As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON S-26L AND SUPPORT ANGLES O/B OF S-26L AT STA 595. REMOVED CLIPS, FABRICATED NEW SECTION OF STRINGER AND SPLICE PER SRM 53-10-3. TREATED AND PAINTED PER PS 900-3-6 NR 3. INSTALLED STRINGER SECTIONS, SPLICE AND CLIP PER SRM 53-10-3 FIG 1.