As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON INNER DOUBLER BETWEEN FRAMES 39 AND 40 BOTTOM CENTERLINE OF FUSE. THINNEST AREA MEASURED .085 THICK. REPAIRED PER EA 6-5310-29140 DATED, 7-11-97. REMOVED CORROSION, FABRICATED STRAP FROM .003 2024.73 LENGTH WAS AREA PLUS 3 FASTENERS EACH END. CORROSION PROTECTED AREA AND STRAP AND INSTALLED WET WITH SEALANT AND FLUSH H6 LOCKS.