CLEANING AT PANEL ATTACH FRAMES AND CHECK ON CORROSION. CLEANED AREA IAW BOEING SOPM 20-30-03, REMOVED CORROSION ON LH A ND RH TEE BEAM BTW 995-1040 IAW B757-200 SRM 51-10-02-0G-0. ORIG INAL THICKNESS .130" REMAINING THICKNESS .127" FOUND TO BE WITHI N LIMITS IAW SRM 53-00-71-1A-1. REMOVED AND REPLACED SPLICE ANGLE IAW SRM 51-40-02-0G-0.