As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HEAVY CORROSION ON SPLICE PLATE AFT OF BS 280 AND BETWEEN STRG 26L AND 26R. REMOVED CORROSION FROM BS 280 BUTTSTRAP, UPPER SURFACE BETWEEN FS280-284, STR 26L-26R IAW SRM 51-21-06-001-001 A01. COMPLIED WITH EC/TC EO 32-2016-109 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NONROUTINE WORK CARD.