What was found
FS280 BUTT STRAP HAS CORROSION AT 26L-26R. BLENDED CORROSION ON FS280 BUTT STRAP, NTD, REMAINING MATERIAL IS .076, ORIGINAL THICKNESS WAS .080, .004 REMOVED. COMPLIED WITH EA 05-2017-065.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FS280 BUTT STRAP HAS CORROSION AT 26L-26R. BLENDED CORROSION ON FS280 BUTT STRAP, NTD, REMAINING MATERIAL IS .076, ORIGINAL THICKNESS WAS .080, .004 REMOVED. COMPLIED WITH EA 05-2017-065.